|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/27 F02K-001/32 B64D-037/00 F02C-009/18 F02C-009/46 F02C-007/262 F02C-007/26|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 3|
Several embodiments include a system and method for providing thrust recovery in an aircraft engine. The system and method enables a wider range of safe operation for aircraft where the aircraft engine is rapidly reactivated from a substantially deactivated state. The method thereby reduces noise output and fuel usage during descent and shortens runway lengths and occupancy time required for landing. Thrust recovery is provided via the use of stored bleed air being re-injected back into the aircraft engine. An onboard air storage tank and a system of val...
1. A method for thrust recovery in a jet engine, comprising: storing pressurized gas including at least a portion of a pressurized bleed air from a compressor on the jet engine in at least an onboard tank;substantially deactivating a combustor of the jet engine during flight;operating a valve to feed the pressurized gas from the onboard tank through the jet engine thereby reactivating the combustor;monitoring the storing of the pressurized gas in the onboard tank; anddisplaying via a pilot terminal an indication that sufficient pressurized gas has been s...