Source: http://www.google.com/patents/US4643166?dq=2040248
Timestamp: 2017-04-27 18:12:00
Document Index: 401960865

Matched Legal Cases: ['art.\n3', 'art.\n4', 'art.\n6', 'art 38', 'art 40', 'art 38', 'art 40', 'art 40', 'art 38', 'art 40', 'art 38', 'art 38', 'art 38', 'art 38', 'art 38', 'art 38', 'arts 38']

Patent US4643166 - Steam engine reaction chamber, fuel composition therefore, and method of ... - Google PatentsSearch Images Maps Play YouTube News Gmail Drive More »Sign inPatentsA fuel composition for a reaction chamber which when combined with a selected reactant produces heat energy and hydrogen gas. A reaction chamber structure, method of making and method of operating the reaction chamber are also disclosed....http://www.google.com/patents/US4643166?utm_source=gb-gplus-sharePatent US4643166 - Steam engine reaction chamber, fuel composition therefore, and method of making and operating sameAdvanced Patent SearchTry the new Google Patents, with machine-classified Google Scholar results, and Japanese and South Korean patents.Publication numberUS4643166 APublication typeGrantApplication numberUS 06/681,160Publication dateFeb 17, 1987Filing dateDec 13, 1984Priority dateDec 13, 1984Fee statusLapsedAlso published asEP0188092A1Publication number06681160, 681160, US 4643166 A, US 4643166A, US-A-4643166, US4643166 A, US4643166AInventorsNorman D. Hubele, Kim L. JohnsonOriginal AssigneeThe Garrett CorporationExport CitationBiBTeX, EndNote, RefManPatent Citations (22), Referenced by (20), Classifications (19), Legal Events (6) External Links: USPTO, USPTO Assignment, EspacenetSteam engine reaction chamber, fuel composition therefore, and method of making and operating same
US 4643166 AAbstract
A fuel composition for a reaction chamber which when combined with a selected reactant produces heat energy and hydrogen gas. A reaction chamber structure, method of making and method of operating the reaction chamber are also disclosed.
1. Heat-supplying reaction chamber apparatus for use with a heat engine comprising; a vessel defining a chamber therewithin, an inlet means for receiving a reactant, and an outlet means for efflux of a gaseous reaction product; a two-part fuel mass disposed within said chamber including a hydrogolic first starting fuel part comprised of lithium hydride and at least one other metallic element and being so disposed with respect to said inlet as to be first contact by said reactant for reaction therewith to liberate (a) heat, (b) a reaction intermediate which is more reactive with the remainder of said fuel mass at ambient temperatures than is said reactant, and (c) said gaseous reaction product at a first determined rate of evolution; a second main fuel part comprising a metallic element which upon being raised to a determined temperature by reaction of said starting fuel part with said reactant itself reacts with the latter to further liberate heat and said gaseous reaction product at a second certain rate of evolution which is substantially equal to said first determined rate of evolution of said gaseous reaction product; and heat transfer means in association with said fuel mass for transfer of heat energy therefrom to said heat engine; whereby said reaction chamber apparatus provides during operation including both a starting reaction phase and a main fuel reaction phase a substantially constant rate of efflux of said gaseous reaction product from said outlet means.
2. The invention of claim 1 wherein said inlet means comprises means for conveying said reactant first into reacting relationship with said starting fuel part.
3. The invention of claim 2 wherein said conveying means comprises a foraminous distribution means disposed within said fuel mass and on one side receiving said reactant for conveyance therethrough to said starting fuel part.
4. The invention of claim 3 wherein said starting fuel part is disposed in surrounding relation with said foraminous distribution means within said fuel mass.
5. The invention of claim 1 wherein said inlet means comprises manifold means for conveying said reactant to a plurality of distribution means, said distribution means being spaced apart in depending relation with said manifold means within said fuel mass and including means for communicating said reactant directly to said starting fuel part.
6. The invention of claim 5 wherein said starting fuel part is disposed in surrounding relationship with said plurality of distribution means as a layer therearound within said fuel mass.
