| 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) |
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| 05/23/1989 | US4831700 Method for making a fuel injector |
| 05/18/1989 | WO1989004439A1 Burner |
| 05/16/1989 | US4830519 Annular seal assembly |
| 05/16/1989 | US4829763 Process for producing power |
| 05/11/1989 | DE3735908A1 Fuel cooling system for high-performance aircraft |
| 05/10/1989 | EP0315486A2 Aircraft engine frame construction |
| 05/10/1989 | EP0315485A2 Gas-cooled flameholder assembly |
| 05/10/1989 | CN1032839A Shut off and pressure regulating valve |
| 05/09/1989 | US4827723 Integrated gas turbine power generation system and process |
| 05/09/1989 | US4827716 Dual function gas generation system for on board installation on turbine powered aircraft |
| 05/09/1989 | US4827714 Gas turbine fuel control system |
| 05/05/1989 | WO1989003960A1 Torch igniters |
| 05/05/1989 | WO1989003763A1 Sound attenuation system for jet aircraft engines |
| 05/03/1989 | EP0313826A1 Axial gas turbine |
| 05/03/1989 | DE3833279A1 Brennstoffduese fuer gasturbinen Fuel nozzle for gas turbines |
| 05/02/1989 | US4826403 Turbine |
| 05/02/1989 | US4825658 Base metal catalyst |
| 05/02/1989 | US4825648 Turbofan engine having a split cowl |
| 05/02/1989 | US4825645 Power turbine and reduction gear assembly |
| 05/02/1989 | US4825643 Gas turbine propulsion unit with devices for branching off compressor air for cooling of hot parts |
| 05/02/1989 | US4825640 Combustor with enhanced turbine nozzle cooling |
| 05/02/1989 | US4825638 Method of and device for recovering heat energy of hot raw gas gererated a coal gasification arrangement of an electric energy generating plant |
| 05/02/1989 | CA1253350A1 Gas turbine engine |
| 04/26/1989 | EP0313464A1 Transition channel for a jet engine |
| 04/26/1989 | EP0313194A1 Interturbine duct |
| 04/19/1989 | EP0236336B1 A changeable cooling control system for a turbine shroud and rotor |
| 04/18/1989 | US4821520 Turbocharger protector screen |
| 04/18/1989 | US4821506 Radial turbine with variable axial nozzle |
| 04/13/1989 | DE3818779A1 Brennstoffverteilungseinrichtung Fuel distribution facility |
| 04/12/1989 | EP0311514A1 Fixed and centrally attached fairing for a jet engine and jet engine with this equipment |
| 04/12/1989 | CN1003879B Cooling scheme for combustor vane interface |
| 04/11/1989 | US4821216 Multifunction meter for use in an aircraft |
| 04/11/1989 | US4820117 Crossed I-beam structural strut |
| 04/11/1989 | US4820116 Turbine cooling for gas turbine engine |
| 04/11/1989 | US4819423 Integrated power unit |
| 04/11/1989 | CA1252353A1 Method and apparatus for removing noncondensable gases from cogenerated process steam in dual fluid cheng cycle engines |
| 04/06/1989 | WO1989003001A1 Fabric expansion joints for exhaust systems of gas turbines |
| 04/05/1989 | EP0309485A1 Wide range gaseous fuel combustion system for gas turbine engines. |
| 04/04/1989 | US4818178 Process for cooling the blades of thermal turbomachines |
| 04/04/1989 | US4817756 Quiet nacelle system and hush kit |
| 04/04/1989 | US4817389 Fuel injection system |
| 03/29/1989 | EP0309267A1 Heat exchanger processes |
| 03/28/1989 | US4815928 Airflow for turbine blades in a gas turbine aircraft engine |
| 03/28/1989 | US4815281 Air take-off for a turbojet engine cold flow duct |
| 03/28/1989 | US4815277 Integrated power unit |
| 03/28/1989 | US4815273 Single propeller turboprop propulsion apparatus |
| 03/28/1989 | US4815272 Turbine cooling and thermal control |
| 03/21/1989 | US4813229 Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas |
