|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 17|
An airflow diverter system for an aircraft may include an external aircraft surface upstream from an engine inlet and a passage having an upstream opening adjacent the engine inlet. The passage may be configured to channel boundary airflow from the external aircraft surface away from the engine inlet. The diverter system may include an occlusion device configured to selectively open and close the opening to the passage.
1. An airflow diverter system for an aircraft, comprising an external aircraft surface on a fuselage wall upstream from an engine inlet,a passage through the fuselage wall having an opening upstream from the engine inlet and visible from below or in front of the aircraft, configured to channel boundary airflow from the external aircraft surface away from the engine inlet, anda door covering the opening of the passage, the door being selectively moveable between an open position and a closed position, and being flush with the external aircraft surface whe...