Abstract:
This invention relates to internal combustion engines and more particularly to internal combustion engines and methods of operating the engines with a new fuel saving cycle. Various embodiments use a passage between adjacent cylinders to enable a mode in which fuel combusted in one cylinder supplies pressure to the other that has not been supplied with fuel, thus enabling driving of both cylinders with less fuel.

Description:
[0001]    The present application claims priority to U.S. application Ser. No. 13/475,253, filed May 18, 2012, and U.S. Provisional Appln. Ser. No. 61/768,127, filed Feb. 22, 2013. Each of these applications is incorporated herein by reference in their entirety. 
     
    
     FIELD OF THE INVENTION 
       [0002]    This invention relates to internal combustion engines and more particularly to internal combustion engines and methods of operating the engines with a new fuel saving cycle. 
       BACKGROUND OF THE INVENTION 
       [0003]    The present economic condition is particularly bad with respect to gasoline and diesel fuel for cars and heavy trucks. While efforts are being made to provide hybrid automobiles that can operate on rechargeable batteries at least part of the time, nevertheless most still have engines as well that must rely upon gasoline or diesel fuel. The need to make engines more efficient still exists particularly because of rising gasoline and diesel fuel costs. 
       BRIEF DESCRIPTION OF THE INVENTION 
       [0004]    It is an object of the present invention to provide an internal combustion engine which achieves a measure of fulfillment of the need for more efficient and fuel saving engines. 
         [0005]    In accordance with the principles of this inventions this objective is achieved by providing an engine which includes at least two piston and cylinder assemblies preferably adjacent to one another, at least one of which includes a fuel injector and both of which are connected to a crank shaft so that the pistons of both assemblies move simultaneously through repetitive cycles each, including simultaneous compression strokes and immediately following simultaneous power drive strokes. The two assemblies, when operating with the new fuel savings cycle, establish at the end of the simultaneous compression strokes a charge of compressed air in one cylinder of one of the assemblies and a charge of compressed air fuel mixture in the other cylinder of the other assembly. When the air fuel mixture is ignited, the high pressure conditions in the other cylinder are immediately communicated through a passage to the one cylinder to accomplish a double expansion during the simultaneous power drive strokes thus using much of the pressure energy before exhaust occurs by the pistons themselves rather than to dump it as is usually done. 
         [0006]    Preferably, the engine includes a second fuel injector which is controlled selectively with respect to the first fuel injector to operate in accordance with a normal mode where both assemblies are simultaneously operated alike in which case both cylinders establish a charge of compressed air-fuel mixture at the ends of the simultaneous compression strokes so that in effect a double charge can be ignited to act on both pistons simultaneously. 
         [0007]    The invention can be embodied in engines in which the injections made by the injectors cause the ignition (as in conventional compression ignition) or in which the injections are made during simultaneously intake strokes and ignition is made by a spark ignition system. In the case of spark ignition, under normal mode operation the ignition of the second air fuel charge is ignited by a high pressure flame resulting from the ignition in the first cylinder extending through the passage. 
         [0008]    The engines embodying the principles of the present invention can be operated either on a four cycle basis or a two cycle basis. 
         [0009]    The invention is most easily applicable to engines of the opposed piston type. A particularly efficient embodiment utilizes the opposed pistons in one cylinder type of setup utilized in the new Eco Motors (located in Allen Park, Mich.) engine. The Eco Motors set up includes two cylinders disposed on opposite sides of a central portion of the crankshaft. The central portion of the crankshift is connected to a pair of connecting rods so as to move a pair of pistons one within each cylinder in two stroke cycles out of phase 180° with respect to one another. An opposing piston is mounted in the cylinders, each of which is constrained to move in a cooperating two stroke cycle by a pair of parallel elongated connecting rods pivoted to an opposing piston and to the crankshaft so as to be 180° out of phase with respect to one another. 
         [0010]    The Eco Motors engine is advertised as being modular. A dual modular engine includes two modular engines connected together by a clutch assembly. The dual modular engine is comparable to the eight cylinder engines capable of operating on four cylinders only to save fuel. Thus, instead of four non-fueled piston and cylinder assemblies simply going through the motions, the clutch makes it possible to render one modular engine totally inoperable. 
         [0011]    One of the objects of the present invention is to reconfigure the Eco Motors dual modular with clutch engine (or another similar such engine) and achieve selective normal operation and fuel saving operation in an improved new cycle way so that the reconfiguration saves parts and the new cycle is more efficient when compared with the dual modular Eco Motors engine and its operation in fuel saving mode. 
         [0012]    In accordance with the principles of the present invention the above objective is achieved by abandoning the modular idea and mounting two side by side cylinders on opposite sides of a single central crank shaft so that in each pair of cylinders a pair of opposed pistons move simultaneously through the same two stroke cycle. In this way the events occurring in each pair of side by side cylinders are the same but 180° out of phase with one another. The fuel saving mode is accomplished simply by providing a passage between each pair of side by side cylinders at the central combustion chamber areas, and then reprogramming the computer operated fuel injectors so that one of the two injectors for the two cylinders does not inject instead of both injecting as in normal operation. Consequently, in fuel saving mode the one cylinder which receives an injection when ignited will immediately communicate the resulting high pressure conditions through the passage to the other cylinder to raise the charge of air therein at compression pressure. With the pressure created by the one ignition acting on two pistons to effect simultaneous power drive strokes of two pistons a double working pressure expansion occurs, thus utilizing much of the pressure energy that usually is dumped to exhaust. 
         [0013]    Another related aspect of the invention provides an internal combustion engine comprising: a frame structure, a pair of piston and cylinder assemblies mounted on said frame structure including two side by side cylinders and pistons movably mounted in the cylinders for simultaneous movements through repetitive cycles, each including simultaneous compression strokes and immediately following simultaneous power drive strokes, and an output shaft connected with said pistons so as to be moved by the pistons through a predetermined number of rotational movements during each cycle of movement of the pistons. A fuel injection and charge ignition system includes an injector operatively associated with one of the piston and cylinder assemblies and another injector operatively associated with the other of the piston and cylinder assemblies. The fuel injection and charge ignition system is constructed and arranged in one mode of operation to establish at the beginning of the simultaneous power drive strokes of the pistons of both cylinders a charge of ignitable compressed air fuel mixture in one of the cylinders and a charge of unignitable compressed air in the other of the cylinders. A passage between the side-by-side cylinders communicates the high pressure conditions created by the ignition of the charge of ignitable air-fuel mixture in the one of the cylinders with the charge of compressed air to raise the pressure in the other of the cylinders during the one mode to move the number of the pistons associated therewith through the simultaneous drive stroke thereof. 
         [0014]    The fuel injection and charge ignition system is constructed and arranged to operate in a second mode of operation to establish at the beginning of the simultaneous power drive strokes a charge of ignitable compressed air-fuel mixture in both cylinders so that the ignition of both ignitable charges moves the pistons of both assemblies together through the simultaneous power drive strokes thereof. A controller is provided for selecting between the first and second modes of operation for the fuel injection and charge ignition system. 
