| 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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| 02/21/2012 | US8117828 Constant volume combustor having a rotating wave rotor |
| 02/16/2012 | DE102010034848A1 Dual fuel engine, particular position-control power unit, is based on cryogenic liquefied gases, where ignition device has catalytic converter in form of electrically heated cartridge made of ceramic or metallic material |
| 02/02/2012 | WO2011156923A3 Multitube valveless pulse detonation engine |
| 02/01/2012 | CN202132128U 多级热冲压发动机 Multi-stage heat ramjet |
| 02/01/2012 | CN202132112U Compressed air backflow compression system |
| 02/01/2012 | CN202132101U 动力流体气体工质压缩系统 Dynamic fluid refrigerant gas compression system |
| 01/26/2012 | WO2012011830A1 Device for transmitting a detonation |
| 01/19/2012 | WO2011104685A3 Rotary type internal combustion engine |
| 01/12/2012 | WO2012003706A1 Supersonic rotor engine |
| 01/11/2012 | CN102313274A Low-entropy mixed combustion high supercritical thermodynamic system |
| 01/11/2012 | CN101806260B Multitube parallel pulse detonation combustion chamber and ignition detonation method thereof |
| 01/10/2012 | US8091336 Method to initiate multiple chamber detonation wave combustors |
| 01/04/2012 | EP1745207B1 Pulse jet engines |
| 01/04/2012 | CN102305153A Novel heat engine |
| 12/28/2011 | EP2400137A2 Rotating ram-jet turbine with exhaust turbocharger |
| 12/28/2011 | CN202092094U 低熵混燃高超临界热动力系统 Co-firing a superb low entropy critical thermal power systems |
| 12/27/2011 | US8082728 System and method of continuous detonation in a gas turbine engine |
| 12/22/2011 | DE102010024329A1 Super sonic combustion ramjet-thruster for hypersonic aircraft, has fuel supplying unit provided with fuel outlet openings, where distance of fuel supplying unit is adjusted at thruster inlet along longitudinal axis of thruster |
| 12/22/2011 | CA2803247A1 Multitube valveless pulse detonation engine |
| 12/21/2011 | CN102288070A 气体延迟反冲方法 Gas delayed recoil method |
| 12/21/2011 | CN101691201B 一种基于微燃烧产生电能和推力的新型动力装置 A new micro-burning power plant to produce electricity and thrust based |
| 12/20/2011 | US8079308 Ramjet engine incorporating a tubular structure and a missile propelled by a ramjet engines of this type |
| 12/15/2011 | WO2011155248A1 Engine |
| 12/15/2011 | US20110302908 Multitube valveless pulse detonation engine |
| 12/14/2011 | CN202073656U 一种水下气液两相发动机 Underwater gas-liquid two-phase engine |
| 12/14/2011 | CN102278233A 超音速转子发动机 Supersonic rotary engine |
| 12/14/2011 | CN102278232A 改进的超燃燃烧室及其旋流器的设计方法 Improved supersonic combustion chamber and cyclone design method |
| 12/07/2011 | EP2391802A1 Jet engine, in particular a jet engine for an aircraft |
| 12/07/2011 | CN1784574B 截流涡流式燃烧器 Closure vortex burner |
| 11/30/2011 | CN202053881U 增程式空气动力汽车 Increase aerodynamic car program |
| 11/23/2011 | CN102251880A Underwater gas-liquid two-phase engine |
| 11/16/2011 | CN202039972U Turbo-ramjet combination engine on basis of detonating combustion |
| 11/10/2011 | WO2011139339A1 Propulsion system and method |
| 11/10/2011 | WO2011041822A8 Optimal feedback heat energy internal combustion engine and its applications |
| 11/09/2011 | CN102235268A Flywheel turbine |
| 11/03/2011 | DE102010018928A1 Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form |
| 11/02/2011 | CN202023655U Pulse detonation engine with ejector |
| 11/02/2011 | CN202023654U Particle engine |
| 11/02/2011 | CN102230428A Aviation jet engine |
| 10/27/2011 | WO2011131493A2 Air breathing reaction propulsion engine |
| 10/20/2011 | WO2011127901A1 Multi-shaft engine having a tandem generator |
| 10/05/2011 | CN202001139U Stamping engine with pneumatic turbine |
| 09/28/2011 | CN102200074A Stow abort mechanism for a ram air turbine |
| 09/22/2011 | WO2011113306A1 Gas piston pulse engine |
| 09/21/2011 | CN102192045A Stamping type rotor fan engine |
| 09/14/2011 | EP2365250A1 Partial filling of a pulse detonation combustor in a pulse detonation combustor based hybrid engine |
| 09/13/2011 | US8015795 Aircraft combination engines plural airflow conveyances system |
