Abstract:
A free piston drive combustion engine is provided wherein the piston are reciprocated by the force of combustion in combination with its compressed exhaust gases. A compressed air fuel mixture is ignited in the combustion chamber exploding driving a piston backward, while expelling a blast of exploding gases into an open area in the side of a turbine wheel, forcing it to rotating in a rotary motion. The compressed exhaust gases is carry within the turbine wheel, then expelling the exhaust gases into the bottom of engine and driving the piston forward. The compressed exhaust gases closes a door onto an opening in the combustion chamber and with the forward movement of the piston this would compressed air fuel mixture, therefore commence the combustion-exhaust cycle thereat. Before any exhaust is expel from the engine, it help to drive piston forward and help to closed door onto combustion chamber opening therefore helping compressing incoming air fuel mixture.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
   Not applicable. 
   REFERENCE TO MICROFICHE APPENDIX 
   Not applicable. 
   CROSS REFERENCE TO RELATED APPLICATIONS 
   Dainton device (U.S. Pat. No. 1,802,881 issued April 1931). 
   Benoit device (U.S. Pat. No. 3,068,639 issued September 1961). 
   Pais device (U.S. Pat. No. 3,757,515 issued September 1973). 
   Wallis device (U.S. Pat. No. 3,978,827 issued September 1976). 
   Heaton device (U.S. Pat. No. 4,344,288 issued August 1982). 
   Benaroya device (U.S. Pat. No. 4,403,577 issued September 1983). 
   Southard device (U.S. Pat. No. 4,733,534 issued March 1988). 
   Heaton device (U.S. Pat. No. 4,449,488 issued May 1984). 
   David device (U.S. Pat. No. 4,561,252 issued December 1985). 
   Chaneac device (U.S. Pat. No. 4,848,282 issued July 1989). 
   Hammett device (U.S. Pat. No. 4,920,928 issued May 1990). 
   Wilson device (U.S. Pat. No. 4,951,618 issued August 1990). 
   Han device (U.S. Pat. No. 5,036,667 issued August 1991). 
   Han device (U.S. Pat. No. 5,678,522 issued October 1997). 
   Bailey device (U.S. Pat. No. 6,205,961 issued March 2001). 
   Valentin device (U.S. Pat. No. 6,293,231 issued September 2001). 
   Young device (U.S. Pat. No. 6,408,717 issued June 2002). 
   Nagel device (U.S. Pat. No. 6,449,940 issued September 2002). 
   Morikami device (U.S. Pat. No. 6,450,846 issued September 2002). 
   STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT 
   Not applicable. 
   REFERENCE TO SEQUENCE LISTING, A TABLE, OR A COMPUTER PROGRAM LISTING APPENDIX 
   Not applicable. 
   BACKGROUND OF INVENTION 
   
       
       1. This Invention relates generally to the free-piston type internal combustion engine that is connected to a turbine wheel. Particular to innovations which improve controllability and efficiency of the free-piston engine by using a turbine wheel. Using a turbine wheel along with a free moving piston, this will reduce toxic emissions, weight and size of such engines. 
       2. Turbine wheel is a rotation wheel used to minimize variations in angular velocity and revolutions per minute. Using a combustion chamber along with a turbine wheel in the use of fuel or propellant that is initiated and controlled would transmit power to the turbine wheel. This would take advantage of bypassing the use of having a crankshaft. 
       3. There is an advantageous application, by using a turbine wheel along with its combustion gases in transmitting energy. Simple concept of free-piston internal combustion engines is transferring combustion energy direct into mechanical energy. 
       4. Invention is directed to an internal combustion engine, which is well known. There are engines with a combustion chamber that are with its piston and rod rigidly attached to the crankshaft. Free-piston engine moves freely and independently of main shaft of the engine. Advantages of a free-piston engine that its piston not being rigidly attached to a crankshaft connected by a rod. 
       5. Free-piston internal-combustion engines having a cylinder and one or more reciprocation pistons therein. One piston at least of which is movable freely and independently of the main shaft. Engine on the stroke of such piston immediately following ignition of the charge. Burned gases during which stroke the energy is stored. Energy is thereafter transferred to main shaft of the engine. Energy is ordinarily stored by forcing piston against pressure of the atmosphere. Therefor stored energy is ordinarily transferred to the main shaft by securing piston thereto by means of a suitable clutch. Such energy provided with suitable converting mechanism upon its return stroke. 
       6. Cylinder of an internal-combustion engine is closed at one end by a plate called a head and open at the other end. Permitting free oscillation of the connection rod, which joins piston to crankshaft. 
       7. Internal-combustion engine, fuel-air mixture is burned in the engine proper. Hot gaseous products of combustion act directly on the surfaces of its moving parts, such as those of pistons. 
       8. Turbine wheel is a wheel attached to a rotating shaft, which the kinetic energy of a moving exhaust gases is converted to mechanical power by the impulse or reaction of the gases with a series of notch or fagged cut arrayed about the circumference of the turbine wheel. 
