| Patents for F02K 99 - Subject matter not provided for in other groups of this subclass (464) |
|---|
| 09/30/2008 | US7429018 Variable fluid intake with ramp and inflatable bag |
| 09/18/2008 | US20080223978 Variable fluid intake with ramp and inflatable bag |
| 08/21/2008 | DE10300621B4 Strahlantriebsverfahren zB für ein Segelflugzeug Jet propulsion methods, eg for a glider |
| 08/19/2008 | US7412831 Integral cooling system for rotary engine |
| 08/07/2008 | WO2008094696A1 Rotary heat engine powered by radiant energy |
| 07/30/2008 | EP1948921A2 Methods and apparatus for a fluid inlet |
| 06/11/2008 | EP1928734A1 Cooling system for an aircraft, aircrft comprising the cooling system and cooling method |
| 05/27/2008 | US7377099 System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle |
| 05/20/2008 | US7373774 Enhanced performance torroidal coolant-collection manifold |
| 05/08/2008 | WO2007051137A3 Methods and apparatus for a fluid inlet |
| 05/02/2008 | WO2008031394A3 Measuring arrangement for detecting a rotary momentum of an engine rotor, and associated method |
| 04/30/2008 | EP1915564A2 Fluid line assembly |
| 03/27/2008 | DE102006043283A1 Messanordnung zur Erfassung eines 1/Umdrehungsimpulses eines Triebwerkrotors sowie Verfahren hierzu Measuring arrangement for detecting a 1 / rotary momentum of an engine rotor and method therefor |
| 03/20/2008 | WO2008031394A2 Measuring arrangement for detecting a rotary momentum of an engine rotor, and associated method |
| 03/19/2008 | EP1784557B1 Fluid injection in a gas turbine during a cooling down period |
| 03/13/2008 | US20080060345 Gas turbine system |
| 03/12/2008 | EP1898066A2 Gas turbine system |
| 03/12/2008 | CN100374706C Process for replacing an abradable on the fan case of a turbojet |
| 03/06/2008 | WO2007051137A8 Methods and apparatus for a fluid inlet |
| 03/04/2008 | US7337875 High admittance acoustic liner |
| 02/27/2008 | CN100371580C Long service life jet deflection plate for turbine jet motor of aircraft |
| 02/19/2008 | US7331421 Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods |
| 01/29/2008 | US7322195 Acoustic dampers |
| 01/24/2008 | WO2007092649A3 Rotary heat engine |
| 01/24/2008 | US20080016846 System and method for cooling hydrocarbon-fueled rocket engines |
| 12/04/2007 | US7302794 Rocket engine member and a method for manufacturing a rocket engine member |
| 11/20/2007 | US7296656 Acoustic mechanical retainer |
| 11/20/2007 | US7296655 Duct liner acoustic splice |
| 11/13/2007 | US7293403 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
| 11/01/2007 | US20070251210 Liquid Injection in a Gas Turbine During a Cooling Down Phase |
| 10/18/2007 | WO2006057653A3 Integrated air inlet system for multi-propulsion aircraft engines |
| 10/18/2007 | US20070240427 Compact compound engine package |
| 10/18/2007 | US20070240416 Integral cooling system for rotary engine |
| 10/09/2007 | US7278208 Method of replacing an abradable portion on the casing on a turbojet fan |
| 10/04/2007 | WO2007001371A3 Vibration isolation engine mount system and method for ducted fan aircraft |
| 08/16/2007 | WO2007092649A2 Rotary heat engine |
| 07/12/2007 | WO2006137857A3 Vertical or short take off and landing vehicle |
| 07/05/2007 | US20070151226 Rotary heat engine |
| 06/28/2007 | US20070144142 Outlet nozzle and a method for manufacturing an outlet nozzle |
| 06/26/2007 | US7234294 Outlet nozzle and a method for manufacturing an outlet nozzle |
| 05/18/2007 | WO2007035124A3 Plasma vehicle engine |
| 05/16/2007 | EP1784557A1 Fluid injection in a gas turbine during a cooling down period |
| 05/15/2007 | US7216474 Integrated air inlet system for multi-propulsion aircraft engines |
| 05/09/2007 | EP1781925A2 Propulsion device with enclosed plenum |
| 05/03/2007 | WO2007051137A2 Methods and apparatus for a fluid inlet |
| 05/03/2007 | WO2007001371A9 Vibration isolation engine mount system and method for ducted fan aircraft |
| 05/03/2007 | US20070095048 Propulsion device with enclosed plenum |
| 04/24/2007 | US7207520 System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines |
