| Patents for F02K 7 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof (1,599) |
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| 09/13/1994 | US5345758 Rotary valve multiple combustor pulse detonation engine |
| 09/06/1994 | US5343695 Combined jet engine provided with means for switching between two operating states |
| 08/30/1994 | US5341639 Solids; burns partial decomposition products in secondary combustor to achieve complete combustion |
| 08/11/1994 | DE4402941A1 Kombinierter Motor mit integrierten Arbeitsweisen als Ejektor für turbokomprimierte, gekühlte oder verflüssigte Luft, als Staustrahltriebwerk und als Überschall-Staustrahltriebwerk Combined motor with integrated ways of working as an ejector for turbo-compressed, cooled or liquefied air as ramjet and a supersonic ramjet |
| 08/02/1994 | US5333445 Scramjet engine having improved fuel/air mixing |
| 07/27/1994 | EP0608142A1 Gas turbine engine cooling system |
| 07/12/1994 | US5327721 Ejector ramjet |
| 06/07/1994 | US5317866 Free-flying tubular vehicle |
| 06/07/1994 | CA1329992C Hypersonic scramjet engine fuel injector |
| 05/17/1994 | US5311774 Method and installation for generating a high mass flow of unpolluted high enthalpy air |
| 05/17/1994 | US5311735 Jet engine |
| 04/28/1994 | WO1994007013A3 Method and apparatus for power generation |
| 04/27/1994 | EP0593987A1 Variable square air intake duct |
| 04/26/1994 | US5305616 Gas turbine engine cooling system |
| 04/14/1994 | WO1994008131A1 Laser initiated non-linear fuel droplet ignition |
| 04/06/1994 | EP0590016A1 A solid fuel ramjet engine for, e.g., a spin-stabilized projectile |
| 03/31/1994 | WO1994007013A2 Method and apparatus for power generation |
| 03/31/1994 | DE4232738A1 Supersonic missile flight control system - has air intakes in shell between tip and body connected to control nozzles in shell wall via reservoir and fluid elements |
| 03/31/1994 | CA2144536A1 Method and apparatus for power generation |
| 03/19/1994 | CA2106292A1 Free-flying tubular vehicle |
| 02/17/1994 | DE4226666A1 Heat exchanger with cruciform, counter-current matrix of profiled tubes - adds fraction of part-stream to gas flowing round profile tubes in coupling region to centre tube |
| 02/09/1994 | CN1081743A Marine jet engine |
| 02/08/1994 | US5284014 Turbojet-ramjet hypersonic aircraft engine |
| 02/01/1994 | US5282359 Impulse jet engine |
| 02/01/1994 | US5282356 Flywheel engine |
| 01/25/1994 | US5280705 Fuel injection system for scramjet engines |
| 01/20/1994 | WO1994001657A1 An inert gas turbine engine |
| 01/19/1994 | EP0578951A1 Jet engine |
| 12/29/1993 | EP0576355A1 Changeover valve for a combi jet engine having two operational configurations |
| 12/29/1993 | EP0576354A1 Combined turbo-ram jet engine |
| 11/18/1993 | DE4215543A1 All-blade propeller functioning as turbine - has hollow blades acting as combustion chambers and gas discharge nozzles |
| 10/26/1993 | US5255513 Method of operating a scramjet including integrated inlet and combustor |
| 10/19/1993 | US5253474 Apparatus for supersonic combustion in a restricted length |
| 10/06/1993 | EP0564135A2 Gas turbine engine cooling system |
| 10/05/1993 | USH1234 Solid propellant air-turborocket |
| 07/06/1993 | US5224344 Variable-cycle storable reactants engine |
| 06/29/1993 | US5223651 Supersonic combustion engine and method of combustion initiation and distribution |
| 06/23/1993 | EP0547936A1 Method and device for generating non contaminated air gust by high enthalpy |
| 06/22/1993 | US5220787 Scramjet injector |
| 06/19/1993 | CA2085438A1 Method and installation for generating a high mass flow of unpolluted high enthalpy air |
| 04/29/1993 | WO1993008397A1 Turbojet engine with a fan or propfan |
| 04/27/1993 | US5205119 Ejector ramjet |
| 04/22/1993 | DE4134051A1 Turbinenstrahltriebwerk mit geblaese oder prop-fan Turbojet engine with fan or prop-fan |
| 04/13/1993 | US5202525 Scramjet engine having improved fuel/air mixing |
| 04/13/1993 | US5201886 Method of operating a pulse thruster |
| 03/30/1993 | US5197399 Pulse combusted acoustic agglomeration apparatus and process |
| 03/09/1993 | US5191761 Aerospace plane and engine |
| 03/02/1993 | US5189875 Self starting valved pulse jet |
| 02/09/1993 | CA1313457C Gas compressor for jet engine |
| 01/12/1993 | US5178922 For protecting wall to be submitted to ablative flow at high temperature, thermally insulative matrix, open-weave woven refractory material provided with meshes, refractory armature in form of fringed mat |