       9. Turbine wheel is a wheel smoothing out delivery of power from a motor to a machine. Inertia of the turbine wheel opposes and moderates fluctuations in speed of engine. Turbine wheel stores the excess energy for intermittent use and smoothes out pulses of energy provided by combustion. 
     
  
   BRIEF SUMMARY OF THE INVENTION 
   The present invention substantially departs from conventional concepts and designs of prior art. Providing for a flywheel combustion engine  10 , utilizing a combustion chamber  28  mounted around the periphery of a turbine wheel  20 , enclosed within said flywheel combustion engine  10 , with said combustion chamber  28  communicating at the combustion and thereof with said turbine wheel  20 . A cylinder  58  utilizing said combustion chamber  28 , a upper piston  60 , a lower piston  68  with a rod  66  connecting said pistons  60 ,  68  with a cylinder in-between area  78  between said pistons  60 ,  68 , axially slid ably mounted therein, to reciprocate between the combustion end and gas exhaust flow end of said cylinder  58 . A upper engine open area  12  utilizing a head door  46  in proximity periphery with said turbine wheel  20 , with a turbine wheel open area  24  receiving exploding gases within said combustion chamber  28 , therefore said exploding gases expelling and compressed into said turbine wheel open area  24 , concurrently rotating said turbine wheel  20 . 
   With said pistons  60 ,  68  advancing forward toward said combustion chamber  28  within said cylinder  58 , and feeding air-fuel mixture into said combustion chamber  28  at the combustion end thereof. Compressing and Igniting said mixture to drive said pistons  60 ,  68  backward toward a cylinder bottom area  80 , with said exploding gases expelling toward said head door  46  end of said combustion chamber  28 . With said exploding gases therefore opening said head door  46  and expelling said exploding gases into said upper engine open area  12 , and against said turbine wheel  20 . Said exploding gases pushes open said head door  46  by said exploding gases, sequence driving of said turbine wheel  20  in a rotary motion. 
   Said exploding gases expelling into said turbine wheel open area  24 , from said upper engine open area  12  therefore concurrently rotating said turbine wheel  20  in a rotary motion. 
   Said exploding gases now would be turning into compressed exhaust gases. Said turbine wheel open area  24  in a rotary motion with said compressed exhaust gases within expelling into a lower engine area  18 , then said compressed exhaust gases expelling into a door ba-line  52  within said head door  46 . Said compressed exhaust gases expelling out said door ba-line  52 , then said compressed exhaust gases expelling into said upper engine open area  12 , bushing and closing said head door  46  on top of a combustion chamber outlet opening  34 , of said combustion chamber  28 . 
   Said exploding gases pushing said pistons  60 ,  68  downward toward said lower engine area  18 , this would be helping closing said head door  46  by pushing some of said compressed exhaust gases in said lower engine area  18  into a head door aa-line  38 , than pushing said expelling compressed exhaust gases into said door ba-line  52 , then pushing said compressed exhaust gases out into said upper engine open area  12 , therefore said compressed exhaust gases would be helping to close said head door  46 . 
   Said compressed exhaust gases within said lower engine area  18  expelling into said cylinder bottom area  80 , pushing of said pistons  60 ,  68  forward movement toward said combustion chamber  28 , then expelling said compressed exhaust gases into a bore inlet opening  86 , then expelling said compressed exhaust gases a bore line  88 , then expelling said compressed exhaust gases into said cylinder in-between area  78 . Said pistons  60 ,  68  forward movements open up a bore outlet opening  90 . 
   At the same time said bore inlet opening  86  is opening up into said bore line  88 , also opening said bore outlet opening  90  into said cylinder in-between area  78 , at the same time closing off a exhaust line inlet opening  92  of said a exhaust line  94 . 
   Said backward movement of said pistons  60 ,  68  toward said lower engine area  18 , closing off said bore line  88  and said bore outlet opening  90 , therefore opening up said exhaust line  94  within said cylinder in-between area  78 , than said compressed exhaust gases expelling into said exhaust line  94 , then expelling out a exhaust line outlet opening  96  commencing said combustion exhaust cycle thereat. Provided an automatic cycle, self timing, exhaust piston drive, said flywheel combustion engine  10 , and more fully described the here-in after. 
   Further objects and advantages of my invention will become apparent. The drawing and ensuring description will become apparent. 

   
     BRIEF DESCRIPTION OF THE DRAWING 
     This invention relates to apparatus and methods. 
       FIG. 1  is a perspective view of flywheel combustion engine. This is in accordance with principles of the present invention. 
       FIG. 2  is a perspective view of Turbine wheel. This is in accordance with principles of the present invention. 
       FIG. 3  is a perspective view of Combustion Chamber, Upper Engine Open Area, Head Door, Head Door Open Area. This is in accordance with principles of the present invention. 
       FIG. 4  is a perspective view of Lower Engine Area. This is in accordance with principles of the present invention. 
       FIG. 5  is a perspective view of Cylinder, Head door aa-line, bore Line, Exhaust Line This is in accordance with principles of the present invention. 
       FIG. 6  is a perspective side view of flywheel combustion engine. This is in accordance with principles of the present invention. 