| 04/19/2007 | WO2007020504A3 Fluid line assembly |
| 03/29/2007 | WO2007035141A1 Cooling system for an aircraft, aircrft comprising the cooling system and cooling method |
| 03/29/2007 | WO2007035124A2 Plasma vehicle engine |
| 03/08/2007 | US20070051404 Fluid line assembly |
| 02/22/2007 | WO2007020504A2 Fluid line assembly |
| 01/25/2007 | US20070018038 Engine heat exchanger with thermoelectric generation |
| 01/24/2007 | EP1746257A2 Vehicle and corresponding operating method |
| 01/23/2007 | US7165388 Propulsion device with enclosed plenum |
| 01/19/2007 | CA2551767A1 Engine heat exchanger with thermoelectric generation |
| 01/04/2007 | WO2007001371A2 Vibration isolation engine mount system and method for ducted fan aircraft |
| 12/28/2006 | WO2006137857A2 Vertical or short take off and landing vehicle |
| 12/06/2006 | EP1729234A1 Method for designing streamline traced, mixed compression inlets for aircraft engines |
| 11/30/2006 | US20060266412 System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines |
| 11/30/2006 | US20060266016 System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle |
| 11/29/2006 | EP1726811A2 System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle |
| 11/09/2006 | US20060248873 Vibration isolation engine mount system and method for ducted fans |
| 11/09/2006 | DE202006008158U1 Propeller-power machine e.g. gas turbine, for airplane`s drive system, has combustion chamber placed between compressor and pressure reducer stages having propeller plant with main and adjacent rotors having circular arcs and epicycloids |
| 11/08/2006 | EP1718857A2 Integrated air inlet system for multi-propulsion aircraft engines |
| 10/26/2006 | US20060237261 Acoustic mechanical retainer |
| 10/26/2006 | US20060237260 Duct liner acoustic splice |
| 10/25/2006 | EP1715172A2 Acoustic liner assembly and corresponding fabrication method |
| 10/25/2006 | EP1715158A2 Duct liner acoustic splice |
| 10/25/2006 | EP1714871A2 Acoustic dampers |
| 10/24/2006 | US7124856 Acoustic liner for gas turbine engine |
| 10/22/2006 | CA2537643A1 Dust liner acoustic splice |
| 10/22/2006 | CA2536583A1 Acoustic mechanical retainer |
| 10/19/2006 | US20060231329 Acoustic dampers |
| 10/12/2006 | US20060225404 Vertical or short take off and landing vehicle |
| 10/05/2006 | US20060219475 Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods |
| 10/05/2006 | US20060219191 Heat transfer enhancement features for a tubular wall combustion chamber |
| 09/28/2006 | US20060213179 Subsonic diffuser |
| 09/21/2006 | US20060207827 Support means for an acoustic liner used in an auxiliary power unit exhaust muffler |
| 09/13/2006 | EP1701028A2 Acoustic liner with a nonuniform depth backwall |
| 09/05/2006 | US7100368 Drive device for a secondary air injection system |
| 08/17/2006 | DE19748795B4 Endoskop Endoscope |
| 08/03/2006 | US20060169533 Acoustic liner with a nonuniform depth backwall |
| 07/18/2006 | US7078886 Appliance for reading identification connectors |
| 07/11/2006 | US7073319 Nuclear-fueled power generating system |
| 06/07/2006 | EP1352170B1 Rocket engine member and a method for manufacturing a rocket engine member |
| 06/01/2006 | WO2006057653A2 Integrated air inlet system for multi-propulsion aircraft engines |
| 05/30/2006 | US7051513 Rocket engine tubular chamber with single piece jacket |
| 05/25/2006 | US20060107648 Integrated air inlet system for multi-propulsion aircraft engines |
| 03/28/2006 | US7017333 Wall structure |
| 03/02/2006 | WO2006021520A1 Injection of liquid into a gas turbine during a cooling phase |
| 03/01/2006 | EP1630356A1 Fluid injection in a gas turbine during a cooling down period |
| 02/23/2006 | DE102004038039A1 Raketenmotor Rocket motor |
| 02/08/2006 | EP1624178A1 Rocket motor |
| 02/07/2006 | US6993898 Microwave heat-exchange thruster and method of operating the same |
| 02/02/2006 | WO2006011978A2 Propulsion device with enclosed plenum |
| 01/19/2006 | US20060011408 Acoustic liner for gas turbine engine |
| 01/12/2006 | US20060005528 Propulsion device with enclosed plenum |
| 01/04/2006 | EP1612769A2 High admittance acoustic liner |