| 01/07/1993 | EP0521788A1 Pollution abating fuel burner for ramjet |
| 12/24/1992 | DE4120095A1 Pitot tube accelerator for projectile - has closed chamber formed in it contg. pressurised, combustible gas mixt. which can flow through projectile forming damming channel |
| 12/23/1992 | WO1992022742A1 A solid fuel ramjet engine for, e.g., a spin-stabilized projectile |
| 12/23/1992 | CA2111334A1 A solid fuel ramjet engine for, e.g., a spin-stabilized projectile |
| 12/22/1992 | US5172547 Electronic valve control for gas generator outflow |
| 12/01/1992 | US5167117 Method and apparatus for cooling an airplane engine |
| 11/24/1992 | US5165228 Turboramjet engine |
| 11/24/1992 | US5165227 Propelling nozzle for a hypersonic engine |
| 11/03/1992 | US5159809 Highly adaptable combined propulsion engine for an aircraft or a space-going airplane |
| 10/20/1992 | US5155992 Method and means for generating a force |
| 10/08/1992 | DE4110615A1 Nozzle for RAM jet engine - uses suction effect to exclude acceleration to high speed for engine start |
| 10/06/1992 | US5152136 Capable of increased and variable thrust for boost and final, or dash, phases of the mission |
| 09/22/1992 | US5148673 Integrated turboramjet engine |
| 09/22/1992 | US5148672 Pulse thruster |
| 08/13/1992 | DE4104134A1 Soln.-discharge system using pulsation instrument - disintegrates into fine mist forming thin coating for poison gas decontamination |
| 08/04/1992 | US5135184 Propellant utilization system |
| 07/14/1992 | US5129227 Low speed engine for supersonic and hypersonic vehicles |
| 06/30/1992 | US5125229 Nozzleless propulsion unit of low aspect ratio |
| 06/25/1992 | WO1992010661A1 Thrust nozzle for a rotating body |
| 06/17/1992 | DE4039910A1 Rohrartige vorrichtung, insbesondere fuer blattspitzenantriebe von helikoptern Tube-like device, in particular for blade tip drives helicopters |
| 06/16/1992 | US5121670 Ram accelerator |
| 06/09/1992 | US5119626 Combined turborocket and ramjet propulsion unit |
| 06/09/1992 | CA1302712C Autopyrolitic compositions for aerobic propulsion where the oxydant is an explosive |
| 05/21/1992 | DE4139338A1 Build-up jet drive unit - works with pulsation-controlled ignition-combustion to make start thrust possible, and has front hollow conical central body |
| 05/05/1992 | US5109670 Scramjet combustor |
| 04/21/1992 | US5105615 Turbojet engine with at least one axially movable arranged sliding valve |
| 04/14/1992 | US5103633 Scramjet combustor |
| 03/31/1992 | US5099764 Propulsion unit fireable from an enclosure |
| 03/24/1992 | US5097663 Scramjet combustor |
| 03/18/1992 | EP0474633A1 Controlling the flow ratio in a multiflow jet engine. |
| 03/12/1992 | DE4127994A1 Jet engine assisting in glider take=off - has front part of combustion chamber formed as backwardly open cover surface ofacute-angled hollow cone |
| 03/10/1992 | US5094071 Turboramjet engine |
| 03/10/1992 | US5094070 Propelling nozzle for a hypersonic jet plane |
| 02/27/1992 | DE4113976A1 Hyper-sonic aircraft engine - has speed matching of tangential blower rollers on drive turbine facilitated and noise radiation reduced |
| 02/04/1992 | US5085717 Generate reducing gases; smokeless |
| 02/04/1992 | US5085048 Scramjet including integrated inlet and combustor |
| 01/21/1992 | US5081831 Scramjet combustor |
| 01/09/1992 | DE4029279A1 Lightweight rocket propulsion aggregate - esp. for helicopter blade tip motor and operation using monergolic and/or hypergolic propellant and catalyst pack |
| 01/07/1992 | USH1008 Dump combustor with noncoherent flow |
| 01/07/1992 | USH1007 Solid fuel ramjet combustor |
| 12/31/1991 | US5076052 Blocking device for fan ramjet engines |
| 12/24/1991 | US5074118 Air turbo-ramjet engine |
| 12/19/1991 | DE4018747A1 Jet propulsion system for aircraft - has curved combustion chambers converting heat and explosion impulses directly into thrust |
| 12/17/1991 | US5072582 Scramjet combustor |
| 12/17/1991 | US5072581 Scramjet combustor |
| 11/26/1991 | US5067406 Supersonic, low-drag, solid fuel ramjet tubular projectile |
| 11/21/1991 | DE4117933A1 Gas turbine unit for hypersonic aircraft - has axial compressor and blower replaced by tangential blower |
| 11/12/1991 | US5063826 Armament system |
| 10/31/1991 | WO1991016535A1 Supercharged vapor pressure thermodynamic drive |
| 10/24/1991 | DE4012212A1 Hypersonic aircraft jet engine |