   

   REFERENCE NUMERALS IN DRAWINGS 
   
       
         10  flywheel combustion engine 
         12  upper engine open area 
         14  upper engine open area outlet opening 
         16  lower engine inlet opening 
         18  lower engine area 
         20  turbine wheel 
         22  turbine wheel inlet-outlet opening 
         24  turbine wheel open area 
         26  turbine wheel outer edge 
         28  combustion chamber 
         30  injector 
         32  spark plug 
         34  combustion chamber outlet opening 
         36  top bore outlet opening 
         38  head door aa-line 
         40  head door line inlet ab-opening 
         42  head door line outlet ac-opening 
         44  head door open area 
         46  head door 
         48  top side of head door 
         50  bottom side of head door 
         52  door ba-line 
         54  door line inlet bb-opening 
         56  door line outlet bc-opening 
         58  cylinder 
         60  upper piston 
         62  top side of upper piston 
         64  bottom side of upper piston 
         66  rod 
         68  lower piston 
         70  top side of lower piston 
         72  bottom side of lower piston 
         74  lwer cylinder in let-outlet opening 
         76  top bore area 
         78  cylinder in-between area 
         80  cylinder bottom area 
         82  lower side of combustion chamber 
         84  lower side of cylinder 
         86  bore inlet opening 
         88  bore line 
         90  bore outlet opening 
         92  exhaust line inlet opening 
         94  exhaust line 
         96  exhaust line outlet opening 
         98  metal ca-ring 
         100  metal cb-ring 
         102  drive shaft 
         104  means of controlling head door. 
     
  
   DETAILED DESCRIPTION 
   Flywheel Combustion Engine 
   The present description provides for said flywheel combustion engine  10  having said combustion chamber  28  mounted at the periphery of said turbine wheel  20  and enclosed within said flywheel combustion engine  10 . Enclosed within said flywheel combustion engine  10  utilizing member including said cylinder  58 , said upper engine open area  12 , said turbine wheel  20 , said lower engine area  18 , said head door aa-line  38 , said bore line  88 . Said exhaust line  94  mounted on said cylinder  58  on said flywheel combustion engine  10 . A sensor not shown mounted on said flywheel combustion engine  10 . 
   Cylinder 
   Enclosed within said flywheel combustion engine  10 , said cylinder  58 , utilizing member including said combustion chamber  28 , a injector  30 , a spark plug  32 , a top bore outlet opening  36  that is an opening into said combustion chamber  28  from a top bore area  76 , said upper piston  60 , said rod  66 , said lower piston  68 , said top bore area  76 , said cylinder in-between area  78 , said cylinder bottom area  80 , said combustion chamber outlet opening  34  that is an opening into said upper engine open area  12  from said combustion chamber  28 , a lower cylinder inlet-outlet opening  74  that is an opening into said lower engine area  18  from said cylinder bottom area  80  and being the same opening into said cylinder bottom area  80  from said lower engine area  18 , said bore inlet opening  86  that is an opening into said bore line  88  from said cylinder bottom area  80 , said bore outlet opening  90  that is an opening into said cylinder in-between area  78  from said bore line  88 . Said top bore area  76  being a lower side of combustion chamber  82  this being at top side of said top bore area  76 . Said cylinder bottom area  80  being a lower side of cylinder  84  this being at bottom side of said cylinder bottom area  80 . Said upper piston  60  with a top side of upper piston  62  as this is being the top side of said upper piston  60 . Said upper piston  60  with a bottom side of upper piston  64  this is being the bottom side of said upper piston  60 . Said lower piston  68  with a top side of lower piston  70  this is being the top side of said lower piston  68 . Said lower piston  68  with a bottom side of lower piston  72  this is being the bottom side of said lower piston  68 . Said exhaust line  94  mounted on said cylinder  58  with said exhaust line inlet opening  92  being connected within said cylinder in-between area  78 . Said upper piston  60  has a metal ca-ring  98  fitting around said upper piston  60 . Said lower piston  68  has a metal cb-ring  100  fitting around said lower piston  68 . Said injector  30  mounted on said cylinder  58  with said injector  30  being connected to said combustion chamber  28 . A electrical fuel pumping means not shown mounted on said cylinder  58  with said electrical fuel pumping means not shown being connected to said combustion chamber  28 . Said spark plug  32  mounted on said cylinder  58  with said spark plug  32  being connected to said combustion chamber  28 . Said combustion chamber  28  utilizing said injector  30 , said spark plug  32 , said electrical fuel pumping means not shown. 
