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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/55 ; 244/35R ; 244/198 ; 244/130|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 38 인용 특허 : 3|
Modifications to a jet aircraft of the type having aft fuselage-mounted engine nacelles overlapping trailing edge portions of the aircraft\s wings, wherein a channel area defined by the fuselage, wing, pylon and attached nacelle is shaped to prevent air flowing therethrough from forming a shock wave during flight operation in the transonic regime, resulting in significant drag reduction as compared to an unmodified jet aircraft of a similar type. Further modifications to the jet aircraft\s wings provide additional lift while significantly reducing drag a...
In a jet aircraft of the type having aft fuselage-mounted engine nacelles partially overlapping trailing edge portions of the aircraft\s wings, said jet aircraft being capable of flight in the transonic regime and including a channel on either side of the aircraft defined by said trailing edge portion of said wing, the aircraft fuselage, a pylon support assembly extending between said fuselage and said nacelle, a surface of said nacelle overlapping said wing, and an imaginary plane of symmetry extending from a lower-most outer surface of said nacelle int...