         [0015]    Aspects of the present application also relate to dual mode improvements in engines of the type contemplated by Pinnacle Engines, Inc. as exemplified in the following Pinnacle patent disclosures, each of which is hereby incorporated by reference into the present application: US Pat Appln. Pub. No. 2009/0266329 Dated Oct. 29, 2009; US Pat. Appln. Pub. No. 2010/0147269 Dated Jun. 17, 2010; US Pat. Appln. Pub. 2010/0212622 Dated Aug. 26, 2010; US Pat. Appln. Pub. No 2011/0041799 Dated Feb. 24, 2011; US Pat. Appln. Pub. 2011/0220058 Dated Sep. 15, 2011; US. Pat. Appln. Pub. No. 2012/0085302 Dated Apr. 12, 2012; and US Pat. Appln. Pub. No. 2012/0085305 Dated Apr. 12, 2012. 
         [0016]    A typical Pinnacle type engine as disclosed in the cited disclosures includes a plurality of opposed piston and cylinder assemblies in which the cylinder of the assembly is made up of two cylinder sections movable separately toward and away from one another to seal off and open a centrally located inlet by one cylinder section and a centrally located outlet to the other cylinder section. A distinct feature of the Pinnacle engine is the ability to move one of the crankshaft driven piston units of one assembly toward and away from the opposed crankshaft piston driven unit of the other assembly to thereby change the compression ratio within the cylinders as between the two assemblies. While the patent disclosures of the Pinnacle type engine attributes various advantages to these features, the arrangement does not provide for selective operation in a normal mode or in a fuel saving mode where fuel injection is cut off. 
         [0017]    In a fuel saving mode, one example of this type of dual mode operation is the type presently built into eight cylinder engines wherein four of the eight cylinders are not fed fuel as they go through their cyclical movements. Another example is to provide two unitized engines with a clutch between them enabling one to be completely shut down. See, for example, US Pat. Appln. Pub. No. 2010/0056327. Both of these examples involve disruption of operation and non use of parts. 
         [0018]    The present invention contemplates the provision in a Pinnacle type engine of a dual mode of operation in an improved manner where all parts function in both modes; which renders the engine in fuel saving mode to be more efficient while allowing full variable Pinnacle operation. The improvement of the present invention contemplates the use of the underlying principles of the dual mode of operation discussed above and with respect to example embodiments disclosed below, and also disclosed in my pending U.S. Patent Application Ser. No. filed Ser. No. 13/475,253 filed May 18, 2012. That application is hereby incorporated by reference into the present application. Thus, two piston and cylinder assemblies which in normal mode operate separately in usual fashion have a fuel saving mode wherein only one assembly fed fuel is fired and the high pressure conditions created by the firing are transmitted to the other assembly to drive it simultaneously, the increased expansion being more efficient. 
         [0019]    The present invention contemplates allowing each one of two parallel piston and cylinder assemblies of a Pinnacle type engine to operate at all times 180° out of phase with each other with all variables and to add a two stroke piston and cylinder assembly valved by piston movement between the two four stroke pinnacle assemblies. The two stroke assembly is constructed (1) so that the fuel component normally fed thereto can be selectively cut off, leaving the internal pressure condition at normal firing time simply air under compression pressure, and (2) so that alternately this compression air pressure condition can be alternately communicated with the combustion chamber of a 4 stroke assembly during the firing stroke thereof so as to drive the two stroke assembly through a simultaneous increased pressure drive stroke. 
         [0020]    The two stroke assembly preferably has a displacement greater than the four stroke assemblies. It can be seen that in normal operation, the two stroke assembly is fed fuel twice during one feed of fuel to each 4 stroke assembly. Consequently, when the fuel saving mode is in operation the two fuel feeds to the two stroke assembly are saved, and there is a fuel saving of at least one half when compared with normal. Moreover, the added expansion by the two stroke assembly during each four stroke assembly cycle serves as an efficiency booster in the fuel saving mode. 
         [0021]    Others objects, features and advantages of the present disclosure will become apparent from the following detailed description, the accompanying drawings, and the appended claims. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0022]      FIG. 1  is a horizontal sectional view of an internal combustion engine embodying the principles of the present invention; 
           [0023]      FIG. 2  is a section view taken alone the line  2 - 2  of  FIG. 1 ; 
           [0024]      FIG. 3  is a schematic view showing a pressurized air intake system; 
           [0025]      FIG. 4  is a schematic view showing a computer controlled fuel injection system; 
           [0026]      FIG. 5  is a top plan view of another engine embodying the principles of the present invention with parts broken away and shown in horizontal section for purposes of clearer illustration; 
           [0027]      FIG. 6  is an enlarged horizontal sectional view of one end portion of the engine of  FIG. 5  showing the position of the parts in mid stroke; 
           [0028]      FIG. 7  is a view similar to  FIG. 6  showing the position of the parts after a 180° turn of the output shaft from the position show in  FIG. 6  shaft; 
           [0029]      FIG. 8  is a view similar to  FIG. 5  showing the position of the parts after another 180° turn of the output shaft from the position shown in  FIG. 7 ; 
           [0030]      FIG. 9  is a view similar to  FIG. 5  showing the position of the parts after another 180° turn of the output shaft from the position shown in  FIG. 8 ; 
           [0031]      FIG. 9A  is a schematic diagrammatic view of a preferred computerized system for controlling the fuel injectors of the engine shown in  FIGS. 5-9 ; 
           [0032]      FIG. 10  is a horizontal sectional view of a spark ignited engine embodying the principles of the present invention which operates on a two stroke cycle; 
           [0033]      FIG. 11  is a top plan view of an internal combustion engine embodying the principles of the present invention showing the three opposed crankshaft driven opposed pistons and cylinder assemblies of the engine in horizontal section arranged with a two stroke assembly between two four stroke assemblies with the opposed pistons of the three assemblies two 4 stroke assemblies in minimum spaced apart combustion chamber defining limiting positions; 
           [0034]      FIG. 12  is a view similar to  FIG. 11  wherein the opposed pistons are disposed in a maximum spaced apart limiting position; 
           [0035]      FIG. 13  is a diagrammatical view showing the components of the engine shown in  FIGS. 11 and 12  which enable the combustion ratio of the two four stroke assemblies to be varied; 
           [0036]      FIG. 14  is a block diagram view of a computer controlled operating system forming a part of the engine shown in  FIGS. 11 and 12  when embodied in an automotive vehicle as a drive motor for the vehicle; 
           [0037]      FIG. 15  is a schematic line diagram view of one modification of the internal combustion engine shown in  FIG. 11 ; and 
           [0038]      FIG. 16  is a view similar to  FIG. 5  showing another modification. 
