Patents
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
12/1990
12/25/1990US4979587 Jet engine noise suppressor
12/25/1990US4979362 Aircraft engine starting and emergency power generating system
12/13/1990WO1990015288A1 Apparatus for use in a fuel delivery system for a gas turbine engine
12/11/1990US4976585 System for the rapid balancing of revolving shafts, particularly suitable for gas turbines
12/11/1990US4976102 High bypass ratio gas turbine engine
12/06/1990CA2013594A1 Apparatus for use in a fuel delivery system for a gas turbine engine
12/05/1990CA2013933A1 Gas turbine powerplant
12/04/1990US4974638 Transition pipe for a jet pipe assembly of a turbojet engine
12/04/1990US4974416 Low coke fuel injector for a gas turbine engine
12/04/1990US4974413 Recuperative heat exchanger
12/04/1990US4974410 Inverted flight valve
12/01/1990CA2012248A1 Hybrid laminar flow nacelle
11/1990
11/29/1990WO1990014511A1 Aircraft engine starting and emergency power generating system
11/28/1990EP0399692A1 Gas turbine engine fuel control system with enhanced relight capability
11/28/1990EP0222769B1 Thermally balanced restraint system for a heat exchanger
11/27/1990US4973221 Gas turbine engine motor assembly
11/27/1990US4972672 Controlled bypass inlet duct
11/27/1990US4972671 Turbo-engine air intake grill
11/22/1990EP0398005A2 Pump
11/22/1990DE3916477A1 Removing fuel from injection nozzle - involves releasing compressed air from storage vessel
11/20/1990US4971336 Enhanced performance brush seals
11/20/1990US4971005 Fuel control utilizing a multifunction valve
11/20/1990CA1276474C Gas turbine drive with devices for branching off compressor air for cooling hot parts
11/14/1990EP0397566A1 Heat insulation structure for an afterburner liner or turbine transition piece
11/14/1990EP0397041A2 Rotary hydraulic pump
11/14/1990EP0396736A1 Sustainer propulsion system
11/14/1990EP0396554A1 Burner.
11/13/1990US4969326 Hoop shroud for the low pressure stage of a compressor
11/07/1990CN1046783A System for supporting rotor in axial exhaust turbine with exhaust end bearing having isotropic stiffness and directly connected to foundation
11/07/1990CN1046782A System for supporting rotor of axial exhaust turbine with exhaust end bearing being integrated in foundation
11/06/1990US4967561 Combustion chamber of a gas turbine and method of operating it
11/06/1990US4967552 Method and apparatus for controlling temperatures of turbine casing and turbine rotor
10/1990
10/31/1990EP0395110A1 Rotor support structure for a turbine with an axial outlet, the bearing at the outlet side being integrated in the foundation
10/31/1990EP0394899A1 Rotor support structure for a turbine with an axial outlet, the bearing at the outlet side being directly and isotropically fastened to the foundation
10/31/1990EP0394481A1 Gas turbine generator
10/30/1990US4966065 Multiplexed hydraulic control systems
10/30/1990US4965995 Power unit with stored energy
10/30/1990US4965994 Jet engine turbine support
10/25/1990DE3940424A1 Dichtung fuer eine axialsymmetrische strahlumlenkungsschubduese Gasket for an axisymmetric strahlumlenkungsschubduese
10/24/1990EP0393283A1 A ducted fan gas turbine engine with a spinner.