7. The invention of claim 1 wherein said outlet means comprises filter means for allowing substantially only said gaseous reaction product to flow from said reaction chamber.
8. The invention of claim 7 wherein said filter means comprises a perforate plate and a felt metal pad in serial relationship between said fuel mass and the outlet.
9. The invention of claim 8 wherein said fuel mass is disposed in a lower portion of said chamber, said filter means being disposed in an upper portion of said chamber above said fuel mass and comprising in ascending order, said perforate plate, and said felt metal pad.
10. The invention of claim 8 wherein said perforate plate comprises multiple apertures of substantially 0.125 inch diameter and in aggregate comprising substantially 60% of the area of said plate.
11. The invention of claim 8 wherein said felt metal pad comprises metallic filaments of substantially 0.006 inch size in aggregate comprising substantially 60% of the bulk density of said pad and cooperating to yield a pore size of substantially 95μ inch.
12. The invention of claim 1 wherein said starting fuel part comprises lithium hydride and a metallic element from the group including magnesium and aluminum.
13. The invention of claim 1 wherein said starting fuel part comprises lithium hydride and both metallic magnesium and metallic aluminum.
14. The invention of claim 13 wherein said starting fuel part is composed essentially of lithium hydride, metallic magnesium and metallic aluminum in substantially equal molar relationship.
15. The invention of claim 1 wherein said main fuel part comprises a metallic element from the group including magnesium and aluminum.
16. The invention of claim 1 wherein said main fuel part comprises both metallic aluminum and metallic magnesium.
17. The invention of claim 16 wherein said main fuel part is composed essentially of metallic aluminum and metallic magnesium in substantially a 2:1 molar relationship, respectively.
18. The invention of claim 1 wherein said starting fuel part is composed essentially of lithium hydride, metallic magnesium, and metallic aluminum in substantially equal molar relationship; said main fuel part being composed essentially of metallic aluminum and metallic magnesium in substantially 2:1 molar relationship, respectively; said fuel mass being composed of said starting fuel part and said main fuel part in substantially 1:4 weight relationship.
19. The invention of claim 1 wherein said main fuel part is disposed in a lower portion of said chamber, said starting fuel part being disposed as a layer upon said main fuel part, said inlet means being disposed above and spaced apart from said fuel mass, and said outlet means being disposed above said inlet means with respect to receipt of said reactant into said chamber.
20. The invention of claim 19 wherein said outlet means comprises filter means for allowing substantially only said gaseous reaction product to flow from said reaction chamber.
21. The invention of claim 20 wherein said inlet means comprises a conduit dependent within said chamber above said fuel mass and terminating in a nozzle means for penetratingly directing said reactant upon said fuel mass.
22. Reaction chamber apparatus for supplying both sensible heat and a substantially constant flow of hydrogen gas upon introduction of a liquid reactant consisting essentially of water, said apparatus comprising:(a) chamber defining housing means also defining an inlet and an outlet both opening to said chamber, and heat transfer means for transport from said housing means of heat energy; (b) a two-part fuel mass disposed within said chamber for reaction with said reactant to produce heat and hydrogen gas, said fuel mass consisting essentially of a first starting fuel part which is hypergolic with said liquid reactant at substantially ambient temperature to produce hydrogen gas while heating the second part of said two-part fuel mass to a molten state and producing a reaction intermediate assisting in reacting of said second fuel mass part, said second fuel mass part comprising a main fuel which is reactive with said liquid reactant substantially only at elevated temperature in a molten state also to produce heat and hydrogen gas; (c) said starting fuel part consisting essentially of lithium hydride, metallic magnesium, and metallic aluminum each in substantially equal molar weight relation; (d) said main fuel part consisting essentially of metallic aluminum and metallic magnesium in substantially 2:1 molar weight ratio, respectively; (e) said starting fuel part and said main fuel part being in substantially 1:4 weight ratio, respectively; and (f) said starting fuel part being disposed relative said inlet and said main fuel part to first react with said reactant and being both in heat transfer and mass transfer relation with said main fuel to heat the latter to a molten state and provide said reaction intermediate thereto. Description
The field of the present invention is Rankine cycle vapor pressure or steam engines obtaining their driving heat energy from a chemical reaction other than the usual combustion of fuel with oxygen from the air. Particularly, the theoretical possibility of utilizing the reaction energy of a reactive metal fuel such as Aluminum, Magnesium, or Lithium, and alloys or hydrides of these and similar reactants, with an "oxidizer" such as hydrogen peroxide, Freons, sulfur hexaflouride, water, and others, has been recognized for many years. However, the technical difficulties and conflicts standing between a theoretical construction of such a power system and a practical apparatus which is functional outside of the laboratory are legion.