       
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
       [0039]    Referring more particularly to the drawings, there is shown in  FIGS. 1 and 2  there of an internal combustion engine, generally indicated at  10 , that embodies the principles of the present invention. 
         [0040]    The engine  10  includes a main frame structure  12  shown illustratively as one piece in the drawings. In actuality, the frame may be made up of many conventional pieces. In the illustrative one piece embodiment shown the frame structure defines pairs of side by side cylinders  14 L and  14 R disposed in general alignment on opposite sides of an output crank shaft  16 . Mounted within the pairs of cylinders  14 L and  14 R are pairs of opposed pistons  18 L and  20 L and  18 R and  20 R respectively. 
         [0041]    The pair of pistons  18 L are slidably sealingly mounted in the pair of cylinders  14 L for simultaneous movements together toward and away from the crank shaft  16  by a pair of connecting rods  22 L pivotally connected at one of their ends to the pair of pistons  18 L (as by wrist pins not shown) with their opposite ends rotatably mounted on two aligned interior cranks  24  of the crank shaft  16 . 
         [0042]    The pair of pistons  18 R are slidably sealingly mounted in the pair of cylinders  14  R for simultaneous movements together toward and away from the crank shaft  16  by a pair of connecting rods  22 R pivotally connected at one of their ends to the pair of pistons  18 R (as by wrist pins not shown) with their opposite forked ends rotatably mounted on the two interior cranks  24 . 
         [0043]    The pair of pistons  20 L are slidably sealingly mounted in the pair of side by side cylinders  14 L outwardly of the pair of pistons  18 L therein for simultaneous movements toward the pistons  18 L as the pistons  18 L move away from the crankshaft  16  and away from the pistons  18 L as the pistons  18 L move toward the crank shaft  16 . 
         [0044]    The simultaneous movements of the pair of pistons  20 L is accomplished by a pair of fixed rods  26 L extending outwardly of the pair of pistons  20 L and having a shaft  28 L extending transversely therethrough so as to be relatively pivoted with respect to the piston rods  26 L about the axis of the shaft  28 L. The shaft  28 L moves within three axially spaced slots  30 L formed in the adjacent end of the frame structure  12  as shown, the central portion of the shaft  28 L extending between the spaced connecting rods  26 L slides in the central slot  30 L and opposite ends of the shaft  29 L extend outwardly of the rods  26 L through the outer two slots  30 L and then beyond the adjacent frame structure  12 . 
         [0045]    Pivoted to the outwardly extending ends of the shaft  28 L are one of the ends of a pair of exterior connecting rod&#39;s  32 L. The pair of exterior connecting rods  32 L extend inwardly toward the crank shaft  16  and have their inner ends rotatably connected to two exterior cranks  34  on the opposite ends of the crank shaft  16  transversely outwardly of the adjacent frame structure  12 . 
         [0046]    The pair of outer pistons  20 R are related to the pair of inner pistons  18 R and move simultaneously together and away from one another by a similar assembly of components including piston rods  26 R, shaft  28 R moving in slots  30 R and a pair of exterior connecting rods  32 R having their inner ends rotatably connected to the cranks  34  of the crank shaft  16  and their outer ends pivotally connected with outer ends of the shaft  28 R. 
         [0047]    It can be seen from the connection of the connecting rods  22 L and  22 R, between the crank shaft  16  and inner pairs of pistons  18 L and  18 R and the connection of the exterior connecting rods  32 L and  32 R between the crank shaft  16  and the outer pairs of pistons  20 L and  20 R, the pairs of pistons  18 L and  20 L move simultaneously trough two stroke repetitive cycles each including (1) a compression stroke wherein the pairs of pistons  18 L and  20 L move from an outer limiting position spaced widely apart toward one another into inner limiting position spaced apart but almost together and (2) a power drive stroke wherein the pairs of pistons  18 L and  20 L move from the inner limiting position to the outer limiting position away from one another. 
         [0048]    The pairs of pistons  18 R and  20 R have a similar two stroke repetitive cycle. However, since they are connected to the same cranks of the crank shaft  16  (i.e., at the same crank axis), the two stroke cycle thereof is displaced 180° from the two stroke cycle of the pairs of pistons  18 L and  20 L. Stated differently, the pistons  18 L and  20 L move through a compression stroke while the pistons  18 R and  20 R move through a power drive stroke and when the pistons  18 L and  20 L move through a power drive stroke the pistons  18 R and  20 R move through a compression stroke. 
         [0049]    The pistons  18 L- 20 L and  18 R- 20 R are moved through repetitive out of phase two stroke cycles during each revolution of the crankshaft  16  because during the time when the pistons are near the outer limiting positions a flow of air under pressure is made to pass into one end of each pair of side by side cylinders  14 L or  14 R through an inlet opening  36  in each cylinder  14  and out an outlet opening  38  at the opposite end of each cylinder. Conversely, the pistons in the other cylinders are in the inner limiting position and the openings  36 ,  36  are closed off. 
         [0050]      FIG. 3  illustrates schematically how a pump  41  (suitable to be driven by the output shaft  16 ) feeds a pressurized flow of air through tubes to each inlet opening  36  when the inlet openings and outlet openings  38  are opened in accordance with known practice by the movement of the associated pistons  18  or  20  thereby near the end of the power drive strokes thereof. 
         [0051]    As the pistons  18  and  20  move through the initial portion of their compression stroke, the pressurized air that has moved into the cylinders  14  is trapped therein because the pistons move past the openings  36  and  38  in the opposite direction to close them. The trapped air is then pressurized as pistons  18  and  20  move together in their compression stroke. 
         [0052]    In the embodiment shown, the compression ratio is chosen so that when the pistons  18  and  20  reach near or at their inner limiting positions, the pressure and temperature conditions of the air is such that an injection of fuel also causes compression ignition to occur. 
         [0053]    As shown in the drawings, there is a fuel injector  42  carried by the frame structure  12  in association with each cylinders  14  is positions so that its nozzle enters within the cylinder  14  in the combustion chamber space between the pistons  18  and  20  when in their inner limiting positions. 
         [0054]      FIG. 4  illustrates schematically the four fuel injectors  42  having high pressure fuel lines  44  leading thereto from a conventional source, indicated schematically by the numeral  46 . The fuel injectors  42  are constructed and arranged with electrically operated valves shown schematically at  48  which open to inject fuel into the cylinder  14  and close to stop injection. Electrical lines  50  are shown schematically connected to the valves  48 . The lines  50  are shown connected to a controller, such as a computer, shown schematically by the numeral  52 . The lines  50  transmit signals to the valves  48  to open and close them with the interval between the opening signal and the closing signal determining the amount of fuel injected. 
         [0055]    Also, each pair of side by side cylinders  14  are made to communicate with one another by a passage  54  extending between each side by side pair at central portions thereof opposite the injectors  42 . The computer  52  is programmed to selectively cause one injector  42  associated with one cylinder of each pair of side by side cylinders  14  to inject zero fuel or in other words not to inject. 