| 09/08/2011 | US20110214409 Combustion Turbine in which Combustion is Intermittent |
| 09/07/2011 | EP2363588A2 Pulse detonation system for a gas turbine |
| 09/07/2011 | CN101749142B Integrated burner with back step precombustion stage and V-groove main combustion stage |
| 09/04/2011 | CA2732899A1 Pulse detonation system |
| 09/01/2011 | WO2011104685A2 Rotary type internal combustion engine |
| 08/24/2011 | CN102165168A Combustion turbine in which combustion is intermittent |
| 08/24/2011 | CN101368510B Cut-spraying type engine |
| 08/17/2011 | CN102155331A Turboramjet combined engine based on knocking combustion |
| 08/17/2011 | CN102155292A Fan-type one-stroke engine |
| 08/16/2011 | US7997081 Gas delivery system |
| 08/10/2011 | CN102146858A Stamping engine for pneumatic turbine |
| 08/03/2011 | EP2350445A2 Method and system for altering engine air intake geometry |
| 07/28/2011 | WO2010145641A3 Water jet pump type drive, in particular for a flying object |
| 07/28/2011 | US20110180145 Tailorable Stiffness Shape Morphing Flow-Path |
| 07/21/2011 | WO2011056193A3 A method of controlling engine performance |
| 07/21/2011 | US20110173985 Thruster comprising a plurality of rocket motors |
| 07/21/2011 | DE102010005039A1 Supersonic-adjustment-segment-nozzle for use as injector-drive nozzle for injector-centrifugal-turbine-engine of motor vehicles, has main nozzle with multiple segment-nozzles in form of nozzle pockets |
| 07/20/2011 | CN201902267U Detonation tube structure of multi-tube pulse detonation engine |
| 07/14/2011 | WO2011041049A3 Internally nested variable-area fuel nozzle |
| 07/14/2011 | US20110167787 Pulse jet engine |
| 07/13/2011 | CN201896675U Combined detonation chamber of pulse detonation engine |
| 07/13/2011 | CN201896674U Intake cone of air-breathing pulse detonation engine |
| 07/13/2011 | CN102121435A Particle engine |
| 07/06/2011 | CN102116216A Hybrid detonation rotor shaft (all-electric) intelligent engine |
| 06/30/2011 | WO2011078740A1 Method for generating thrust for a vehicle |
| 06/29/2011 | EP2339160A2 Pulse detonation turbine engine |
| 06/23/2011 | US20110146286 Self-starting turbineless jet engine |
| 06/22/2011 | EP2336523A2 Pulse detonation system with fuel lean inlet region |
| 06/21/2011 | US7963100 Cooling system for high-speed vehicles and method of cooling high-speed vehicles |
| 06/15/2011 | EP2333279A2 Rotating valve assembly for high temperature and high pressure operation |
| 06/15/2011 | CN201865787U Flywheel machine |
| 06/14/2011 | CA2523495C Trapped vortex combustor |
| 06/14/2011 | CA2426906C Rotary ramjet engine |
| 06/08/2011 | CN201858045U Detonation tube of high-frequency pulse detonation engine |
| 06/08/2011 | CN102086822A Power plant of water surface ship |
| 06/07/2011 | US7954329 Statically-operating ejector ramjet |
| 06/02/2011 | US20110126510 Pulse detonation combustor |
| 06/01/2011 | EP2326815A1 Combustion turbine in which combustion is intermittent |
| 06/01/2011 | CN201851228U Engine of rocket |
| 05/31/2011 | US7950235 Jet engine |
| 05/30/2011 | CA2721530A1 Thrust modulation in a multiple combustor pulse detonation engine using cross-combustor detonation initiation |
| 05/18/2011 | CN201835941U Delayed ignition controller of pulse engine |
| 05/18/2011 | CN102062018A Durable pulse-type stamping jet engine technology |
| 05/17/2011 | US7945353 Adaptive control in the presence of input constraints |
| 05/12/2011 | WO2011056193A2 A method of controlling engine performance |
| 05/12/2011 | US20110107738 Combined Cycle Integrated Combustor and Nozzle System |
| 05/11/2011 | CN102052254A Power generator utilizing wind energy and fuel chemical energy |
| 05/10/2011 | US7937945 Combining a series of more efficient engines into a unit, or modular units |
| 05/05/2011 | US20110100014 Hybrid propulsive engine including at least one independently rotatable propeller/fan |
| 05/04/2011 | CN201818392U Swirl ramjet engine |
| 05/04/2011 | CN201818358U Fluid gas-phase working medium compression system |
| 05/04/2011 | CN102046954A Subsonic and stationary ramjet engines |
| 05/04/2011 | CN102042121A Detonation tube structure of multi-tube pulse detonation engine |