By way of example, many of the fuel-reactant combinations proposed in the past require that the fuel be raised above ordinary ambient temperatures in order to permit reaction with the reactant. Such a heating requirement necessitates that some heating means, such as electrical heating coils or pyrotechnic chemicals be provided. In the former case, a significant start-up delay is incurred while a portion or all of the fuel is raised to reaction temperature. In the latter case, the pyrotechnic chemicals, which are or may be considered to be low velocity explosives, present the possibility of rupturing the reaction chamber and escape of highly reactive or toxic fuels. Such pyrotechnic heating chemicals also frequently produce a quantity of gaseous reaction products which must be contained within the reaction chamber, or else vented therefrom while preventing loss of fuel.
Another undesirable aspect of many previously proposed fuel-reactant systems is that intermediate reaction products or end reaction products are formed which on the one hand inhibit further progress of the reaction between the fuel and reactant, or on the other hand freeze at a temperature higher than the desired reaction chamber temperature. In the one case, complex structures and methods have been proposed to cure the shortcoming by removing the intermediate or final reaction product from the reaction chamber. Alternatively, only a portion of the fuel could be brought into contact with the reactant so that reaction products could not contaminate the remaining fuel. Again, complexity is increased.
A novel approach to the above-discussed problem is presented by the copending patent application Ser. No. 681,161 of Palmer Wood, having the same filing date and assignee as this application (hereinafter the Wood application). In the Wood application a fuel is reacted with water in the absence of oxygen to produce heat and hydrogen. The heat from this reaction is used to produce water steam. The hydrogen is burned with oxygen in a separate second reaction chamber to produce super heated steam. The steam from the first reaction chamber is used as a coolant and diluent in the second reaction chamber so that steam flowing from the second reaction chamber to a turbine, or other expander, has a metalurgically acceptable temperature. The disclosure of the Wood application is hereby incorporated herein by reference to the extent necessary for a complete understanding of the present invention.
A shortcoming of the invention of the Wood application discovered by the present inventors is that a hydrogen bearing reaction intermediate is formed which initially partially prevents the evolution of the hydrogen from the first reaction chamber. As the reaction progresses, the reaction intermediate further reacts to release the bound hydrogen. The result is that over the period of the reaction, the rate of hydrogen production is at first relatively low, reaches a stable plateau, and then raises above the plateau as the fuel supply is consumed.
A consequence of this nonuniform rate of hydrogen production is that the power output of the Rankine cycle steam engine is relatively low initially and cannot be increased until the hydrogen production rate of the chemical reaction chamber increases. Understandably, this sluggish initial power output of such a system is undesirable in almost every prospective applications. Additionally, the nonuniform rate of hydrogen production creates many difficulties in controlling the power output level of the Rankine cycle engine.
Conventional reaction chambers, fuel-reactant combinations, and methods of operating engines of the above-defined character are presented in U.S. patents noted hereinabove.
In view of the above discussion it is an object of the present invention to provide a reaction chamber fuel composition reactive with water to produce hydrogen at a substantially uniform rate during the life of the fuel supply. Another object of this invention is to provide such a reaction chamber fuel composition which is reactive with water at common ambient temperatures, and which does not require preheating or pyrotechnic chemicals, for example, to be used in starting the reaction.
Another object of the present invention is to provide a reaction chamber structure for use with the inventive present fuel composition, and other fuel compositions of a similar nature.
Still another object of the present invention is to provide a method of making a reaction chamber according to the present invention.