10/24/1990CN1046371A Axisymmetric vectoring exhaust nozzle seal
10/23/1990US4964844 Gearbox arrangement for driving coaxial contra rotating multi-bladed rotors
10/23/1990US4964315 Transmission having dual counterrotating output shafts
10/23/1990US4964270 Gas turbine engine fuel system
10/18/1990WO1990012205A1 Dual range air turbine starter
10/18/1990WO1990012204A1 High performance turbine engine
10/18/1990WO1990012168A1 Sound attenuating laminate and installation for jet aircraft engines
10/17/1990EP0392664A2 Cooled turbine blade and combined cycle power plant having gas turbine with this cooled turbine blade
10/17/1990EP0392527A1 Combined turbo/ramjet engine
10/17/1990EP0392520A1 Turbo-ram jet
10/17/1990EP0392401A1 Flow control device for fanjet/ramjet engine
10/17/1990EP0391935A1 Sound attenuation system for jet aircraft engines
10/17/1990CN1010041B Dual entry radial turbine gas generator
10/16/1990US4962889 Airblast fuel injection with adjustable valve cracking pressure
10/16/1990CA1275176C Cooling air manifold for a gas turbine engine
10/11/1990CA2013934A1 Axisymmetric vectoring exhaust nozzle seal
10/11/1990CA2010151A1 Power turbine ventilation system
10/10/1990EP0391610A1 Fuel control valve for an aircraft gas turbine engine fuel system
10/10/1990EP0391609A1 Management of heat generated by aircraft gas turbine installations
10/10/1990EP0391288A2 Pumping apparatus
10/10/1990EP0391082A2 Improved efficiency combined cycle power plant
10/09/1990US4961312 Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
10/09/1990US4961309 Apparatus for venting the rotor structure of a compressor of a gas turbine power plant
10/04/1990WO1990011440A1 Combustion heated air turbine starter system
10/03/1990CN1045842A Single spool, two-stage high performance compress unit
10/03/1990CA2013642A1 Efficiency combined cycle power plant
10/02/1990US4960085 Pneumatic and electro-pneumatic starters
10/02/1990US4959954 Gas turbine system and method of controlling the same
09/1990
09/30/1990CA2012304A1 Dual range air turbine starter
09/26/1990EP0389353A1 Support for the low pressure rotor of a two-spool turbomachine
09/26/1990EP0388527A1 Improved titanium aluminide alloys
09/25/1990US4958489 Means for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
09/25/1990CA1274403A1 Transmission having dual counter-rotating output shafts
09/20/1990CA2010672A1 Titanium aluminide alloys
09/19/1990EP0388046A2 Gas turbine engine fuel control system, and metering valve
09/19/1990CN1045442A System and method for cooling in gas turbine
09/12/1990EP0387123A1 Thermic protection liner for hot pipe of turbo-jet engine
09/12/1990EP0386486A1 Titanium alloy component with a protection layer
09/12/1990EP0386200A1 Guide vane assembly for auxiliary power unit
09/12/1990EP0386028A1 Torch igniters.
09/11/1990US4955201 Fuel injectors for turbine engines
09/07/1990WO1990010147A1 Bypass valve and visual indicator for a fuel system
09/05/1990EP0385294A1 Turbojet
09/05/1990EP0385046A2 Fuel transfer system for aircraft
09/05/1990CN1045157A Lourver dampers for use in gas turbines exhaust systems and having blades protected against becoming warped
09/05/1990CN1009476B Fuel nozzle guide structure and retainer for gas turbine engine
09/05/1990CN1009475B Process for manufacturing cooling film device of combustion chambers of turbomachines, and products
08/1990
08/29/1990EP0384336A1 A method and equipment for converting thermal energy into mechanical energy
08/28/1990US4951460 Apparatus and method for optimizing the air inlet temperature of gas turbines
08/28/1990CA1273212A1 Fuel and oil heat management system for a gas turbine engine
08/22/1990EP0383186A1 Guillotine dampers with blade sealing means accommodative of thermal expansion forces
08/22/1990EP0383185A1 Louver dampers for use in gas turbines exhaust systems and having blades protected against becoming warped
08/22/1990EP0382907A2 Capacitive discharge ignition exciter using SCR discharge switches
08/22/1990CN1044845A Guillotine dampers with blade sealing means accommodative of thermal expansion forces
08/21/1990US4949544 Series intercooler
08/21/1990US4949538 Combustor gas feed with coordinated proportioning
08/16/1990EP0382585A1 Nickel-based superalloy for industrial turbine blades
08/16/1990EP0382377A1 Fuel supply apparatus
08/16/1990EP0381755A1 High pressure intercooled turbine engine
08/14/1990US4948055 Fuel injector