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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-02900 B64C-02504 B60V-00308|
|미국특허분류(USC)||244/013; 244/118.1; 244/100.R; 180/116|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 19|
An extremely large aircraft which is suitable for overseas cargo transport and which includes a fuselage defining a central storage cavity, a wing assembly defining a pair of wing storage cavities, an altitude control system, and a plurality of independently steerable landing gear units. The central storage cavity has a length, height and width of at least 100 feet, at least 16 feet and at least 24 feet, respectively. The wing assembly has a wingspan of at least 300 feet and is configured with a moderate aspect ratio to permit both ground-effect and high...
1. An aircraft comprising:a fuselage defining a central storage cavity, the central storage cavity having a length of at least 100 feet, a height of at least 16 feet and a width of at least about 24 feet; a wing assembly extending through and fixedly coupled to the fuselage in an unswept manner and providing the aircraft with a wingspan of at least 300 feet, the wing assembly defining a pair of wing storage cavities each of which being located on an opposite side of the fuselage, the wing assembly having a moderate aspect ratio of at least 3.5 to permit ...