Yet another object of the present invention is to provide a method of operating a reaction chamber according to the present invention.
The present invention according to one aspect provides a two-part fuel composition including a first or main fuel part of magnesium and aluminum in a molar ratio of 1:2, respectively. The second or starter fuel part is composed of lithium hydride, magnesium, and aluminum in equal molar ratio. On a weight basis, the starting fuel composition and main fuel composition are presented at a ratio of about 1:4.
In a reaction chamber according to the present invention, the above-outlined fuel is present in the form of prealloyed powders produced, for example, from condensed vaporized or atomized metal. The reaction chamber structure provides in addition to heat transfer means, a means for introducing water into the chamber for reaction with the fuel.
According to one aspect of the invention, the means for introducing water comprises a manifold with foraminous distribution tubes depending in the fuel. The distribution tubes are immediately surrounded by a comparatively thin layer of the starting fuel part. The main fuel part is received within the reaction chamber around the distribution tubes and layer of starting fuel part.
According to another aspect of the invention, the main fuel part is disposed in a lower portion of the reaction chamber. In an upper portion of the reaction chamber is disposed an appropriate quantity of the starting fuel part. The reaction chamber includes a water inlet nozzle disposed in an upper part of the reaction chamber above both the starting and main fuel parts. Preferrably, the water nozzle is separated from the fuel during operation of the reaction chamber and engine.
In accord with yet another aspect of the invention, a method of operating a reaction chamber of the descibed character includes reacting water with a hydride of a reacting fuel element to form a hydroxide of the fuel element which hydroxide is further reactive with a first mixture of fuel elements being rather less reactive than the hydride of the first fuel element. The heat liberated from the above described reaction is employed to raise the temperature of the less reactive fuel elements to a level where they are vigorously reactive with the present hydroxide and with water.
Still another aspect of the present invention involves the method of making a reaction chamber according to the invention and including the steps of providing means for introducing water into the reaction chamber, disposing a selected quantity of the first starting fuel part in proximity with said water introducing means to be first contacted by water introduced therethrough, and filling the remainder of the reaction chamber, or a selected portion thereof, with the second main fuel part.
The advantages offered by the present invention include the absence of any need or requirement to provide fuel preheating before the reaction chamber is operational. Further, the introduction of simple water is all that is required to initiate operation of the reaction chamber to produce both heat and a supply of hydrogen. This latter feature is of particular advantage when the invention is used in connection with a water bourne vehicle. Understandably, a quantity of the available water may be used in the Rankine cycle steam engine, eliminating entirely the need to store water aboard the vehicle for such use.
Further to the above, the rate of heat and hydrogen, production may be moderated during the life of the available fuel supply by controlling the rate of water supply to the reaction chamber so that the Rankine cycle engine may be throttled. Additionally, the rate of hydrogen production during the use of the fuel supply is substantially uniform in proportion to moderation of the reaction rate with the rate of water supply. The reaction intermediates and final reaction products do not seriously interfere with heat transfer out of the reaction chamber.
Still further, the applicants have discovered that the present invention virtually eliminates anticipated difficulties with separating the evolved hydrogen from the reaction products and fuel. Such separation is essential to prevent fuel and reaction products being carried into and damaging the steam expander of the Rankine cycle engine. Surprisingly, the fuel composition and reaction chamber of the present invention allows a very simple filter structure to be interposed between the fuel and the hydrogen outlet from the reaction chamber. An unexpected phenomenon described herein below results in a simple filter accomplishing almost perfect filtering of the evolved hydrogen
FIG. 1 schematically depicts a reaction chamber according to the present invention, and having a two-part fuel composition disposed therein;
FIG. 2 schematically depicts an alternative embodiment of a reaction chamber according to the invention; and
FIG. 3 graphically depicts and compares the rates of hydrogen production of reactions according to the Wood application, and in accordance with the present invention.
