140367 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto; Other construction of jet pipes; Couplings or connections Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
ASSEMBLY FOR A TURBINE ENGINE
#2SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#3VARIABLE AREA NOZZLE ASSEMBLY
#4TURBINE ENGINE TURBINE ASSEMBLY
#5COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE
#6EXHAUST NOZZLE ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEM
#7Seal system using layers of seal segments forced into sealing engagement using tension cable
#8BONDED DOUBLE WALL SEAL ASSEMBLY
#9APPARATUS TO PREVENT AIR LEAKAGE IN TURBINE ENGINES
#10Thrust reverser for the nacelle of an aircraft turbofan engine
#11Cowl seal assembly for an aircraft propulsion system
#12Sealing assembly for a turbine ejection cone
#13Variable area nozzle for aircraft propulsion system
#14Plunger seal apparatus and sealing method
#15Plunger seal assembly and sealing method
#16BONDED DOUBLE WALL SEAL ASSEMBLY
#17Flexurally actuated self-sealing plunger apparatus
#18Skirted leaf seal apparatus
#19SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#20Exterior nozzle member for a turbomachine
#21Aircraft turbojet engine comprising two thrust reverser modules
#22Aircraft seal
#23Sealing joint for aircraft turbojet engine nacelle
#24Aircraft propulsion system nozzle with internal flow passage
#25Structural panel with integrated coupler
#26Attitude control and thrust boosting system and method for space launchers
#27Nozzle and apparatus for cooling jet engine for maintenance and method for maintenance of jet engine
#28Flexible seal for gas turbine engine
#29Fire resistance device intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment
#30Variable area fan nozzle for turbofan aircraft engine
#31Ceramic seal component for gas turbine engine and process of making the same
#32Rear assembly of a turbojet engine nacelle including a fireproof sealing device
#33AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA
#34Exhaust liner deflection limiter
#35Seal system for variable geometry gaps in aircraft systems
#36Non-metallic engine case inlet compression seal for a gas turbine engine
#37Seal interface with a deflection control feature
#38Ceramic seal component for gas turbine engine and process of making the same
#39Methods and apparatus for sealing variable area fan nozzles of jet engines
#40Composite piston ring seal for axially and circumferentially translating ducts
#41Methods of replacing seals in exhaust frames of turbine systems and related components
#42High temperature seals for blanketless inner fixed structure
#43Seals for a gas turbine engine
#44Hinged seal using wire mesh
#45Coated thermoplastic seal retainer for fire seal test
#46Nacelle thrust reverser
#47Bulb seal and spring
#48Thrust reverser compression rod with spring biased engagement
#49Seal assembly
#50Dielectric seal device
#51Gas turbine engine convergent/divergent exhaust nozzle divergent seal with preloaded dovetail interface background
#52Jet engine with multiple chambers and a bearing chamber support
#53Fire seal for use with a gas turbine engine
#54Gas turbine engine with stream diverter
#55Thrust reverser with forward positioned blocker doors
#56Composite piston ring seal for axially and circumferentially translating ducts
#57Seals for a gas turbine engine
#58NACELLE WITH A THRUST REVERSER DEVICE WITH MAINTAINED MOVEABLE CASCADES
#59Sealing system for variable area fan nozzle
#60Seal for a thrust reverser of a turbojet engine nacelle
#61Large displacement high temperature seal
#62Combustion gas discharge nozzle for a rocket engine provided with a sealing device between a stationary part and a moving part of the nozzle
#63Hinged seal using wire mesh
#64Actively controlled cooling air exhaust door on an aircraft engine nacelle
#65Castellated latch mechanism for a gas turbine engine
#66Center body attachment system
#67Gas turbine engine convergent/divergent exhaust nozzle divergent seal with dovetail interface
#68Divot for blocker doors of thrust reverser system
#69PASSIVE TANGENTIAL EJECTOR FOR AN EXHAUST NOZZLE OF A GAS TURBINE ENGINE
#70Gas turbine with gap sealing between gas-washed components
#71Variable area fan nozzle systems with improved drive couplings
#72Shape memory alloy actuation system for variable area fan nozzle
#73Seals for a gas turbine engine
#74Exhaust section for bypass gas turbine engines
#75Methods and apparatus for sealing variable area fan nozzles of jet engines
#76Aeroengine thrust reverser arrangement
#77Leaf spring hanger for exhaust duct liner
#78Clamshell seal
#79Anti-fire seal assembly and nacelle comprising such a seal
#80Channeled spring seal for sealing an air gap between moving plates
#81Seal assembly
#82Seal for a variable area fan nozzle
#83Flexible seal system for a gas turbine engine
#84Variable width gap seal
#85VARIABLE AREA NOZZLE FOR GAS TURBINE ENGINE
#86Gas path liner for a gas turbine engine
#87Flap seal for gas turbine engine movable nozzle flap
#88Gas turbine exhaust nozzle divergent flap seal
#89Cable-actuated variable area fan nozzle with elastomeric seals
#90Gas turbine engine exhaust nozzle including a plurality of flaps movable over a flow control surface
#91REVERSE THRUST DEVICE
#92Flexible seal for gas turbine engine system
#93Flexible seal for gas turbine engine system
#94COMPLIANT SEALING JOINT
#95RADIAL AND AXIAL COMPLIANT SLIDING SEAL INCORPORATING SPRING CAPTURING FEATURES FOR IMPROVED BEARING PLANE SEALING IN AN ARTICULATING NOZZLE
#96Nacelle with a variable nozzle section
#97Engine exhaust system with directional nozzle
#98Baffle seal for gas turbine engine thrust reverser
#99Baffle seal for gas turbine engine thrust reverser
#100Exhaust nozzle seal with segmented basesheet disposed between side rails
#101Laminate air seal for a gas turbine engine
#102Flexible seal for gas turbine engine system
#103Duct installation
#104Low-leakage seal system for pivot door type thrust reverser
#105Convergent divergent nozzle with edge cooled divergent seals
#106Expansion joint for gas turbines
#107Seal assembly
#108Method and device for reducing engine noise
#109Convergent divergent nozzle with supported divergent seals
#110Method and apparatus for increasing a durability of a body
#111System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
#112Turbojet axisymmetric nozzle controlled hot flap shutter
#113Convergent turbojet exhaust nozzle
#114Reduced radar cross section exhaust nozzle assembly
#115Cooled dual wall liner closeout
#116Floating flexible firewall seal
#117Method and device for reducing engine noise
#118Method for resistance welding two sheet metal elements together
#119Cowl structure for a gas turbine engine
#120Divergent flap for a gas turbine engine
#121High temperature dynamic seal for scramjet variable geometry
#122Axial divergent section slot nozzle
#123Exhaust nozzle segmented basesheet and production method thereof
#124Method and apparatus for increasing a durability of a body
#125Method and apparatus for arresting a crack within a body
#126Flexible flap for a variable-section turbomachine nozzle
#127System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber
#128Variable area nozzle assembly for an aircraft propulsion system
#129Seal for gimbaling and/or fixed rocket engine nozzles, and associated systems and methods
#130Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system