   Said combustion chamber  28  mounted at periphery of said upper engine open area  12 , lying next to said head door  46  as closed, said head door  46  as open would be inside said upper engine open area  12 . Said combustion chamber  28  that being the space between the opening of said combustion chamber outlet opening  34  and said top bore outlet opening  36 . Said top bore area  76  that is the space between said top side of upper piston  62  as said pistons  60 ,  68  move forwards or backwards and said top bore outlet opening  36 . Said cylinder in-between area  78  that being the space between the bottom side of upper piston  64  and the top side of lower piston  70  as the pistons  60 ,  68  move forwards or backwards. The cylinder bottom area  80  being space between the bottom side of lower piston  72  as the pistons  60 ,  68  move forwards or backwards and the lower cylinder inlet-outlet opening  74 . The combustion chamber outlet opening  34  that being the opening between said upper engine open area  12  and the combustion chamber  28 . Said top bore outlet opening  36  an opening between said combustion chamber  28  and said top bore area  76 . Said pistons  60 ,  68  move forwards or backwards within said cylinder  58  being said top bore outlet opening  36  at the top forward movement to said lower cylinder inlet-outlet opening  74  at the bottom backward movement. Said top side of upper piston  62  of said upper piston  60  would be within said top bore area  76 . Said bottom side of upper piston  64  of said upper piston  60  would be within said cylinder in-between area  78  between. Said top side of lower piston  70  of said lower piston  68  would be within said cylinder in-between area  78  between. Said bottom side of lower piston  72  of said lower piston  68  would be within said cylinder bottom area  80 . The rod  66  connected to the upper piston  60  and the lower piston  68 , with the rod  66  connecting the pistons  60 ,  68  within the cylinder in-between area  78 . Said bore outlet opening  90  that is the opening from said bore line  88 . Said cylinder in-between area  78  that area between said pistons  60 ,  68  with said bore outlet opening  90 , and said exhaust line inlet opening  92 , within said cylinder in-between area  78 . Said exhaust line inlet opening  92  that is the opening into said exhaust line  94 . 
   Said exhaust line inlet opening  92  that is the opening between said cylinder in-between area  78  and said exhaust line  94 . 
   Said bore inlet opening  86  that is the opening into said bore line  88 . Said bore inlet opening  86  that is the opening between said cylinder bottom area  80  and said bore line  88 . 
   Said pistons  60 ,  68 , axially slid ably mounted therein, to reciprocate between the said combustion chamber  28  end and said cylinder bottom area  80  end within said cylinder  58 . Said upper piston  60  having adjustable split said metal ca-ring  98  fitting around said upper piston  60 , for stopping exploding gases entering said cylinder in-between area  78 . Said lower piston  68  having adjustable split said metal cb-ring  100  fitting around said lower piston  68 , for stopping compressed exhaust gases entering said cylinder in-between area  78 . Said combustion chamber  28  utilizing said injector  30  would be admitting air-fuel into said combustion chamber  28 . Said spark plug  32  threaded into said combustion chamber  28  delivers a spark igniting the mix. Said injector  30  with said electrical fuel pumping means not shown receives a signal from said sensor not shown measuring the inwardness of said turbine wheel  20  as rotating to determine the point for fuel pumping through said injector  30 . Air-fuel inside said combustion chamber  28  explodes into exploding gases. With said head door  46  as closed and as said pistons  60 ,  68  forward movements toward said upper engine open area  12  within said combustion chamber  28 , compressing said incoming air-fuel mix within said combustion chamber  28 . 
   Said exploding gases within said combustion chamber  28 , would then expel said exploding gases into said upper engine open area  12  from said combustion chamber  28 , would then expel said exploding gases into said turbine wheel open area  24  concurrently rotating said turbine wheel  20 . Said exploding gases now would be turning into compressed exhaust gases. Said compressed exhaust gases expelling into said upper engine open area  12  from said combustion chamber  28 , then would expel said exploding gases into said turbine wheel open area  24  therefore concurrently rotating the already rotating said turbine wheel  20 . 
   Said exploding gases expelling into said turbine wheel open area  24  from said upper engine open area  12 , with the concurrently rotating said turbine wheel  20 , now becoming compressed exhaust gases, then expelling said compressed exhaust gases into said lower engine area  18 . Said compressed exhaust gases within said lower engine area  18 , from said turbine wheel open area  24  that is concurrently rotating, would expel said compressed exhaust gases into said cylinder bottom area  80 . Some of said compressed exhaust gases within said lower engine area  18  would expel into said cylinder bottom area  80  and some of said compressed exhaust gases would expel into said head door aa-line  38 . Some of said compressed exhaust gases that expel into said cylinder bottom area  80 , that is now pushing said pistons  60 ,  68  upward toward said combustion chamber  28 . As said bore inlet opening  86  of said bore line  88  open up, by the forward movement of said pistons  60 ,  68 , expelling said compressed exhaust gases into said bore line  88 , would then expel said compressed exhaust gases into said bore outlet opening  90 , would then expel said compressed exhaust gases into said cylinder in-between area  78 . 
   Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86  of said bore line  88  within said cylinder bottom area  80  expelling said compressed exhaust gases into said bore line  88 . Forward movement of said pistons  60 ,  68  opens said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78 , and closes said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 , would then expel said compressed exhaust gases into said cylinder in-between area  78 . 
   Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86  and opens said bore outlet opening  90  of said bore line  88 . Forward movement of said pistons  60 ,  68  closes said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 . 
   Backward movement of said pistons  60 ,  68  toward said lower engine area  18 , closes said bore inlet opening  86  of said bore line  88  within said cylinder bottom area  80  stopping said compressed exhaust gases from entering said bore line  88 . Backward movement of said pistons  60 ,  68  closes said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78  and opens said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 , would be expelling said compressed exhaust gases into said exhaust line  94 . Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86  and opens said bore outlet opening  90  of said bore line  88 . Backward movement of said pistons  60 ,  68  opens said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 . 