With reference to FIG. 1, a preferred embodiment of the inventive reaction chamber 10 is depicted. The reaction chamber 10 includes a vessel 12 defining a reaction water inlet 14 and a hydrogen outlet 16. Additionally, the vessel 12 includes structure 18 for transfering heat from the interior of vessel 12 to a Rankine cycle or other heat engine (not illustrated). The heat transfer structure is depicted as a boiler tube 20 passing into the vessel 12 at 22 to define a water inlet, and passing out of the vessel at 24 to define a steam outlet.
Within the vessel 12, the reaction water inlet 14 communicates with a manifold 26 having a plurality of foraminous water distribution tubes 28 depending therefrom. Also disposed within the vessel 12 in surrounding relation with the inlet 14 is a hydrogen filter structure generally referenced with the numeral 30. The hydrogen filter 30 preferrably includes a lower perforate plate 32, and a pair of felt-metal pads 34,36 disposed above the plate 32.
Also disposed within the vessel 12 in surrounding relation with the perforate distribution tubes 28 is a selected quantity of a first or starting fuel part 38. The starting fuel 38 is disposed within the reaction chamber 10 somewhat in the form of a coating upon or around the tubes 28. Similarly, around the starting fuel 38 is disposed a certain quantity of a second or main fuel part 40. The main fuel 40 fills substantially all of the remaining volume of the vessel 12 and is in surrounding relation or otherwise in heat transfer relation with the structure 18.
One example of a fuel composition for use within reaction chamber 10 is composed of starting fuel part 38 having equal molal components of lithium hydride, magnesium, and aluminum. This starting fuel composition is employed with a main fuel part 40 of aluminum and magnesium in a molar ratio of 2:1. Preferably, the main fuel part 40 and starting fuel part 38 are present in a ratio of about 4:1, on a weight basis.
Turning now to FIG. 2, an alternative embodiment of the invention is depicted wherein reference numerals previously used and with a prime added designate similar elements. The reaction chamber 10' includes a vessel 12' with reaction water inlet 14', hydrogen outlet 16', heat transfer structure 18', and filter structure 30'. However, the main fuel part 40' is simply disposed in the lower portion of the vessel 12', with a layer of the starting fuel part 38' disposed on the main fuel part in an upper portion of the vessel 12'. A distance above the upper surface of the starting fuel part 38' is disposed an inlet nozzle 26' at the lower end of the inlet 14'. The nozzle 26' is arranged to project water received via inlet 14, downwardly upon and into the fuel 38',40' as a single penetrating stream, plurality of such streams, or penetrating mist. Importantly, the nozzle 26' is spaced sufficiently away from the fuel 38',40' that even allowing for thermal expansion of the reactants, nozzle 26' is not contacted by the molten fuel.
Having observed the structure of the two preferred embodiments of the invention, attention may now be directed to their operation. With respect to FIG. 1, when it is desired to start operation of the Rankine cycle heat engine (not shown) water is supplied to inlet 14 at a determined rate. The supplied water is distributed by manifold 26 to distribution tubes 28. The perforate distribution tubes 28 carry the supplied water into immediate contact with substantially all of the starting fuel part 38. Such is the case because, as pointed out above, the starting fuel part 38 is disposed in surrounding relation with the tubes 28 as a relatively thin layer or coating. The supplied water reacts with the starting fuel part to produce Lithium hydroxide and heat. Lithium hydroxide further reacts with the other constituents of the starting fuel part and with the main fuel part to produce hydrogen gas and additional heat. The initial heat production from the starting fuel part 38', serves both to increase the temperature and to increase the propensity to react with water of the remaining fuel. In very short order, the entire mass of fuel is raised to a sufficiently high temperature that the fuel is molten and readily reacts with water.
FIG. 3 graphically depicts the time rate of hydrogen production from a reaction chamber according to the invention with the passage of time from the moment of first water injection into the reaction chamber, Viewing FIG. 3, line A represents, for comparison only, the rate of hydrogen production from a reaction chamber according to the Wood application. As line A represents, a reaction chamber according to the Wood application initially produces hydrogen at a relatively low rate which increases more slowly than desired (portion A1,). Following the initially slow start, the reaction chamber reaches a plateau (portion A2) of relatively stable hydrogen production rate. Finally, as the fuel mass nears exhaustion, the reaction chamber according to the Wood application produces hydrogen at an increased rate (portion A3), leading to a drop off at exhaustion of the service life of the reaction chamber.
