145575 ⎘
Function; Fluid transfer Venting into the ambient atmosphere or the like
ACTIVE CONTROL OF GEARBOX CASE PRESSURE
#2AERIAL VEHICLE FLUID CONTROL SYSTEM WITH MULTI-WAY FLOW REGULATOR
#3VENT STACK ASSEMBLIES FOR HYDROGEN DISTRIBUTION SYSTEMS AND RELATED METHODS
#4CORE COMPARTMENT VENT DURING ENGINE SHUTDOWN TO REDUCED BOWED ROTOR START
#5MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS
#6AIRCRAFT NACELLE COMPRISING A SEALED BOX STRUCTURE AND A DOOR WHICH OPENS THE BOX STRUCTURE TO THE OUTSIDE
#7Anti-ice system for gas turbine engine and inlet guide vane
#8HYDROGEN FUEL SYSTEM
#9ELECTRONICALLY CONTROLLED PRESSURE RELIEF SYSTEM FOR AN ENGINE
#10Core compartment vent during engine shutdown to reduced bowed rotor start
#11Ejection tube incorporated in a central ventilation tube
#12Self-damping actuator
#13Gas turbine engine bleed air flow control
#14Aerial vehicle fluid control system with multi-way flow regulator
#15Aerial vehicle fluid control system integrated with gas turbine engine
#16Means for handling gaseous fuel
#17PURGE SYSTEM FOR A HYDROGEN FUEL SYSTEM
#18Reducing contrails from an aircraft powerplant
#19Mixed flow exhaust thrust reverser with area control nozzle systems and methods
#20Turbine engine having a balance cavity
#21Mixed flow exhaust thrust reverser with area control nozzle systems and methods
#22Thrust reverser interspatial blocker system
#23Axial fan with openings in the hub
#24Orifice pack for compressor bleed valve
#25Sump auxiliary vent system
#26MEANS FOR HANDLING GASEOUS FUEL
#27Means for handling gaseous fuel
#28Sweep flow structures for fuel systems
#29Hydrogen fuel leak detection system
#30DEGASSING TUBE AND EJECTION CONE FOR A TURBINE ENGINE, AS WELL AS TOOL FOR ASSEMBLY THEREOF
#31Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
#32PLENUM RESONANCE PREVENTION FOR GAS TURBINE ENGINE
#33Self-damping actuator
#34Ducted fan turbine engine comprising a system involving screens for blocking off the duct for the secondary flow
#35SYSTEMS FOR THRUST REVERSER WITH TEMPERATURE AND FLUID MANAGEMENT
#36Venting system for bearing sump
#37Bellows-enabled bleed valve
#38System and method for engine eductor powered by alternate managed air system
#39Measuring device and method for an aircraft engine and an aircraft engine
#40Rotor drum for a turbomachine
#41Pressure relief door rotating exhaust deflector
#42System and method for engine eductor powered by alternate managed air system
#43Sump auxiliary vent system
#44Aircraft propulsion system comprising an internal fixed structure with a discharge slot
#45Dual trip manifold assembly for turbine systems
#46Systems and methods for thrust reverser with temperature and fluid management
#47Systems and methods for thrust reverser with temperature and fluid management
#48Centrifugal fan and air supply device having the same
#49Hydraulic and pneumatic control circuit having a fuel/air heat exchanger for a turbojet
#50TURBOFAN ENGINE
#51Degassing tube and ejection cone for a turbine engine, as well as tool for assembly thereof
#52Gas turbine engine
#53Apparatus and method for controlling a pressure differential across a seal of a bearing chamber
#54Bleeding structure for gas turbine engine
#55Dual trip manifold assembly for turbine systems
#56Discharge flow duct of a turbine engine comprising a VBV grating with variable setting
#57Dual trip manifold assembly for turbine systems
#58Turbofan engine and a method for exhausting breather air of an oil separator in a turbofan engine
#59Center vent tube aligning mechanism and center vent tube support device
#60Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine
#61High pressure exhaust muffling device with multiple sources
#62Combined cycle plant, method for controlling same, and device for controlling same
#63Valve device and jet engine with a valve device
#64Gas turbine engine variable area fan nozzle with ice management
#65Trailing edge core compartment vent for an aircraft engine
#66Motive air conditioning system for gas turbines
#67System for discharging compressed air from a compressor
#68PNEUMATIC PORTING VIA SELF-ACTUATED DUAL PIVOT FLAPPER VALVE
#69Gearbox with sealed accessory vent
#70Bleed valve resonator drain
#71Ventilation of a turbomachine nacelle
#72Pressure controlled chamber
#73Flapper valve assembly and method of flowing air therethrough
#74Jet engine with at least one oil separator, through which an air-oil-volume flow can be guided
#75Jet engine with at least one oil separator
#76SYSTEM FOR PROVIDING FUEL TO A COMBUSTOR ASSEMBLY IN A GAS TURBINE ENGINE
#77Reflex annular vent nozzle
#78TurbinAL™ high flow COdelivery system
#79CONTINUOUS PURGE SYSTEM FOR A STEAM TURBINE
#80Variable turbine/compressor geometry
#81Gas turbine engine variable area fan nozzle with ice management
#82Air turbine starter and method for venting without loss of oil
#83System and method for turbine compartment ventilation
#84Air-provisioning system with ejectors
#85Reducing contrails from an aircraft powerplant
#86Self compensating rocket engine enhancement