         [0056]    The computer  52  normally operates the four injectors  42  to inject the same amount of fuel into both of each same-side pair of cylinders  14 L or  14 R to cause ignition to occur therein bearing in mind that the injection in the one pair of cylinders  14 L or  14 R is 180° out of phase with other pair of cylinders  14 L or  14 R. It will be noted that simultaneous ignition occurs in both cylinders of a pair so that passage  54  is not significantly in play as the high pressure created by ignition in both cylinders  14  will act on both pairs of opposed pistons  18  and  20 . 
         [0057]    When the computer  52  signals one of the two injectors  42  of each same-side pair of cylinders  14  not to inject, the ignition of the fuel in the other that receives fuel causes high pressure to rise in that cylinder  14 , which high pressure is immediately communicated by the passage  54  to the other cylinder  14  at the lower compression pressure so that both pairs of opposed pistons  18  and  20  are moved through power drives strokes together. In effect, the single ignition results in double working expansion of the pressure energy created. 
         [0058]    This fuel saving mode of operation which can be selected by the computer  52  reduces the fuel used by the engine in half just as is done with the V-8 that can selectively operate on four cylinders or the dual modular Eco Motor with clutch. The fuel saving mode of the present invention operates all moving components of the engine with a more efficient use of the lesser fueled ignitions. 
         [0059]    In order for the computer  52  to select the fuel saving mode in automobile usage, the function of the automobile must be electrically sensed and transmitted to the computer  52 . Known sensors exist in automobiles equipped with the V-8 Engine that operates fuel savings with four cylinders. For example, normal operation is selected when the gas pedal movement to accelerate the car is sensed and fuel saving mode is selected when brake pedal movement is sensed. Cruise control when sensed to be on could be used to select fuel saving mode. Sensing motor rotation without wheels turning (idling) would select fuel saving mode. 
         [0060]    Referring again more particularly to the drawings there is shown in  FIGS. 5-9  thereof a spark ignite internal combustion engine, generally indicated at  110 , embodying the principles of the present invention. The engine  110  includes a frame structure, generally indicated at  112 , which is shown, in  FIG. 5  as being of three piece construction including a main body structure  114  with a head structure  116  on opposite ends of the main body structure  114 . It will be understood that the three piece construction is illustrative only and that the frame structure  114  would be actually constructed in many pieces in accordance with known practice. 
         [0061]    As shown in  FIG. 5 , the engine  110  is opposed piston configuration having opposed duplicate operative piston and cylinder assemblies connected to opposite sides of a centrally located output crankshaft  124  so that the assembles are 180° out of phase with respect to one another. 
         [0062]    Since the piston and cylinder assemblies are duplicates of one another, a description of one will suffice to give an understanding of both, keeping in mind that they are 180° out of phase with respect to one another. 
         [0063]    Referring now more particularly to the drawings there thereof as best shown in  FIGS. 5-8 , the body structure  114  includes structures defining four inline cylinders, designated by the numeral  118  with added letters A through D respectively. Slid ably sealingly mounted in the four cylinders  118  are four pistons, designated by the numeral  120  with added letters A through D respectively. 
         [0064]    Each piston  120  has one end of a connecting rod  122  pivotally connected thereto as by a conventional wrist pin (not shown). The opposite end of each connecting rod  122  is rotatably connected to the output shaft  124 . The output shaft  124  is formed with four U-shaped crank portions, designated by the numeral  126  with added letters A through D respectively, spaced apart by straight bearing portions  128  journalled in bearings suitably mounted on the body structure  114 . The crank portions  126 A and  126 D are oriented to extend outwardly from the adjacent bearing portions  128  in the same directions and the crank portions  126 B and  126 C are oriented to extend outwardly from the adjacent bearing portions  128  in the same direction but disposed 180° from the direction of extent of the crank portions  128 . 
         [0065]    Each connection between the ends of the piston rods  122  with the output crank shaft  124  is accomplished by journaling an end of a respective piston rod  122  rotationally on the right of a respective U-shaped crank portion  126 . As a result of the orientation of the crank portions  126  and the connection of the piston rods  122  rotatably connected thereto and to the pistons  120  for pivotal movement, the pistons  120 A and  122 D will move together through simultaneous strokes in one direction while the pistons  120 B and  120 C move together through simultaneous strokes in an opposite direction. 
         [0066]    The head structure  116  which defines an end wall closure for all four cylinders  118  has formed therein an air supply passage designated by the numeral  132  with added letters A through D respectively which communicates with the four cylinders  118  through four inwardly facing valve seat defining inlet openings designated by the numeral  134  with added letters A through D respectively. The head structure  116  also has formed therein four exhaust passages designated by the numeral  136  with added letters A through D respectively which communicate with the four cylinders  118  through four inwardly facing valve seat defining outlet openings, designated by the numeral  138  with added letters A through D respectively. 
         [0067]    Mounted on the head structure  116  for movements toward the inlet openings  134  into sealing relation thereto and away from the inlet openings  134  into opening relation thereto are four stem operated poppet valves, designated by the numeral  140  with added letters A through D respectively. Also mounted on the head structure  116  for movements toward the outlet openings  138  into sealing relation thereto and away from the outlet openings  138  into opening relation thereto are four stem operated poppet valves, designated by the numeral  142  with added letters A through D respectively. 
         [0068]    The poppet valves  140  and  142  are spring biased to move into sealing relation with their associated openings  134  and  138  by conventional springs  139  and are moved against the spring bias into opening relation to their associated openings  134  and  138  by a camshaft  144  rotatably mounted on the head structure  116  in a position overlying the valves  140  and  142  and the openings  134  and  138 . The camshaft  144  is rotationally moved at a rotational speed one half the rotational speed of the output shaft  124  by a conventional rotational movement transmitting mechanism  145  connected between the output shaft  124  and the camshaft  144  so that during every two revolutions of the output shaft  124  the camshaft  144  is driven thereby through one revolution. In this way, the camshaft  144  is able to move the valves  140  and  142  through one cycle of movement while the pistons  120  are moving through a four consecutive 180° strokes of movement. 
         [0069]    The sequence of the cycle of movements of the valves  140  and  142  is determined by four inlet opening and closing cam portions, designated by the numeral  146  with added letter A through D respectively. 