In contrast, line B on FIG. 3 depicts the rate of hydrogen production from a reaction chamber according to the present invention. As line B shows, after an initial starting surge, the rate of hydrogen production is substantially uniform throughout the service life of the reaction chamber. It will be understood, of course, that FIG. 3 is representative for comparison purposes only. In fact, the actual rate of hydrogen production from a particular reaction chamber is variable dependent on many factors including the relative size of the chamber and the controlled rate of reaction water introduction thereto.
With respect to the reaction chamber of FIG. 2, it will be noted that inlet 14', and nozzle 26' direct the water supplied thereto downwardly from above onto and into the fuel 38', 40'. Of course, the upper layer of starting fuel part 38' is first contacted by the introduced reaction water, much in the same fashion as the reaction chamber of FIG. 1. However, the nozzle 26' is at all times spaced apart from and above the zone of reaction which is formed where the reaction water reacts with the fuel parts 38' and 40'. Because the nozzle 26' is not immersed in the molten fuel 38',40', there is virtually no chance of the nozzle 26' becomming plugged with fuel or reaction products. Further, because the nozzle 26' is substantially free of heat transfer from the molten fuel 38',40', high-temperature materials of construction for the nozzle are not necessary, and the nozzle may be made of relatively common, inexpensive materials.
Surprisingly, an actual test of a reaction chamber similar to that of FIG. 2 has shown that the bath of molten fuel does not, as previously assumed, require agitation from direct immersed reactant injection. In other words, the reaction is sufficiently vigorous that the stirring, mixing influence of a jet or stream of water injected from a nozzle immersed in the bath is unnecessary. Simply spraying the water upon the fuel will allow the reaction chamber to run to completion of the reaction with acceptably high utilization of the fuel mass. Specifically, the Applicant's tests have shown a 95% or greater fuel utilization may be expected from a reaction chamber according to FIG. 2. The reaction chamber of FIG. 1, it is beleived, would provide a somewhat higher percentage of fuel utilization.
With both of the reaction chambers shown in FIGS. 1 and 2, the evolved hydrogen is filtered by filter structures 30 and provided via outlet 16 for utilization in the Rankine cycle engine (not shown). The fuel mixtures of the present invention are believed to offer a supprising and unexpected advantage by simplifying the required filter structure. The conflicting requirements for the filter structure 30 are that it be open to passage of hydrogen while being sufficiently closed to both fuel and reaction products that the latter are not allowed to pass downstream with the hydrogen via outlet 16. Further, the filter dare not clog. Surprisingly, the present fuel mixtures have been found to deposit reaction products on the filter 30 to a extent resulting in a self-regulating filter mechanism. An actual test of a reaction chamber 10' according to FIG. 2 employed a perforate plate 32 having apertures of 0.125" size, and comprising 60% open area of the total plate area. The felt metal pads 34, 36 were of 0.006" filament size with 95μ" pore size having 60% theoretical density. During operation of the reaction chamber virtually perfect filtering of the evolved hydrogen resulted. The internal pressure of the reaction chamber was within acceptable limits, indicating that the filter 30 was not clogged or overly restrictive to passage of Hydrogen. Neither was there indication of excessive openness or porosity of the filter. Astonishingly, where the reaction chamber was disassembled for visual inspection, the filter 30, and particularly pad 34, gave the appearnce of being clogged with reaction products. The filter was not in fact clogged with respect to passage of evolved hydrogen, however, as the acceptably low internal pressure of the reaction chamber during operation indicated.
Examination of the start up fuel reaction products of a test run indicated two product phases. The primary product phase was LiAlO2. The smaller secondary reaction product phase was MgAL2 O4 +LiAL5 O5. The percentages of pure fuel metals remaining were Li less than 1%, Mg less than 1%, and AL less than 1%. LiOH and MgO were both present in trace amounts.
