JP2022103349A - 航空機及び航空機を飛行させる方法 - Google Patents
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/42—Adjusting about chordwise axes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/10—Aircraft characterised by the type or position of power plant of gas-turbine type
- B64D27/12—Aircraft characterised by the type or position of power plant of gas-turbine type within or attached to wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
Description
この出願は、2017年4月27日に出願された米国仮特許出願第62/490,814号の利益を主張するものであり、該出願は、参照によってその全体が本願明細書に組み込まれるものとする。
Claims (19)
- 胴体と、
前記胴体の対向側から延びている対向する翼と、
前記対向する翼の各々に取り付け可能である少なくとも一つのエンジンと、を備え、
前記少なくとも一つのエンジンを含む、各対向する翼の少なくとも一部は、回転軸周りに前記胴体に対して回転可能であり、
前記少なくとも一つのエンジンは、循環ピッチ変動のために構成された複数のブレードを含むプロペラを有している、航空機。 - 前記回転軸は、前記胴体の長手方向軸に対して直角ではなく、横断している、請求項1に記載の航空機。
- 前記少なくとも一つのエンジンを含む、各対向する翼の前記少なくとも一部は、垂直離着陸用に構成された第一のコンフィギュレーションと、水平飛行用に構成された第二のコンフィギュレーションとの間で前記胴体に対して回転する、請求項1に記載の航空機。
- 前記少なくとも一つのエンジンは、前記第一のコンフィギュレーションにおいて前記航空機に揚力を提供するように構成されている、請求項3に記載の航空機。
- 前記プロペラの前記複数のブレードの前記循環ピッチ変動と、集合ピッチ変動との少なくとも一方は、前記対向する翼の前記第一のコンフィギュレーションでのホバリングを可能にする、請求項3に記載の航空機。
- 前記プロペラの前記複数のブレードの前記循環ピッチ変動は、前記対向する翼の前記第一のコンフィギュレーションでの前方飛行を可能にする、請求項3に記載の航空機。
- 前記エンジンの各々の出力は独立して調節可能である、請求項1に記載の航空機。
- 前記対向する翼の各々は、前記胴体から延びている固定部と、該固定部の外側寄りの回転部とを含む、請求項1に記載の航空機。
- 前記対向する翼の各々の前記回転部の前縁は、前記対向する翼の前記第一のコンフィギュレーションにおいて上を向く、請求項8に記載の航空機。
- 前記対向する翼の各々は、前記固定部に対する前記回転部の回転を制御する少なくとも一つのアクチュエータを備える、請求項8に記載の航空機。
- 前記少なくとも一つのアクチュエータはリニアアクチュエータである、請求項10に記載の航空機。
- 胴体と、
前記胴体の対向側から延びている対向する翼と、
前記対向する翼の各々に取り付け可能である複数のエンジンと、を備え、
前記複数のエンジンを含む、各対向する翼の少なくとも一部は、前記胴体の長手方向軸に対して直角ではなく、横断している回転軸周りに、垂直離着陸用に構成された第一のコンフィギュレーションと、水平飛行用に構成された第二のコンフィギュレーションとの間で、前記胴体に対して回転可能であり、
前記エンジンの各々の出力は、少なくとも前記第一のコンフィギュレーションにおいて独立して調節可能である、航空機。 - 前記エンジンの各々の前記出力は、前記エンジンの各々の速度を変化させることにより独立して調節可能である、請求項12に記載の航空機。
- 前記複数のエンジンは、前記第一のコンフィギュレーションにおいて前記航空機に揚力を提供するように構成されている、請求項13に記載の航空機。
- 前記対向する翼の各々は、前記胴体から延びている固定部と、該固定部の外側寄りの回転部とを含む、請求項12に記載の航空機。
- 前記対向する翼の各々の回転部の前縁は、前記対向する翼の前記第一のコンフィギュレーションにおいて上を向く、請求項12に記載の航空機。
- 航空機を飛行させる方法であって、
対向する翼の少なくとも一部を胴体に対して、前記胴体の長手方向軸に対して直角ではなく、横断している回転軸周りに回転させて、前記対向する翼の各々の前縁を垂直方向に向け、前記対向する翼の回転される部分は少なくとも一つのエンジンを有することと、
前記少なくとも一つのエンジンを作動させることと、
前記航空機をホバリングさせるために前記少なくとも一つのエンジンの出力を独立して制御することと、を含む、方法。 - 前記少なくとも一つのエンジンが取り付けられた、前記対向する翼の前記回転される部分を回転させて、前記少なくとも一つのエンジンと、前記翼の前縁とを、前方飛行のために水平方向に向けることをさらに含む、請求項17に記載の方法。
- 前記対向する翼と前記少なくとも一つのエンジンとが、ホバリングと前方飛行との間で移行するために、垂直方向と水平方向との間にあるように、前記対向する翼の前記回転される部分の回転を中断することをさらに含む、請求項17に記載の方法。
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JP2023215907A JP2024019668A (ja) | 2017-04-27 | 2023-12-21 | 航空機アセンブリ、航空機の翼アセンブリ及び航空機を製造する方法 |
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US201762490814P | 2017-04-27 | 2017-04-27 | |
US62/490,814 | 2017-04-27 | ||
US15/848,705 US10252798B2 (en) | 2017-04-27 | 2017-12-20 | Vertical takeoff and landing airframe |
US15/848,705 | 2017-12-20 | ||
PCT/US2018/022814 WO2018200093A1 (en) | 2017-04-27 | 2018-03-16 | Vertical takeoff and landing airframe |
JP2019559092A JP7080500B2 (ja) | 2017-04-27 | 2018-03-16 | 垂直離着陸機体 |
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JP2022081615A Active JP7414310B2 (ja) | 2017-04-27 | 2022-05-18 | 航空機及び航空機を飛行させる方法 |
JP2023215907A Pending JP2024019668A (ja) | 2017-04-27 | 2023-12-21 | 航空機アセンブリ、航空機の翼アセンブリ及び航空機を製造する方法 |
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EP (1) | EP3615420A4 (ja) |
JP (3) | JP7080500B2 (ja) |
CN (1) | CN110869276A (ja) |
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WO2018200093A1 (en) | 2018-11-01 |
JP7414310B2 (ja) | 2024-01-16 |
JP7080500B2 (ja) | 2022-06-06 |
US20200277051A1 (en) | 2020-09-03 |
US20190225333A1 (en) | 2019-07-25 |
JP2020524106A (ja) | 2020-08-13 |
US10556679B2 (en) | 2020-02-11 |
JP2024019668A (ja) | 2024-02-09 |
CN110869276A (zh) | 2020-03-06 |
US10252798B2 (en) | 2019-04-09 |
US20180312251A1 (en) | 2018-11-01 |
EP3615420A1 (en) | 2020-03-04 |
EP3615420A4 (en) | 2021-01-20 |
US10967969B2 (en) | 2021-04-06 |
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