   Said compressed exhaust gases within said cylinder bottom area  80 , expelling said compressed exhaust gases into said lower cylinder inlet-outlet opening  74  on the backward movement of said pistons  60 ,  68  toward said lower engine area  18 , pushing said compressed exhaust gases into said lower engine area  18 . 
   Upper Engine Open Area 
   Enclosed within said flywheel combustion engine  10 , said upper engine open area  12 , utilizing member including a upper engine open area outlet opening  14  that is an opening into said upper engine open area  12  and meeting with opening of the rotating a turbine wheel inlet-outlet opening  22  meeting said upper engine open area  12 , said combustion chamber outlet opening  34  that is a opening into said combustion chamber  28  from said upper engine open area  12 , said head door  46  would have part of lying within said upper engine open area  12  and would have part of lying within a head door open area  44 , said head door  46  having a top side of head door  48  being at top side of said head door  46 , said head door  46  having a bottom side of head door  50  being at bottom side of said head door  46 , said door ba-line  52  having a door line inlet bb-opening  54  that is a opening into said door ba-line  52  lying within said head door open area  44 , said door ba-line  52  having a door line outlet bc-opening  56  that is a opening into said upper engine open area  12 , a means of controlling head door  104  that is lying between said upper engine open area  12  and said head door open area  44 . 
   Said upper engine open area  12  mounted at periphery of said combustion chamber  28  and said turbine wheel  20 . The upper engine open area  12  that being the space between the combustion chamber outlet opening  34  and the upper engine open area outlet opening  14 . Said combustion chamber outlet opening  34  would be an opening into said combustion chamber  28 , from said upper engine open area  12 . Said combustion chamber outlet opening  34  would be an opening between said upper engine open area  12 , and said combustion chamber  28 . 
   Said head door  46  having said top side of head door  48  being at top side of said head door  46 , within said upper engine open area  12 . Said head door  46  having said bottom side of head door  50  being at bottom side of said head door  46 , within said upper engine open area  12  as open. Said head door  46  having said bottom side of head door  50  being at bottom side of said head door  46 , lying next to and on top of said combustion chamber outlet opening  34  as closed. Said head door  46  having said door ba-line  52 , lying within said head door  46  and being an open line between said head door open area  44 , and said upper engine open area  12 . Said head door  46  having said door line inlet bb-opening  54 , this is a inlet opening into said door ba-line  52  from said head door open area  44 . Said head door  46  having said door line outlet bc-opening  56 , this is a outlet opening from said door ba-line  52 , into said upper engine open area  12 . Said part of said head door  46  within said upper engine open area  12 , would have said door line outlet bc-opening  56 . Said part of said head door  46  within said head door open area  44 , would have said door line inlet bb-opening  54 . Said means of controlling head door  104  this is a means for having movement of said head door  46  within said upper engine open area  12  and for having movement of said head door  46  within said head door open area  44 . 
   Said means of controlling head door  104  between said upper engine open area  12 , and said head door open area  44 , with having part of said head door  46  within said upper engine open area  12  and with having part of said head door  46  within said head door open area  44 . The means of controlling head door  104  also used for stopping said compressed exhaust gases from entering into the upper engine open area  12  or entering into the head door open area  44 , except into the door line inlet bb-opening  54 . Said means of controlling head door  104 , this would be a means for having movement of said head door  46  within said upper engine open area  12  also have movement of said head door  46  within said head door open area  44 . Said head door  46  having said top side of head door  48 , being at top side of said head door  46 . Said head door  46  having said bottom side of head door  50 , being at bottom side of said head door  46 . The upper engine open area outlet opening  14  being the opening that would be lying next to the turbine wheel open area  24 , within said turbine wheel  20 . Said head door  46  as closed, would be lying next to said combustion chamber outlet opening  34 , and would be inside said upper engine open area  12 . 
   Said head door  46  as closed and having said pistons  60 ,  68  in a forward movements toward said upper engine open area  12 , within said combustion chamber  28 , compressing said incoming air-fuel mix within said combustion chamber  28 . Said exploding gases within said combustion chamber  28 , expelling said exploding gases into said upper engine open area  12 , pushing said head door  46  open into said upper engine open area  12 . 
   Said combustion chamber outlet opening  34 , would be on the side of said upper engine open area  12  and mounted at periphery of said combustion chamber  28 , with said combustion chamber outlet opening  34  expelling said exploding gases into said upper engine open area  12 , from said combustion chamber  28 . Said head door  46  lying next to said combustion chamber outlet opening  34 , would be on the top of as closed and would be within said upper engine open area  12  as open. Said exploding gases expelling into said upper engine open area  12  from said combustion chamber outlet opening  34 , would be pushing said head door  46  open, into said upper engine open area  12 . Said head door  46  as closed would stop said compressed exhaust gases from entering back into said combustion chamber  28 . 
