|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 35|
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...
1. An aircraft, comprising: a hydrogen source;an oxygen source;a control system configured to actively control and vary the pressures at which the hydrogen and oxygen are supplied for reaction in the fuel cell, wherein the control system is configured to actively control and vary the reaction pressures of the fuel cell based on the altitude of the aircraft;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 ...