         [0070]    Formed on the camshaft  144  in axially spaced relation in alignment with and to engage the stem end of the four inlet valves  140  are four outlet opening and closing cam portions, designated by the numeral  148  with added letters A through D respectively. The cam portions  148  are formed on the camshaft  144  in axially spaced relation in alignment with and to engage the stem ends of the four outlet valves  142 . Each cam portion  146  and  148  is configured to provide (1) leading surfaces which when engaged with a valve stem moves the valve  142  or  144  in opening relation to the associated opening, (2) a trailing surface which when engaged with a valve stem moves the valve  140  or  142  into sealing relation to the associated opening and (3) a central surface between the leading and trailing surfaces which when engaged with a valve stem holds the valve  140  or  142  in opening relation to the associated opening. The four stroke cycle of movement of each piston  120  controlled by the rotation of the output shaft  124  through two revolutions are as shown in  FIGS. 6-9  and indentified in order as an intake stroke, a compression stroke, a power drive stroke, and an exhaust stroke. The coordinated movements of each inlet valve  140  and outlet valve  142  during the four identified piston strokes of the associated piston  120  is as follows (1) during the intake stroke inlet valve  140  is opened and outlet valve  142  is closed (2) during the compression and power drive strokes both valves  140  and  142  are closed and during the exhaust stroke inlet valve  140  is closed and outlet valve  142  is opened. The exact timing of the required valve movement within the associated strokes is in accordance with known practice. 
         [0071]    It will be understood that the four supply passages  132  are communicated with a source of filtered air similar to that shown in  FIG. 3  and the four exhaust passage  136  are communicated with a muffled exhaust manifold (not shown). 
         [0072]    The engine  110  also includes four fuel injectors, designated generally by the numeral  150  with added letters A through D respectively. The four fuel injectors  150  are of known construction and embody a known control system similar to the one shown in  FIG. 4  an example, is embodied in a 4 cylinder, four cycle GM engine. Each injector  150  is communicated with a pressurized fuel containing manifold (not shown) through a opening in an upper end  152  thereof. Each upper open end  152  communicates the fuel under pressure received therein to a lower discharge nozzle  154 . Each injector  150  also includes an electrically controlled valve similar to the valves between the upper ends  152  of  FIG. 4  and lower nozzle  154 , which allows fuel under pressure to flow from the nozzle  154 , when open, and to prevent the flow of fuel under pressure from the nozzle  154  when closed. The timing between the opening of the control valve and the closing of the control valve determines the amount of fuel injected. The electrically operated control valves are operated by electrical signals from a computerized system as shown in  FIG. 9A . 
         [0073]    In accordance with the principles of the present invention, the frame structure  116  has a passage  156  formed therein that communicates cylinder  118 B to cylinder  118 C (the two middle cylinders) adjacent the valve ends thereof. 
         [0074]    A conventional distributor —spark plug ignition system is provided for the engine  110 , the distributor components of which also not shown, the ignition system includes a spark plug  162  associated with cylinder  118 B and spark plugs  164 A and  164 D associated with cylinders  18 A and  18 D. 
         [0075]    In the normal operation of the engine  110 , the pistons  120 A and  120 D in cylinders  118 A and  118 D have simultaneous intake strokes during which the injectors  150 A and  150 B inject the same amount of fuel into the air being drawn into the respective cylinder  118 A or  118 D. The charges of air fuel mixture within the cylinders  118 A and  118 D established at the end of the simultaneous intake strokes of pistons  120 A and  120 D therein are compressed during the following simultaneous compression stroke of the pistons  120 A and  120 D into compressed charges of mixed fuel and air. When the spark plugs  164 A and  164 D are simultaneously activated, the pistons  120 A and  120 D will be moved through their simultaneous power drive strokes, followed by simultaneous exhaust strokes. 
         [0076]    In normal operation, the injectors  150 B and  150 C in cylinders  118 B and  118 C are also injected with the same amount of fuel as cylinders  118 A and  118 D. When pistons  120 B and  120 C establish charges of compressed air and fuel mixture therein at the end of the simultaneous compression strokes thereof, the charges of compressed air and fuel mixture in cylinders  118 B is ignited by spark plug  162  and the resulting ignition creates a pressurized flame in cylinder  118 B which passes through passage  156  into cylinder  118 C to ignite the charge of compressed air and fuel mixture in cylinder  118 C. 
         [0077]    In accordance with the principles of the present invention, during the fuel saving cycle of a fuel saving mode, the injector  150 C associated the cylinder  118 C does not go through an injection cycle but injector  150 B does. Thus, when the pistons  120 B and  120 C reach the end of their simultaneous compression strokes, cylinder  118 B will have established therein a charge of compressed air and fuel mixture while cylinder  118 C will have established therein a charge of compressed air. 
         [0078]    When the charge of compressed air and fuel mixture in cylinder  118 B is ignited by spark plug  164 B, the high pressure conditions created as a result thereof are immediately communicated by means of passage  156  with the charge of compressed air in cylinder  118 C to raise the pressure acting on pistons  120 C during the simultaneous power drive stroke thereof with piston  120 B. 
         [0079]    Since the pistons  120 A and  120 D together are 180° out of phase with the pistons  120 B and  120 C together. The simultaneous power drive strokes of both pairs will fall within one rotation of the output shaft  124 . It will be remembered that the opposite duplicate bank is also 180° out of phase with the first bank so that the simultaneous power drive strokes of both duplicate pairs in the duplicate bank will occur within the other full rotation of the out put shaft  124  in each two rotational cycle. Thus, a pair of simultaneous power drive strokes will be applied to the shaft  124  during each half revolution thereof. In normal mode operation all of the power drive strokes will be of the same force. During the fuel saving mode of operation, the outer pair of pistons in each bank have equal power drive strokes equal to those of normal operation. However, the power drive stroke of the inner pair of each bank are powered by one half the fuel and go through twice the expansion. 
         [0080]    It should be noted that with spark ignition in normal mode operation, the time delay between the ignition in the first cylinder and the time the ignition of the first takes to ignite the second could move peak pressures in the second nearer the most efficient crank angle. 
         [0081]    It is also within the contemplation of the present invention to provide either a one bank or two bank internal combustion engine which operates at all items within the gas saving cycle of the present invention. 
         [0082]    Referring now more particularly to  FIG. 9A  there is shown therein a preferred embodiment of a computerized system for controlling the injectors  150  A-D associated with each bank of four piston and cylinder assemblies. To distinguish between the two banks, the injectors of bank 1 have the designation (1) added and the injectors of bank 2 have the designation (2) added. 
         [0083]    The system includes a computer  52  ( 1  &amp;  2 ) which receives electrical signals from a switch panel having three switches S( 1 ), S( 2 ), and S( 3 ). The three switches as shown are manually actuatable but it would be possible to actuate them in response to sensed conditions such as the vehicle going onto an upgrade, or the cruise control being activated and the like. 
         [0084]    With the three button panel as shown, when switch S( 1 ) is activated, the computer  52  ( 1  &amp;  2 ) is programmed to operate all of the injectors  150  A-D ( 1  &amp;  2 ) in properly timed relation. When all injectors are injecting fuels the engine  110  is operating at full power mode useful when the vehicle is on an upgrade or any time a burst of power is needed. It is noted that when in this mode, a double firming will occur during each stroke or 180° turn of the output shaft. 