In view of all of the above, it is seen the present invention provides novel fuel compositions for use in a reaction of the type described. Two preferred embodiments of the reaction chamber itself are presented along with methods of operating and making the reaction chambers. The invention also provides a substantially uniform rate of hydrogen evolution and allows the use of reactant injection nozzles which are optionally either immersed in or spaced above the molten bath of reactive fuel. Finally, it is seen that a significant and unexpected advantage results from the present invention in that filtering of the evolved hydrogen becomes self regulating.
The starting and main fuel part reactions with water are believed to be as follows:
STARTING FUEL REACTIONS
LiH+H2 O&#8594;LiOH+H2 &#8593;+QHEAT       (1)
2LiOH+AL2 O3 &#8594;2LiALO2 +H2 O+Q   (2)
LiOH+H2 O+AL&#8594;LiALO2 +3/2H2 &#8593;+Q (3)
Mg+H2 O&#8594;MgO+H2 &#8593;+Q                  (4)
MAIN FUEL REACTIONS
Mg+H2 O&#8594;MgO+H2 &#8593;+Q                  (1)
4MgO+2AL&#8417;MgAL2 O4 +3Mg               (2)
Patent CitationsCited PatentFiling datePublication dateApplicantTitleUS1532930 *Dec 5, 1919Apr 7, 1925Hugh O'neill JohnMethod and means of producing heatUS2968917 *May 6, 1954Jan 24, 1961Ethyl CorpMethod of operating a jet engine and fuel compositionUS2971325 *May 17, 1948Feb 14, 1961Aerojet General CoJet propulsion device for operation submerged in waterUS3048966 *Apr 23, 1959Aug 14, 1962SnecmaRocket propulsion methodUS3049872 *Oct 30, 1958Aug 21, 1962Phillips Petroleum CoJet engine combustion processUS3101592 *Jan 16, 1961Aug 27, 1963Thompson Ramo Wooldridge IncClosed power generating systemUS3149458 *Nov 1, 1962Sep 22, 1964Harris William SJet engine process using hydrogen produced from metal-hydrocarbon mixture and waterUS3153902 *Apr 4, 1961Oct 27, 1964Morrell Jacques CLithium rocket propellants and process for using the sameUS3153903 *Apr 4, 1961Oct 27, 1964Morrell Jacques CLithium rocket propellants and process for using the sameUS3158993 *Feb 18, 1959Dec 1, 1964Solid Fuels CorpSolid fuels and formulationsUS3158994 *Dec 29, 1959Dec 1, 1964Solid Fuels CorpSolid fuels and methods of propulsionUS3325318 *Feb 19, 1962Jun 13, 1967Trw IncFuel system comprising sulfur hexafluoride and lithium containing fuelUS3357186 *Oct 6, 1964Dec 12, 1967Multer Robert KHigh energy propulsion method using aluminum and waterUS3398536 *May 25, 1965Aug 27, 1968Philco Ford CorpFluid flow nozzle having temperature compensating meansUS3486332 *Oct 12, 1961Dec 30, 1969Trw IncPower plantUS3525223 *Mar 29, 1968Aug 25, 1970Licentia GmbhThermodynamic rocket process using alkali metal fuels in a two phase flowUS3771313 *May 3, 1971Nov 13, 1973 Generation of motive power with metal and water as fuelUS3779011 *Jul 19, 1971Dec 18, 1973Mini DefenseFuel unit for a hybrid hot-gas generatorUS3782112 *Feb 24, 1972Jan 1, 1974Us NavyHybrid generatorUS3964416 *Jul 19, 1965Jun 22, 1976The United States Of America As Represented By The Secretary Of The NavyBoiler reactorUS4118930 *Jun 14, 1974Oct 10, 1978The United States Of America As Represented By The Secretary Of The NavyFilter-coolerUS4406863 *Feb 9, 1982Sep 27, 1983The United States Of America As Represented By The Secretary Of The Air ForceIntegrated solid propellant gas generator and fluid heat exchanger* Cited by examinerReferenced