| Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699) |
|---|
| 09/01/1992 | US5143292 Cooled leaf seal |
| 09/01/1992 | US5142862 Thrust reversing system for high bypass fan engines |
| 09/01/1992 | CA1306872C Aircraft engine frame construction |
| 08/25/1992 | US5141159 Variable area nozzles for turbomachines |
| 08/25/1992 | US5141154 Variable throat convergent/divergent nozzle |
| 08/25/1992 | US5140809 Exhaust nozzle idle thrust spoiling method |
| 07/28/1992 | US5133182 Control of low compressor vanes and fuel for a gas turbine engine |
| 07/22/1992 | CN1017539B Flap support arrangement |
| 07/21/1992 | US5131222 Thermally valved cooling system for exhaust nozzle systems |
| 07/14/1992 | US5129447 Cooled bolting arrangement |
| 07/07/1992 | US5127602 Noise reduction kit for jet turbine engines |
| 07/01/1992 | EP0492864A1 Gas turbine combustor |
| 06/30/1992 | US5125796 Transition piece seal spring for a gas turbine |
| 06/25/1992 | WO1992010660A1 Thrust reverser for a propfan engine |
| 06/22/1992 | CA2056592A1 Multi-hole film cooled combustor liner with slotted film starter |
| 06/11/1992 | WO1992009988A1 Improvements in attenuators |
| 06/10/1992 | EP0489653A1 Seal joint between fuselage and segments of jet engine exhaust nozzle |
| 06/09/1992 | US5120005 Jet engine |
| 06/09/1992 | US5120004 Split door thrust reverser for fan jet aircraft engines |
| 06/03/1992 | EP0488453A1 Variable ejection nozzle for a jet engine |
| 06/02/1992 | US5117630 Pivoting door thrust reverser |
| 06/02/1992 | US5117628 Mixed flow augmentor pre-mixer |
| 05/29/1992 | CA2056054A1 Jet pipe propelling nozzle for jet engine and jet engine equipped with such nozzle particularly bypass type engine |
| 05/26/1992 | US5115979 Conforming plunger seal assembly |
| 05/20/1992 | EP0486226A1 Combustor liner with circumferentially angled film cooling holes |
| 05/20/1992 | EP0486133A1 Film cooled combustor liner for gas turbine |
| 05/16/1992 | CA2048726A1 Combustor liner with circumferentially angled film cooling holes |
| 05/12/1992 | US5111992 Variable throat convergent/divergent nozzle |
| 05/12/1992 | US5111550 Hinged fluid passage assembly |
| 05/05/1992 | US5110069 Single pivot overwing thrust reverser |
| 05/05/1992 | US5110050 Gas turbine engine nozzle |
| 05/05/1992 | US5110047 Vane-type nozzle(s) for varying the magnitude and direction of a thrust vector, and methods of operating same |
| 04/28/1992 | US5107675 Gas turbine engine |
| 04/22/1992 | CN1016374B Coolable thin metal sheet |
| 04/21/1992 | US5105615 Turbojet engine with at least one axially movable arranged sliding valve |
| 04/14/1992 | US5103639 Exhaust nozzle having variable contour exhaust flap |
| 04/14/1992 | US5103634 Thrust reversing system and method |
| 04/07/1992 | US5102050 Divergent flap actuation system for two-dimensional convergent - divergent turbojet exhaust nozzle |
| 04/07/1992 | US5102049 Vane control mechanism |
| 04/07/1992 | US5101624 Exhaust nozzle hinge |
| 04/07/1992 | US5101533 Vibration damping hinge joints for variable area jet engine exhaust nozzles |
| 04/02/1992 | WO1992005356A1 Turbojet thrust reverser with doors associated with an upstream panel |
| 04/01/1992 | CN1016083B Wall having cooling passage |
| 03/24/1992 | US5098022 Flow diverting nozzle for a gas turbine engine |
| 03/24/1992 | US5097662 Apparatus for influencing the flow of air through a passageway |
| 03/24/1992 | US5097661 Jet engine having a planar exit opening |
| 03/24/1992 | US5097656 Dual purpose apparatus for turbine engine exhaust noise and anti-surge air noise reduction |
| 03/17/1992 | US5096144 Reverser door actuation mechanism |
| 03/10/1992 | US5094071 Turboramjet engine |
