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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/2 ; 244/131 ; 244/1374|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 0|
This invention relates to a composite aircraft comprising a conventional aircraft (2) and a carrier aircraft (4) connected together during flight as a composite aircraft by way of a connector (6). The carrier aircraft has a vertical takeoff and/or landing capability and the conventional aircraft is provided with a directable propulsion nozzle so that during operations as a composite aircraft lift is shared by components of lift from the propulsion systems of both aircraft. Therefore, by connecting itself to the carrier aircraft, the conventional aircraft...
A composite aircraft comprising: a fixed wing carrier aircraft constructed and arranged to provide in use a first component of lift, another aircraft provided with propulsive force applying means for providing in use a second component of lift substantially equal in magnitude to said first component, a connector comprising a connecting member constructed and arranged to extend from said carrier aircraft to said another aircraft, respective attachment means, at least one of which is releasable, for attaching said carrier aircraft and said another aircraft...