| 03/21/1989 | US4813228 Gas turbine |
| 03/21/1989 | US4813227 Preheat gas turbine combined with steam turbine |
| 03/16/1989 | DE3829908A1 Multipurpose gas turbine |
| 03/15/1989 | EP0307264A1 Fuel distribution circuit affording enhanced fuel cooling |
| 03/15/1989 | EP0167587B1 Combined engine-starter and accessory drive system |
| 03/15/1989 | EP0146624B1 Process of intensification of the thermoenergetical cycle and air jet propulsion engines |
| 03/14/1989 | US4811919 Volume compensated fluid mount |
| 03/14/1989 | CA1251050A1 Gas turbine power plant |
| 03/08/1989 | EP0306176A1 Improvements relating to liquid pumps |
| 03/08/1989 | EP0305763A1 Energy-delivering installation |
| 03/07/1989 | US4810677 Heat-insulating lining for a gas turbine |
| 03/07/1989 | CA1250750A1 Aircraft engine inlet |
| 03/02/1989 | DE3727608A1 Supersonic aircraft |
| 03/01/1989 | EP0304827A1 Power regulation for a combined plant |
| 03/01/1989 | EP0236337B1 Seal ring means for a bladed rotor assembly |
| 02/28/1989 | US4808073 Method and apparatus for cooling a high pressure compressor of a gas turbine engine |
| 02/28/1989 | US4807433 Gas turbine engine |
| 02/28/1989 | CA1250439A1 Gas turbine engine carburetor |
| 02/22/1989 | CN2033059U Changable diffuser |
| 02/21/1989 | US4805873 Control device for a starter valve of a turbine aero-engine |
| 02/21/1989 | US4805658 Metering the weight flow of fuel to a gas turbine engine |
| 02/21/1989 | US4805398 Turbo-machine with device for automatically controlling the rate of flow of turbine ventilation air |
| 02/14/1989 | US4803836 Method and apparatus for feeding an extrudable fuel to a pressurized combustion chamber |
| 02/08/1989 | EP0302669A2 Volume compensated fluid mount |
| 02/08/1989 | EP0302508A1 Energy-delivering installation |
| 02/08/1989 | CN1030968A Surge control for compressor |
| 02/07/1989 | US4802821 Axial flow turbine |
| 02/07/1989 | US4802334 Augmentor fuel system |
| 02/01/1989 | EP0301993A2 A surge control for a compressor |
| 01/31/1989 | US4800717 Turbine rotor cooling |
| 01/26/1989 | DE3824121A1 Gas turbine |
| 01/24/1989 | US4799787 Optical fibre radiation pyrometer |
| 01/24/1989 | US4799354 Turbopropeller or turbofan gas turbine engine |
| 01/17/1989 | US4798406 Modified friction locking ring |
| 01/17/1989 | US4798047 Power recovery expander for use with a stream of hot gas |
| 01/17/1989 | CA1248842A1 Flow dividing valve |
| 01/11/1989 | EP0298941A1 Method for destructing undesired organic substances |
| 01/11/1989 | EP0298898A2 Crossed I-beam structural strut |
| 01/11/1989 | EP0298897A2 Stiffening ring for a stator assembly of an axial flow rotary machine |
| 01/11/1989 | EP0298637A2 Rotary pump system |
| 01/11/1989 | EP0145738B1 Centrifugal pump |
| 01/10/1989 | US4796424 Intake for a turbopropeller gas turbine engine |
| 01/10/1989 | CA1248420A1 Coated superalloy gas turbine components |
| 01/10/1989 | CA1248358A1 Optical pyrometer sight tube assembly for controlling a gas turbine |
| 01/04/1989 | EP0298014A1 Engine modularity |
| 01/04/1989 | EP0298011A1 Nose cowl mounted oil lubricating and cooling system |
| 01/04/1989 | EP0297672A2 Turbo-compressor having air cooled bearing |
| 01/03/1989 | US4795307 Method and apparatus for optimizing the vane clearance in a multi-stage axial flow compressor of a gas turbine |
| 01/03/1989 | US4794754 For a gas turbine |
| 12/28/1988 | EP0296314A2 Self cleaning filter for gases with preliminary separator for dust |
| 12/28/1988 | CA1247380A Actuator for variable vanes |
| 12/27/1988 | US4793772 Method and apparatus for cooling a high pressure compressor of a gas turbine engine |