| 03/10/1992 | US5094070 Propelling nozzle for a hypersonic jet plane |
| 03/05/1992 | WO1992003649A1 Axisymmetric nozzle with gimbled unison ring |
| 03/05/1992 | WO1992003648A1 Thrust vectoring exhaust nozzle |
| 03/03/1992 | USH1024 Thrust vectoring and reversing nozzle |
| 03/03/1992 | US5092525 Exhaust nozzle with reverser exhaust door mechanism |
| 03/03/1992 | US5092524 Nozzle throat disc for thrust vectoring |
| 03/03/1992 | US5092425 Jet noise suppressor and method |
| 02/25/1992 | US5090197 Pivoting door cascade thrust reverser |
| 02/25/1992 | US5090196 Ducted fan type gas turbine engine power plants |
| 02/25/1992 | CA1296309C Fluid dynamic pump |
| 02/18/1992 | US5088775 Seal ring with flanged end portions |
| 02/06/1992 | WO1992001891A1 Flame tube with a cooled supporting frame for a heat-resistant lining |
| 01/28/1992 | US5083426 Integrated engine shroud for gas turbine engines |
| 01/22/1992 | CN1015322B Method and linkage for positioning convergent flap and coaxial arc valve |
| 01/21/1992 | US5082293 High temperature, flexible, fiber-preform seal |
| 01/21/1992 | US5082209 Thrust reverser assembly |
| 01/21/1992 | US5082182 Thrust vectoring exhaust nozzle |
| 01/21/1992 | US5082181 Gas jet engine nozzle |
| 01/21/1992 | US5081835 Eccentric flap nozzle |
| 01/15/1992 | EP0466316A2 Gas turbine engine thrust reverser control |
| 01/14/1992 | US5080284 Cooling system for the trailing edge of a liner |
| 01/14/1992 | US5079915 Heat protective lining for a passage in a turbojet engine |
| 01/14/1992 | US5079912 Convergent side disk cooling system for a two-dimensional nozzle |
| 01/08/1992 | EP0464050A1 Fluid-tight joints. |
| 01/08/1992 | EP0442899A4 Vane-type thrust vectoring nozzle |
| 01/07/1992 | US5078412 Separately loaded strip seal |
| 01/07/1992 | US5077969 Cooled liner for hot gas conduit |
| 01/07/1992 | CA1293865C Wall having cooling passage |
| 12/31/1991 | US5076590 High temperature, flexible pressure-actuated, brush seal |
| 12/31/1991 | US5076512 Ventral segmented nozzles for promoting rapid temperature and pressure decay |
| 12/31/1991 | US5076496 Exhaust nozzle flap seal |
| 12/17/1991 | US5072580 System for operating gas turbine jet engine with fan damage |
| 12/10/1991 | US5070985 Coupling for a linear displacement transducer |
| 12/03/1991 | US5069034 Heat protective lining for an afterburner or transition duct of a turbojet engine |
| 11/28/1991 | WO1991018199A1 Variable cycle gas turbine engine for supersonic aircraft |
| 11/26/1991 | US5067324 Engine nozzle liner retainer |
| 11/21/1991 | EP0436685A4 An acoustic liner |
| 11/21/1991 | DE4114768A1 Ceramic heat shield for gas turbine flame tube - comprises number of blocks arranged next to one another clamped on cold side of holder |
| 11/21/1991 | DE4016052A1 Ceramic-fibre composite hot gas tube - with ceramic matrix formed from silicon polymer and fibres of inorganic materials or mixts., used for e.g. vehicle exhaust tube |
| 11/08/1991 | CA2039740A1 Exhaust assembly for a high speed civil transport aircraft engine |
| 11/06/1991 | EP0454696A1 Propelling nozzle. |
| 11/06/1991 | CN1014625B Temp. resistant fastener arrangement |
| 11/05/1991 | US5062588 Segmented rotatable nozzles |
| 10/29/1991 | US5060472 Insulated cooling liner |
| 10/29/1991 | US5060471 Jet engine noise reduction system |
| 10/24/1991 | DE4012212A1 Hypersonic aircraft jet engine |
| 10/22/1991 | US5059055 Mechanically attached liner hanger assembly |
| 10/22/1991 | US5058828 Overwing thrust reverser |
| 10/16/1991 | CN1014350B Segmented rigid sliding seal |
| 10/15/1991 | US5056307 Exhaust nozzle cooling utilizing total engine flow |
| 10/08/1991 | US5054998 Thrust reversing system for counter rotating propellers |