   Said upper engine open area outlet opening  14  side of said upper engine open area  12  would be mounted at periphery of said turbine wheel  20 . With said upper engine open area outlet opening  14 , lying next to said turbine wheel inlet-outlet opening  22 , would expel exploding gases into said turbine wheel open area  24  from said upper engine open area  12 . Said head door  46  as open with said exploding gases from said combustion chamber  28  would be expel said exploding gases into said upper engine open area  12 , then would expel said exploding gases into said turbine wheel open area  24 , therefore concurrently rotating said turbine wheel  20  in a rotary motion. Said exploding gases now would be turning into compressed exhaust gases. 
   Said compressed exhaust gases expelling into said turbine wheel open area  24 , from said upper engine open area  12  with the concurrently rotating said turbine wheel  20 , would expel said compressed exhaust gases into said turbine wheel open area  24 , then would expel said compressed exhaust gases into said lower engine area  18 . Said compressed exhaust gases expelling into said lower engine area  18 , from said turbine wheel open area  24  that is concurrently rotating, would then expel said compressed exhaust gases into said head door aa-line  38 . Some of said compressed exhaust gases would be expels into said head door aa-line  38  and some of said compressed exhaust gases would be expel into said cylinder bottom area  80 . 
   Said compressed exhaust gases expelling into said head door aa-line  38  from said lower engine area  18 , would then expel said compressed exhaust gases into said head door open area  44 , would then expel said compressed exhaust gases into said door ba-line  52  that lying within said head door  46 . Said compressed exhaust gases expelling into said door ba-line  52  from said head door aa-line  38 , would then expel said compressed exhaust gases into said door line outlet bc-opening  56 , and would then expel said compressed exhaust gases into said upper engine open area  12 . Said compressed exhaust gases expelling into said upper engine open area  12  from said door line outlet bc-opening  56 , would be pushing on said head door  46  and closing and keeping said head door  46 , onto said combustion chamber outlet opening  34 . Said compressed exhaust gases coming out said door line outlet bc-opening  56  with its said compressed exhaust gases with its outward force, would be forcing said head door  46  down onto said combustion chamber outlet opening  34  and closing along with keeping said head door  46  down. With said head door  46  as closed and with said pistons  60 ,  68  forward movements, would start compressing said incoming air-fuel mix within said combustion chamber  28 . 
   Turbine Wheel 
   Enclosed within said flywheel combustion engine  10 , said turbine wheel  20 , utilizing member including said turbine wheel inlet-outlet opening  22  that is an opening into said turbine wheel open area  24  rotating around meeting opening of said upper engine open area  12  and meeting opening of said lower engine area  18 , said turbine wheel open area  24 , a turbine wheel outer edge  26 , a drive shaft  102 . 
   Said turbine wheel  20  enclosed within said flywheel combustion engine  10  with depressions within said turbine wheel outer edge  26 , these depressions around said turbine wheel outer edge  26  are called said turbine wheel open area  24 . Said turbine wheel  20  is Rota ably mounted on axis called the drive shaft  102 . The turbine wheel outer edge  26  that being the outer edge of and at the periphery of the upper engine open area  12 . Said turbine wheel inlet-outlet opening  22  that is the opening for said upper engine open area  12 . Said drive shaft  102  rotates at the center of said turbine wheel  20 . Said turbine wheel open area  24  that is the space lying within said turbine wheel  20  and having said turbine wheel inlet-outlet opening  22 , this opening would open into said upper engine open area  12  and open into said lower engine area  18 . 
   These depressions being said turbine wheel open area  24 , let said exploding gases expelling into said turbine wheel open area  24 , concurrently rotating said turbine wheel  20  in a rotary motion. Said exploding gases expelling into said turbine wheel open area  24  from said upper engine open area  12 , concurrently rotating said turbine wheel  20  in a rotary motion. 
   Said exploding gases now would be turning into compressed exhaust gases within said turbine wheel open area  24 . 
   Said concurrently rotating said turbine wheel  20 , with said upper engine open area  12 , in a rotary motion rotate around from said upper engine open area outlet opening  14  and rotating to a lower engine inlet opening  16 . Said turbine wheel  20  would in a rotary motion rotate around and around. Said upper engine open area outlet opening  14  that is the opening that open into said upper engine open area  12 . The lower engine inlet opening  16  this would be the opening that open into the lower engine area  18 . 
   Said turbine wheel  20  that is at the periphery of said upper engine open area outlet opening  14 , and that is at the periphery of said lower engine inlet opening  16 . Said compressed exhaust gases within said turbine wheel open area  24 , concurrently rotating expelling said compressed exhaust gases into said lower engine inlet opening  16 , would then expel said compressed exhaust gases into said lower engine area  18 . Said drive shaft  102  rotates at the center of said turbine wheel  20  converting energy of said exploding gases into mechanical energy or work. 
   Lower Engine Area 
   Enclosed within said flywheel combustion engine  10 , said lower engine area  18 , utilizing member including said lower engine inlet opening  16  that is an opening into said lower engine area  18  with the rotating said turbine wheel inlet-outlet opening  22  meeting said lower engine inlet opening  16 , a head door line inlet ab-opening  40  that is an opening into said head door aa-line  38  from said lower engine area  18 , said lower cylinder inlet-outlet opening  74  that is an opening into said cylinder bottom area  80  from said lower engine area  18  and same opening from said cylinder bottom area  80  into said lower engine area  18 . 