         [0085]    When switch S( 2 ) is activated, the computer is programmed to inject fuel alternately to injectors  150  B( 1 ) and  150  C( 1 ) and alternatively to injectors  150  B( 2 ) and  150  C( 2 ) all in properly timed relation. Injectors  150  A ( 1  &amp;  2 ) and  150  D ( 1  &amp;  2 ) are allowed to inject fuel in normally timed relation to their respective cylinders. Depending upon whether the new crankshaft is configured to allow the two remaining cylinders of each bank to operate 180° out of phase with respect to one another or in phase with respect to another, the delivery of fuel by the respective injectors  150  A ( 1  &amp;  2 ) and  150  D ( 1 &amp;  2 ) will result in two double firmings out of phase with respect to one another and with respect to the firming of injectors  150  B ( 1  &amp; 2 ) and  150  C ( 1  &amp;  2 ). In this mode of operation two fuel injector jets of fuel are simply not injected during each cycle and yet all assemblies involved have a power stroke. On this basis, there are still two power strokes per 180° turn of the crankshaft with a saving of one quarter of the amount of fuel injected as compared with the full power mode. This mode is useful except when the full power mode is chosen or except when a full fuel saving mode is chosen by activating button S( 3 ). When switch button S( 3 ) is activated the computer  52  ( 1  and  2 ) is programmed to alternately activate either injectors  150  A( 1 ) and  150  A( 2 ) and injectors  150  D( 1 ) and  150  D( 2 ) or to alternately activate either injectors  150  A( 1 ) and  150  D( 1 ) and injectors  150  A( 2 ) and  150  D( 2 ) depending upon the configuration of the new crankshaft. In this full fuel saving mode two of the remaining four assemblies simply are not fed a supply of fuel with the pistons of the no fuel assemblies moving through their cycles. This “skipped” injection arrangement is well known per se. It is noted that the skipped cylinders are those that previously had entered into double firing either fully as in the full power mode or in conjunction with the fuel cutting of cylinders  150  B and  150  C. The result is an actual single injection and firing every stroke or 180° turn of the crankshaft even though the single injections with respect to the injectors  150  B and C results in double firings. 
         [0086]    Referring now to  FIG. 10  there is shown therein an engine  210  embodying the principles of the present invention which operates on a two stroke cycle rather than on a four stroke cycle. As shown similar parts have been given numbers with a leading  2  rather than the leading  1  as in  FIGS. 5-9  so that the description will be concerned only with the differences. 
         [0087]    First, the exhaust outlets  136  are changed to inlets designed by the numeral  282  with added letters A through D respectively. Thus outlet valves  142  A-D become inlet valves  254 A-D that are moved simultaneously with the inlet valves  240  A-D respectively. 
         [0088]    Second, the cylinders  220  are formed with a series of annularly spaced outlets, designated by the numeral  286  with added letters A through D respectively, as before, the inlets  232  and  282  communicate with a filtered air manifold (source not shown) and the outlets  286  communicate with a muffled exhaust manifold not shown. 
         [0089]    The four piston and cylinder assemblies of the engine  210  are provided with a different cam shaft  288  for controlling each assembly to go through a two stroke cycle of movement during each revolution of output shaft  224 . The rotational motion transmission assembly  145  is changed to effect this change as indicated at  290  so that the rotation of the cam shaft  288  is driven through one revolution during each rotation of the output shaft  224 . Each cycle includes a gaseous charge exchange portion which establishes that each piston has an appropriate charge of compressed gas therein either an air-fuel mixture or air without fuel mixed therein at the end of a first compression stroke. The charges of compressed air-fuel mixture are then ignited to begin a return power drive stroke at the end of which the gaseous charge exchange portion begins when the associated piston  220  moves below the outlets  286  and inlet valves  243  and  284  are opened. The gaseous charge exchange portion ends with the movement of the piston  220  upwardly beyond the outlets  286  after which the rest of the stroke is compression. 
         [0090]    The crank shaft  224  is the same as far as piston movements are concerned. The piston  220 B and  220 C move together while pistons  220 A and  220 D move together. With the cycle the same and thereof 180° out of phase with respect to simultaneous cycles of pistons  220 B and  220 C. 
         [0091]      FIG. 10  shows the position of the parts with the pistons at respective mid positions of movement corresponding to the middle of the power drive strokes of pistons  220 B and  220 C and the middle of the compressing strokes of piston  220 A and  220 D, with all valves closed. When the engine  210  with spark ignition is in a fuel saving mode, the two middle piston and cylinder assemblies B and C go through a gas exchange portion together but only cylinder  218 B receives a fuel charge during gas exchange so that at the end of the compression stroke cylinder  218 B has a charge of compressed air-fuel mixture therein while cylinder  218 C has a charge of compressed air therein. As before the ignition of the charge in cylinder  218 B is communicated through passage  256  to raise the air compression pressure in cylinder  218 C and effect the power drive stroke thereof together with the drive stroke of piston  220 B. 
         [0092]    The same cycle is carried out in cylinders  220 A and  220 D only 180° out of phase with respect to one another. The operation in normal mode operation is that both cylinders receive a charge of air-fuel mixture which are both ignited as before. The engine  210  has the advantage that a double power drive stroke is applied every half turn of the output shaft  224 . The fuel saving mode achieves the advantage previously noted. 
         [0093]    Referring now more particularly to Pinnacle type embodiment, there is shown in  FIGS. 11 and 12  an internal combustion engine partially in horizontal section which embodies the principles of the present invention. The engine is designated generally by the reference numeral  310 . Basically, the engine  310  includes Pinnacle engine components including first and second opposed piston and cylinder assemblies  312  and  314  and an added third opposed piston and cylinder assembly  316  disposed between the first and second assemblies  312  and  314 . 
         [0094]    The first and second opposed piston and cylinder assemblies  312  and  314  may be constructed in accordance with the aforesaid patent disclosures owned by Pinnacle. As such, each assembly  312  and  314  is carried by a frame assembly  318  and includes a pair of opposed pistons  320  and  322  and a further letter designation R or L depending on which is shown at the right (R) or left (L) in  FIG. 11 . Each piston  320  or  322  includes a further letter designation I for Inlet or E for Exhaust. The pistons  320  are slidably mounted in a cylinder section designated by the numeral  324  with a further similar letter designation and the pistons  322  are slidably mounted in a cylinder section designated by the numeral  326  with a further similar letter designation. 
         [0095]    Cylinder sections  324  and  326  constitute valve elements which are each mounted in a fixed main frame section  328  of the frame assembly  318  for cooperating reciprocating movement with respect to a swirl control valve structure, generally indicated at  330 . Each swirl control structure  330  is disposed between the associated cylinder sections  324  and  326  and extends outwardly therefrom in fixed relation to the main frame section  328 . 
