|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/055 F02C-006/08 F02C-007/18 F02C-009/18|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 7|
A device for protecting aircraft equipment against contact by a foreign object including an interference arrangement disposed in an air inlet upstream from the aircraft equipment where the interference arrangement is configured to physically obstruct passage of the foreign object within the air inlet.
1. An engine assembly for an aircraft, comprising: a turbine engine including a compressor and a turbine;a reduction gear mechanism;a fan driven by the turbine through the reduction gear mechanism to deliver ambient air to the turbine engine and to a section that bypasses the turbine engine to generate thrust;a precooler heat exchanger configured to receive bleed air from the compressor and cool the bleed air for distribution to at least one system of the aircraft, the precooler including a cooling air inlet downstream from the fan and facing a direction...