   Said lower engine area  18  mounted at periphery of said turbine wheel  20  being at said lower engine inlet opening  16 , and also mounted next to said head door line inlet ab-opening  40 , also mounted next said lower cylinder inlet-outlet opening  74 . The lower engine area  18  that would be the space between opening of the lower engine inlet opening  16 , said head door line inlet ab-opening  40 , and said lower cylinder inlet-outlet opening  74 . 
   Said compressed exhaust gases within said turbine wheel open area  24  within the concurrently rotating said turbine wheel  20  expelling these said compressed exhaust gases into said lower engine area  18 . 
   Said compressed exhaust gases within said lower engine area  18  expelling said compressed exhaust gases into said head door line inlet ab-opening  40 , then expelling said compressed exhaust gases into said head door aa-line  38 . 
   Some of said compressed exhaust gases within said lower engine area  18  would be expel into said head door line inlet ab-opening  40  and some said compressed exhaust gases would be expel into said lower cylinder inlet-outlet opening  74 . 
   Said compressed exhaust gases within said lower engine area  18 , would expel these said compressed exhaust gases into said lower cylinder inlet-outlet opening  74  would then expel said compressed exhaust gases into said cylinder bottom area  80 . 
   Said backward movement of said pistons  60 ,  68  toward said lower cylinder inlet-outlet opening  74  would be pushing said compressed exhaust gases from said cylinder bottom area  80 , back into said lower engine area  18 , putting added compression within said lower engine area  18 . This added compression would help push said compressed exhaust gases into said head door line inlet ab-opening  40 . 
   Said lower cylinder inlet-outlet opening  74  on the backward movement of said pistons  60 ,  68  toward said lower engine area  18 , would be pushing said compressed exhaust gases into said lower engine area  18  from said cylinder bottom area  80 . Said lower cylinder inlet-outlet opening  74  on the forward movement of said pistons  60 ,  68  toward said combustion chamber  28  said compressed exhaust gases from said lower engine area  18  would expel into said cylinder bottom area  80 . Said compressed exhaust gases that is expelling into said cylinder bottom area  80  would be pushing said pistons  60 ,  68  forward toward said top bore area  76 . 
   Head Door aa-line 
   Enclosed within said flywheel combustion engine  10 , said head door aa-line  38 , utilizing member including said head door line inlet ab-opening  40  that is a opening from said lower engine area  18  into said head door aa-line  38 , a head door line outlet ac-opening  42  that is a opening from said head door aa-line  38  into said head open area  44 , said head open area  44  that is an open area for said head door  46  to have movement in and is for said door line inlet bb-opening  54  to have an opening in. The means of controlling head door  104  between the upper engine open area  12  and the head door open area  44 . Said head door  46  would have part of lying within said upper engine open area  12  and would have part of lying within said head door open area  44 . The door line inlet bb-opening  54  lying within said head door  46  that would be the opening between the head door open area  44  and the door ba-line  52 . Said head door aa-line  38  would be a pipe for conveying said compressed exhaust gases from said lower engine area  18  into said line inlet bb-opening  54  then into said upper engine open area  12 . 
   Said compressed exhaust gases within said lower engine area  18  would then expel into said head door line inlet ab-opening  40 , would then said compressed exhaust gases into said head door aa-line  38 . Said compressed exhaust gases within said head door aa-line  38  expelling into said head door line outlet ac-opening  42 , would then expel said compressed exhaust gases into said into said head door open area  44 . Said compressed exhaust gases within said head door open area  44  expelling into said door line inlet bb-opening  54 , would then expel said compressed exhaust gases into said into said door ba-line  52 . Said compressed exhaust gases within said door ba-line  52  expelling into said door line outlet bc-opening  56 , would then expel said compressed exhaust gases into said upper engine open area  12 . Said compressed exhaust gases coming out said door line outlet bc-opening  56  within said head door  46 , expelling into said upper engine open area  12 , would be pushing said head door  46  down and closing said head door  46  onto said combustion chamber outlet opening  34 . 
   Said means of controlling head door  104  between said upper engine open area  12  and said head door open area  44 , said head door  46  would have part of lying within said upper engine open area  12  and would have part of lying within said head door open area  44 . The means of controlling head door  104  that is also used for stopping said compressed exhaust gases from entering into the upper engine open area  12  or entering into the head door open area  44 , except into the door line inlet bb-opening  54 . Said means of controlling head door  104 , this would be a means for having movement of said head door  46  within said upper engine open area  12  also have movement of said head door  46  within said head door open area  44 . Said part of said head door  46  within said upper engine open area  12  has said door line outlet bc-opening  56 . Said part of said head door  46  within said head door open area  44  has said door line inlet bb-opening  54 . 
   Bore Line 
   Enclosed within said flywheel combustion engine  10 , said bore line  88 , said bore inlet opening  86  that is an opening into said bore line  88  from said cylinder bottom area  80 , said bore outlet opening  90  that is an opening from said bore line  88  into said cylinder in-between area  78 . 