         [0096]    Each swirl control valve structure  330 R or  330 L has interior surfaces which provide valve seats and define the exterior of a centrally located combustion chamber  332 R or  332 L which communicates with the interior of the associated cylinder sections  324 R and  326 R or  324 L and  326 L. Each swirl control valve structure  330 R or  330 L also provides an inlet  334 R or  334 L which leads to the combustion chamber  332 R or  332 L and is opened thereto or closed there from by the position of reciprocating movement of the associated cylinder section  324 RI or  324 LI and an outlet  336 R or  336 L which leads from the combustion chamber  332 R or  332 L and is opened there to or closed there from by the position of reciprocating movement of the associated cylinder section  326 RE or  326 LE. 
         [0097]    In accordance with the teachings of the aforesaid Pinnacle Pat Appln Pubs, each swirl control valve structure  330  also includes air and fuel supply valving (not shown in the drawings) capable of establishing an air-fuel mixture of a controlled fuel richness or leanness in a swirl formation to the combustion chamber  332 R or  332 L in timed relation to the cyclical movement of the pistons  320  and  322  within their respective cylinder section  324  and  326 . The pistons  320  and  322  are cyclically moved within their respective cylinder sections  324  and  326  by means of opposed crankshafts  338  and  340 , each having a pair of axially spaced similarly radially directed crank portions  342 . One end of a connecting rod  344  is pivoted to each crank portion  342  the opposite end of which is pivoted to an associated piston  320  or  322 . 
         [0098]    The opposed crankshaft and connecting rod arrangement has the effect of moving the pistons  320  and  322  within their respective cylinder sections  324  and  326  toward and away from each other and toward and away from the associated centrally located combustion chamber  332 . 
         [0099]    The timing of the cyclical movements of the pistons  320  and  322  is related to the reciprocating movements of the cylindrical sections  324  and  326  by a camshaft assembly (not shown) suitably driven by the crankshaft rotation and constructed in accordance with the aforesaid Pinnacle Pat. Appln. Pubs. The components which transmit the rotational movement of the camshaft assembly to the reciprocating movements of the cylinder sections are not shown in the drawings except for a flange portion  346  on the exterior of each cylinder section  324  and  326  by which each cylinder section  324  and  326  is reciprocatingly moved. 
         [0100]    The timing establishes a conventional four stroke cycle for each assembly  312  and  314  which are essentially 180° out of phase with respect to one another. Each four stroke cycle includes the usual intake stroke where the pistons  320  and  322  move apart to take into the cylinder volume between the pistons  320  and  322  a charge of air fuel mixture provided by the associated swirl control valve structure  332  with a cylinder section  324  opening an inlet  334 . After the pistons  320  and  322  reach a limiting position apart, the inlet is closed by movement of the cylinder section  324  and they begin a movement toward one another through a compression stroke into a limiting position in closely spaced relation to one another wherein the air-fuel mixture is compressed within the combustion chamber  332  to a compression pressure. In appropriately timed relation toward the end of the compression stroke, a spark plug  348 , provided by the associated swirl control valve structure  330 , is energized to ignite the air fuel mixture. The increased pressure conditions of the ignition drive the pistons  320  and  322  away from each other through a power stroke. The cycle is completed by a movement of the pistons  320  and  322  toward each other through an exhaust stroke during which the associated cylinder section  326  opens the outlet  336  provided by the swirl control valve structure  330 . Each stroke of the cycle is accomplished during one half of one revolution of the crankshafts  338  and  340 , with each cycle taking place in two revolutions of the crankshafts  338  and  340 . The four consequative events that take place in four consequative strokes are accomplished by the camshaft assembly which is geared to rotate at half the rotational speed of the crankshaft  338  or  340 . 
         [0101]    In accordance with the disclosure of the cited Pinnacle Pat. Appln. Pubs., the assemblies  312  and  314  are constructed so that the compression ratio of each can be varied, which varies the compression pressure in the combustion chamber  332  at the end of each compression stroke of the assembly  312  or  314 . This variation is accomplished by connecting the crankshafts  338  and  340  rotationally together by a gear train  350  and mounting the crankshaft  340  on a frame assembly subframe  352  pivotally mounted on the main frame assembly  318 . 
         [0102]    Referring now more particularly to  FIG. 13 , the gear train  350  includes a first gear  354  fixed to the crankshaft  338  which, in turn, is journaled on the main frame assembly  318  for rotation about a fixed axis of rotation. The first gear  354  meshes with a second gear  356  suitably journaled on the main frame assembly  318  for rotational movement about a fixed axis. The second gear  355  is preferably double the size of first gear  354  and meshes with it and with a third gear  358  of the gear train  346  of the same size. Third gear  358  is suitably journaled on the main framed assembly  318  for rotational movement about a fixed axis of rotation. 
         [0103]    The gear train  350  includes a fourth and final gear  360  which meshes with third gear  358  and is fixed to the crankshaft  340 . The crankshaft  340  is mounted on the subframe  352  of the main frame assembly  318  which is pivotally mounted for pivotal movement about the rotational axis of movement of the third gear  358 . When the subframe  352  is moved about its pivotally axis by an activator  362 , shown in block diagram in  FIG. 14 , the compression ratio of the first and second opposed piston and cylinder assemblies  312  and  314  can be varied. 
         [0104]    As best shown in  FIGS. 11 and 12 , the third opposed piston and cylinder assembly  316  includes a pair of opposed pistons  364  and  366  mounted for movement toward and away from each other within a cylinder  368  fixedly mounted on the frame section  328  between the spaced assemblies  312  and  314 . The pistons  364  and  336  are moved by the crankshafts  338  and  340  respectively by means of connecting rods  370  and  372  each having one end pivoted to the associated piston  364  or  366  and an opposite end to a central crank portion  372  or  376  on the respective crankshaft  338  or  340 . 
         [0105]    The cylinder  368  has spaced inlet and outlet openings  378  and  380  ( FIG. 14 ) formed in the wall thereof which are valved by the passage of the pistons  364  and  366  there over. When the inlet opening  378  is connected with a source of air-fuel mixture, as shown in  FIG. 14 , the third assembly can operate as a two stroke engine. 
         [0106]    As best shown in  FIGS. 11 and 12 , in accordance with the principles of the present invention, the combustion chamber  332  of each assembly  312  and  314  is communicated with central piston defined combustion chamber of the assembly  316 . As shown the communication is accomplished by passages  382  R and  382  L extending from each combustion chamber  332 , through the associated swirl valve control structure  330  to the center of cylinder  332  by means of an opening  383  therein. Each passage  382  R or  382 L is provided with a check valve  384 R or  384 L respectively which allow gas pressure to flow from the assemblies  312  and  314  to the assembly  316  while preventing gas flow in the opposite direction. 
