VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE

To provide an aerial vehicle that is efficient in flight and that can take off and land vertically.SOLUTION: A flight control apparatus for fixed-wing aircraft includes a first port wing 115 and first starboard wing 120, a first port swash plate 145 coupled between a first port rotor 155 and a first...

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Bibliographische Detailangaben
Hauptverfasser:	CHRISTOPHER EUGENE FISHER, DANA J TAYLOR, JOSEPH FREDERICK KING, PHILLIP T TOKUMARU, BART DEAN HIBBS, JASON SIDHARTHADEV MUKHERJEE, DAVID WAYNE GANZER, WILLIAM MARTIN PARKS
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	To provide an aerial vehicle that is efficient in flight and that can take off and land vertically.SOLUTION: A flight control apparatus for fixed-wing aircraft includes a first port wing 115 and first starboard wing 120, a first port swash plate 145 coupled between a first port rotor 155 and a first port electric motor 135 that is coupled to the first port wing 115, and a first starboard swash plate 150 coupled between a first starboard rotor 130 and a first starboard electric motor 140 that is coupled to the first starboard wing 120.SELECTED DRAWING: Figure 3A 【課題】飛行時に効率がよく、かつ垂直に離着陸できる航空機を提供する。【解決手段】固定翼機の飛行制御装置が、第１の左翼１１５および第１の右翼１２０と、第１の左ロータ１５５と第１の左翼１１５に連結された第１の左電気モータ１３５との間に連結された第１の左スワッシュプレート１４５と、第１の右ロータ１３０と第１の右翼１２０に連結された第１の右電気モータ１４０との間に連結された第１の右スワッシュプレート１５０と、を有する。【選択図】図３Ａ