Synonyme wurden verwendet für:
Gas
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Gas Turbine
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Gas Turbine Propulsion
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Propulsion
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Propulsion Systems
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Turbine
Suche ohne Synonyme:
title: Gas Turbine Propulsion Systems
GAS TURBINE ENGINE WITH LIFING CALCULATIONS BASED UPON ACTUAL USAGE
A method of monitoring a gas turbine engine includes the steps of: (a) receiving information from actual flights of an aircraft
...Gas turbine engine with lifing calculations based upon actual usage
A method of monitoring a gas turbine engine includes the steps of: (a) receiving information from actual flights of an aircraft
...Gas turbine engine with lifing calculations based upon actual usage
A method of monitoring a gas turbine engine includes the steps of: (a) receiving information from actual flights of an aircraft
...Propulsion system cooling control
A propulsion system includes an electric fan propulsion motor with a plurality of propulsion motor windings. The propulsion system also
...PROPULSION SYSTEM COOLING CONTROL
A system for an aircraft (100) includes an engine bleed source (251) of a gas turbine engine (20). The system also includes a means for
...Hybrid electric aircraft system with distributed propulsion
A propulsion system for an aircraft includes at least one gas turbine engine, an electric auxiliary fan driving motor configured to
...HYBRID ELECTRIC AIRCRAFT SYSTEM WITH DISTRIBUTED PROPULSION
A propulsion system for an aircraft includes at least one gas turbine engine, an electric auxiliary fan driving motor configured to
...AIRCRAFT SYSTEM WITH DISTRIBUTED PROPULSION
A propulsion system for an aircraft includes at least two gas turbine engines and at least one auxiliary propulsion fan. The at least
...Aircraft system with distributed propulsion
A propulsion system for an aircraft includes at least two gas turbine engines and at least one auxiliary propulsion fan. The at least
...Aircraft hybrid propulsion fan drive gear system DC motors and generators
An aircraft propulsion system is disclosed and includes a first gas turbine engine including a first input shaft driving a first gear
...AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS
An aircraft propulsion system is disclosed and includes a first gas turbine engine (20A) including a first input shaft (72) driving a
...AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS
An aircraft propulsion system is disclosed and includes a first gas turbine engine including a first input shaft driving a first gear
...AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS
An aircraft propulsion system is disclosed and includes a first gas turbine engine including a first input shaft driving a first gear
...Aircraft hybrid propulsion fan drive gear system DC motors and generators
An aircraft propulsion system is disclosed and includes a first gas turbine engine including a first input shaft driving a first gear
...AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS
An aircraft propulsion system is disclosed and includes a first gas turbine engine including a first input shaft driving a first gear
...HIGH COMPRESSOR BUILD CLEARANCE REDUCTION
High compressor build clearance reduction
Cryogenic cooling system for an aircraft
CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT
A gas turbine engine includes a compressor section and a turbine section operably coupled to the compressor section. The gas turbine
...CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT
ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
A propulsion system includes a fan, a gear, a turbine configured to drive the gear to, in turn, drive the fan. The turbine has an exit
...Elongated geared turbofan with high bypass ratio
A propulsion system includes a fan, a gear, a turbine configured to drive the gear to, in turn, drive the fan. The turbine has an exit
...ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
A propulsion system (20) includes a fan (100), a gear (112), a turbine (116) configured to drive the gear (112) to, in turn, drive the
...Elongated geared turbofan with high bypass ratio
A propulsion system includes a fan, a gear, a turbine configured to drive the gear to, in turn, drive the fan. The turbine has an exit
...Exhaust nozzle arrangement for geared turbofan
A propulsion system according to an example of the present disclosure includes, among other things, a geared architecture configured to
...Exhaust nozzle arrangement for geared turbofan
A propulsion system according to an example of the present disclosure includes, among other things, a geared architecture configured to
...Exhaust nozzle for an elongated gear turbofan with high bypass ratio
A propulsion system includes a fan, a gear, a turbine configured to drive the gear to, in turn, drive the fan. The turbine has an exit
...Non-contact seal assembly for rotational equipment with linkage between adjacent rotors
An assembly is provided for rotational equipment such as a gas turbine engine for an aircraft propulsion system. This assembly includes
...NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT WITH LINKAGE BETWEEN ADJACENT ROTORS
An assembly is provided for rotational equipment such as a gas turbine engine for an aircraft propulsion system. This assembly includes
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