byCiting PatentFiling datePublication dateApplicantTitleUS4846112 *Jul 25, 1988Jul 11, 1989Sundstrand Corp.Fuel bath volume compensator for stored chemical energy power propulsion systemUS4923019 *Feb 28, 1989May 8, 1990Arctic Systems LimitedThermochemical penetrator for ice and frozen soilsUS5143047 *Jun 20, 1991Sep 1, 1992The United States Of America As Represented By The Secretary Of The NavyMaterial and method for fast generation of hydrogen gas and steamUS5634341 *Dec 4, 1995Jun 3, 1997The Penn State Research FoundationSystem for generating hydrogenUS5867978 *May 9, 1997Feb 9, 1999The Penn State Research FoundationSystem for generating hydrogenUS6506360Jul 20, 2000Jan 14, 2003Erling Reidar AndersenMethod for producing hydrogenUS6638493Dec 16, 2002Oct 28, 2003Erling Reidar AndersenMethod for producing hydrogenUS6800258Nov 5, 2002Oct 5, 2004Erling Reidar AndersenApparatus for producing hydrogenUS7052671Jan 11, 2002May 30, 2006Safe Hydrogen, LlcStorage, generation, and use of hydrogenUS7144567Oct 27, 2003Dec 5, 2006Erling Jim AndersenRenewable energy carrier system and methodUS7326263Dec 8, 2003Feb 5, 2008Erling Reidar AndersenMethod and apparatus for hydrogenating hydrocarbon fuelsUS20020166286 *Jan 11, 2002Nov 14, 2002Mcclaine Andrew W.Storage, generation, and use of hydrogenUS20040115125 *Oct 27, 2003Jun 17, 2004Andersen Erling JimRenewable energy carrier system and methodUS20040131541 *Dec 8, 2003Jul 8, 2004Andersen Erling ReidarMethod and apparatus for hydrogenating hydrocarbon fuelsUS20050175868 *Mar 7, 2005Aug 11, 2005Mcclaine Andrew W.Storage, generation, and use of hydrogenUS20100280293 *Dec 12, 2007Nov 4, 2010Erling Reidar AndersenMethod and apparatus for hydrogenating hydrocarbon fuelsUS20110159385 *Aug 31, 2009Jun 30, 2011Atsushi TanakaHydrogen generator and fuel cell system including the sameUS20110165060 *Sep 23, 2009Jul 7, 2011Massimo MilaniMetal-fueled cogeneration plantCN102507198A *Sep 29, 2011Jun 20, 2012北京航空航天大学Device and method for filling solid lithium propellant pipelineCN102507198BSep 29, 2011Nov 13, 2013北京航空航天大学Device and method for filling solid lithium propellant pipeline* Cited by examinerClassifications U.S. Classification126/263.02, 122/21International ClassificationF01K3/18, F22B3/00, F01K15/02, F01K25/00, F01K27/00, C01B3/08, F42B19/12Cooperative ClassificationF01K3/188, F24J1/00, Y02E60/36, C01B3/08, F01K25/005, Y02P20/129European ClassificationF24J1/00, C01B3/08, F01K25/00B, F01K3/18FLegal EventsDateCodeEventDescriptionDec 13, 1984ASAssignmentOwner name: GARRETT CORPORATION, THE, 9851 SEPULVEDA BLVD., POFree format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNORS:HUBELE, NORMAN D.;JOHNSON, KIM L.;REEL/FRAME:004348/0233Effective date: 19841212May 29, 1985ASAssignmentOwner name: GARRETT CORPORATION, THE, A CA CORP.Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNORS:HUBELE, NORMAN D.;JOHNSON, KIM L.;REEL/FRAME:004406/0625Effective date: 19850520Jun 19, 1990FPAYFee paymentYear of fee payment: 4Sep 27, 1994REMIMaintenance fee reminder mailedFeb 19, 1995LAPSLapse for failure to pay maintenance feesMay 2, 1995FPExpired due to failure to pay maintenance feeEffective date: 19950222RotateOriginal ImageGoogle Home - Sitemap - USPTO Bulk Downloads - Privacy Policy - Terms of Service - About Google Patents - Send FeedbackData provided by IFI CLAIMS Patent Services