   Said bore line  88  this is a pipe for conveying said compressed exhaust gases from said cylinder bottom area  80  into said cylinder in-between area  78 . Said bore line  88  mounted at periphery of said cylinder  58 , with said bore inlet opening  86  connected to said cylinder bottom area  80  of said cylinder  58  and said bore outlet opening  90  that is connected to said cylinder in-between area  78  of said cylinder  58 . 
   Some of said compressed exhaust gases that expel into said cylinder bottom area  80 , that is now pushing said pistons  60 ,  68  upward toward said combustion chamber  28 . As said bore inlet opening  86  of said bore line  88  open up, by the forward movement of said pistons  60 ,  68 , expelling said compressed exhaust gases into said bore line  88 , would then expel said compressed exhaust gases into said bore outlet opening  90 , would then expel said compressed exhaust gases into said cylinder in-between area  78 . 
   Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86  of said bore line  88  within said cylinder bottom area  80 , would then expel said compressed exhaust gases into said bore line  88 . Forward movement of said pistons  60 ,  68  opens said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78 , and closes said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 , would then expel said compressed exhaust gases into said cylinder in-between area  78 . 
   Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86 , and opens said bore outlet opening  90  of said bore line  88 . Forward movement of said pistons  60 ,  68  closes said exhaust line inlet opening  92  of said exhaust line  94 , within said cylinder in-between area  78 . 
   Backward movement of said pistons  60 ,  68  toward said lower engine area  18 , closes said bore inlet opening  86  of said bore line  88  within said cylinder bottom area  80 , stopping said compressed exhaust gases from entering said bore line  88 . Backward movement of said pistons  60 ,  68  closes said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78  and opens said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 , would be expelling said compressed exhaust gases into said exhaust line  94 . Forward movement of said pistons  60 ,  68  opens said bore inlet opening  86  and opens said bore outlet opening  90  of said bore line  88 . Backward movement of said pistons  60 ,  68  opens said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 . 
   Exhaust Line 
   The flywheel combustion engine  10 , with the exhaust line  94  mounted on and connected to the cylinder  58 . Said exhaust line  94  utilizing member including said exhaust line inlet opening  92  that is an opening into said exhaust line  94  from said cylinder in-between area  78 , said exhaust line outlet opening  96  that is an opening from said exhaust line  94  and exhausting said exhaust gases out said flywheel combustion engine  10 . 
   Said exhaust line  94  begin a pipe for conveying the exhaust expansion gases from said exhaust line inlet opening  92  to said exhaust line outlet opening  96 . Said exhaust line inlet opening  92 , for expelling said compressed exhaust gases that is within said cylinder in-between area  78 , then expelling said compressed exhaust gases into said exhaust line  94 . Said compressed exhaust gases now would be turning into exhaust gases. Said exhaust line outlet opening  96  for expelling said compressed exhaust gases that is within said exhaust line  94 , would then expel said exhaust gases out of said flywheel combustion engine  10 . 
   Forward movement of said pistons  60 ,  68  would close up said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 . Backward movement of said pistons  60 ,  68  would open up said exhaust line inlet opening  92  of said exhaust line  94  within said cylinder in-between area  78 . 
   Forward movement of said pistons  60 ,  68  would open up said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78 , and would close up said exhaust line inlet opening  92  within said cylinder in-between area  78 . 
   Backward movement of said pistons  60 ,  68  would close up said bore outlet opening  90  of said bore line  88  within said cylinder in-between area  78 , and would open up said exhaust line inlet opening  92  within said cylinder in-between area  78 . 
   Ramifications of Detailed Description 
   The foregoing discussion and claims that follow describe only preferred embodiments of present invention. These embodiments particularly with respect to the claims. Understood a number of changes might be made without departing from essence present invention. It is intended that such changes substantially achieve the same results. Substantially same way will still fall within scope of the present invention. 
   It is not practical to describe in claims all possible embodiments. Embodiments may be accomplished generally in keeping with present invention. Disclosure may include separately or collectively aspects described found throughout description of patent. While these may be added to explicitly include such details. Existing claims should be construed to encompass such aspects. To the extent methods claimed in present invention are not further discussed. Any extent methods are natural outgrowths of the system or apparatus claims. Therefore, separate and further discussions of the methods are deemed unnecessary. Otherwise claim steps implicit in use and manufacture of system or apparatus claims. Furthermore, steps organized in logical fashion and other sequences can and do occur. Therefore, method claims should not be construed to include only this order. Other order and sequence steps may be presented. 
   Furthermore, any references mentioned in the application for this patent as well as all references listed. That all and any information disclosure originally filed with the application is hereby incorporated. That all reference in their entirety to the extent such may be deemed essential. That all supports ennoblement of the invention(s). However, to the extent statements might be considered inconsistent with the patenting of this/these invention(s). Any such statements are expressly not to be considered as made by the applicant. 
   Notice: Subject to any disclaimer, the term of this patent is extended or adjusted under 35 U.S.C. 154(b) by 0 days.