         [0107]    Referring now more particularly to  FIG. 14 , there is shown therein a block diagram of a computer controlled system for an automobile driven by the engine  310 . The system includes a computer  386  powered by the car battery (not shown). The computer  386  receives signals sensed by a knock sensor  388  for each assembly  312  and  314 . The computer  386  also receives signals from other sensors indicated by block diagram  390 . Such sensors may include ignition key on and off, output shaft rotational speed, wheel rotational speed, gas and brake pedal movements and the like. 
         [0108]    In accordance with the teaching of the aforesaid Pinnacle Pat. Appln. Pubs., the system includes a combustion chamber size-varying activator  392  under the control of computer  386  which controls the movement of the combustion size varying structure  350 - 352  and a swirl valve control activator  394  which controls the swirl valve control structure  330 . These components function in the dual manner disclosed in the cited Pinnacle Pat. Appln. Pubs. Specifically, US 2011/0220058 discloses two modes of operation. The first mode is a power mode for medium to high loads and the second is an efficiency mode for low to medium loads. The activators  392  and  394  control the combustion size varying structure  350 - 352  and the swirl valve control structures  330  to feed a lean air-fuel mixture under low compression in the efficiency mode, which mixture is made richer under high compression pressures for more power in the power mode. These pinnacle components of the system can also use ignition timing to allow the first and second modes to be at the same air-fuel mixture. 
         [0109]    The components of the system which are added in accordance with the principles of the present invention include a pressurized air assembly valve  396  with its activator  398  and a pressurized fuel injector  3100  with its activator  3102 . These components operate in known conventional fashion to normally deliver a variably determined amount of mixed air and fuel to the inlet opening  378  of the assembly  316  at the start of the inlet stroke of the pistons  364  and  366 . 
         [0110]    Since the air-fuel mixture initially delivered to assembly  316  is at a pressure greater than the pressure of the air fuel mixture initially delivered to the assemblies  312  and  314 , gas pressure flow passed the check valves  384  from the combustion chambers of the assemblies  312  and  314  to the combustion chamber of the assembly  316  will not occur until firing occurs in the assemblies  312  and  314  and no firing occurs in the combustion chamber of the assembly  316 . 
         [0111]    The no firing condition within the assembly  316  is accomplished by the activator  3102  of the pressurized fuel injector  3100 . The present invention contemplates operating in either one of two computer controls of the activator  3102 . The first is that the injector  3100  is activated to supply fuel when the Pinnacle components are in the second mode and to cut off the supply of fuel from the injector  3100  when the Pinnacle components are in the first mode. The second is that the injector  3100  is activated to cut off the supply of fuel during both the first and second modes of the Pinnacle components and is activated to supply fuel only in response to a different signal such as an uphill sensing switch actuation or a switch actuation in response to a floor boarding of the gas pedal. 
         [0112]    In the first instance there will be no firing in the combustion chamber of the assembly  316  when the Pinnacle components are operating in the first mode, however, because the four stroke cycles of assemblies  312  and  314  are 180° out of phase with respect to one another, one of the assemblies  312  or  314  is fired simultaneously to each firing stroke of the assembly  316  and the increased pressure conditions resulting from the alternate firings in assemblies  312  and  314  will be communicated through passages  382  passed check valves  384  to the combustion chamber of the assembly  316  to add to the air compression pressure therein and drive the pistons through their power strokes simultaneously with the corresponding drive stroke of the assembly  312  or  314 . 
         [0113]    In the first instance when the Pinnacle components are operating in the second mode, the combustion chamber of the assembly  316  will contain a compressed air-fuel charge simultaneous with one of the assemblies  312  and  314 . The firing of the air-fuel charge in the combustion chamber of the assembly  312  or  314  is utilized to ignite the air-fuel charge in the assembly  316  by fire passing through the associated passage  382  beyond the associated check valve  384 . 
         [0114]    In the second instance, when the Pinnacle components are in either first or second mode, the assembly  316  with cut off fuel operates to provide added working expansion for the alternate firing of the assemblies  312  and  314 . When fuel is fed to the assembly  316  its power strokes are simply added to the alternate power strokes of the assemblies  312  and  314 . 
         [0115]    The first instance has the advantage that the first mode of the Pinnacle components is made more efficient while the second mode is made more powerful. The second instance has the advantage that both the first and second modes of the Pinnacle components are made more efficient and power can be added only when needed. 
         [0116]    When the two stroke assembly  316  is operating with fuel it will be fired once each revolution of the crankshafts, whereas the two four stroke assemblies  312  and  314  provide one firing each revolution between them. The result is that at maximum power in the power mode there will be four jets of fuel during a cycle of two revolutions of the crankshafts  338  and  340  and at maximum efficiency in the fuel saving mode half of the fuel injected at maximum power is saved by never being injected. Moreover, it is to be noted, that even when the fuel is cut off, all of the components of the engine  310  are operating and functioning to achieve the efficiency or power boost results. 
         [0117]    It is within the contemplation of the present invention to provide an added third assembly  316  which is never fired and simply functions as an efficiency booster for the other two assemblies  312  and  314 . 
         [0118]    It is noted that in either of the two instances described above, the firing during four consequative strokes will be 2 fires, no fires, 2 fires, no fires. Thus while balanced, there is lacking the usual completely balanced firing of one fire per stroke. 
         [0119]    The engine  310  can be made to fire completely balanced by two fires each stroke by adding three more piston and cylinder assemblies. When added, the three new piston and cylinder assemblies are operated 180° out of phase with respect to the first three piston and cylinder assemblies. 
         [0120]      FIG. 15  schematically illustrates a modified engine  310   1  wherein like added parts are designated by the same reference characters with an added 1 (prime). As shown in  FIG. 15 , when the three new added assemblies  312   1 ,  314   1  and  316   1  are placed in opposed relation to the original three assemblies  312 ,  314  and  316  the added three assemblies  312   1 ,  314   1  and  316   1  are automatically made to move 180° out of phase with the original assemblies  312 ,  314  and  316 , this movement by virtue of having one set of pistons  322   1  and  364   1  being moved by the crankshaft  338  which moves one set of pistons  322  and  364  of the original three assemblies  312 ,  314 ,  316 . 
         [0121]      FIG. 16  schematically illustrates a modified engine  1   310  wherein like added parts are designated by the same reference characters with a prime added in the front of the numeral.  FIG. 6  schematically shows the three added piston and cylinder assemblies  1   312 ,  1   314 , and  1   316  in an inline relationship with respect to the first three assemblies  312 ,  314  and  316 . It will be noted that the crankshafts  1   338  and  1   340  are integral with respect to the crankshafts  338  and  340  and configured to be 180° out of phase with respect thereto. 
         [0122]    The reference herein to a computer, programming, or software may be substituted by any type of controller, including those where the functionality is provided in circuitry with or without the use of software. 
         [0123]    The foregoing embodiments have been provided solely to illustrate the structural and functional principles of the present invention, and are not intended to be limiting. To the contrary, the present application is intended to encompass all modifications, substitutions, and alterations within the spirit and scope of the appended claims.