|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/18 B64C-029/02 F02K-001/00 F02B-027/00|
|미국특허분류(USC)||24/405.3B ; 24/406.0 ; 602/261 ; 602/69 ; 602/30|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 19 인용 특허 : 16|
An auxiliary inlet (60) for a jet engine has a first rod block (62) attached to a first side (64) of a hole (66) in a skin (68) of an inlet of the jet engine. A second rod block (80) is attached to an opposing side (82) of the hole (66) in the skin (68) of the inlet of the jet engine. A first reinforced elastomer section (70) is attached to the first rod block (62). A center beam (74) has a first side attached to the first reinforced elastomer section (70). A second reinforced elastomer section (78) is attached to the second rod block (80) and attached t...
[ What is claimed is:] [1.] An auxiliary air intake system for an aircraft having a jet engine, the system capable of being controlled to provide an auxiliary air inlet opening of variable cross sectional dimensions and without forming gaps or discontinuities in a surface of said aircraft, said system comprising:an inlet having an outer skin, the inlet attached to an intake side of the jet turbine;the outer skin having a hole having a rigid perimeter along three sides thereof;a first reinforced elastomer section attached to a first portion of the rigid p...