Individual bypass injector valves for a double bypass variable c
Inlet and outlet module for a heat exchanger for a flowpath for
Inlet cowl attachment for jet engine
Inlet guide vane bleed system
Installation for the control of the fuel supply to the afterburn
Integral infrared radiation suppressor for a turbofan engine
Integral pulse detonation system for a gas turbine engine
Integrated air inlet system for multi-propulsion aircraft...
Integrated bypass turbojet engines for air craft and other...
Integrated control system for a gas turbine engine
Integrated corner for ducted fan engine shrouds
Integrated engine shroud for gas turbine engines
Integrated fan / low pressure compressor rotor for gas turbine e
Integrated fan-core twin spool counter-rotating turbofan gas...
Integrated fan-core twin spool counter-rotating turbofan gas...
Integrated gas turbine engine-nacelle
Integrated gas turbine engine-nacelle
Integrated turboramjet engine
Integrated turboramjet engine
Interstage seal arrangement for airfoil stages of turbine engine