|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/059; 244/0530R; 244/058|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 34|
Disclosed is an aircraft, configured to have a wide range of flight speeds, consuming low levels of power for an extended period of time, while supporting a communications platform with an unobstructed downward-looking view. The aircraft includes an extendable slat at the leading edge of the wing, and a reflexed trailing edge. The aircraft comprises a flying wing extending laterally between two ends and a center point. The wing is swept and has a relatively constant chord. The aircraft also includes a power module configured to provide power via a fuel c...
We claim: 1. An aircraft, comprising:a hydrogen source;an oxygen source;one or more aircraft engines configured to provide all necessary thrust for the aircraft to fly; anda fuel cell configured to react hydrogen from the hydrogen source with oxygen from the oxygen source to generate power, wherein the fuel cell is configured to react the hydrogen with the oxygen, each being supplied at reaction pressures of less than one atmosphere absolute;wherein power generated by the fuel cell powers the one or more aircraft engines; andwherein the fuel cell is furt...