FR2999150B1 - Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage - Google Patents
Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselageInfo
- Publication number
- FR2999150B1 FR2999150B1 FR1203351A FR1203351A FR2999150B1 FR 2999150 B1 FR2999150 B1 FR 2999150B1 FR 1203351 A FR1203351 A FR 1203351A FR 1203351 A FR1203351 A FR 1203351A FR 2999150 B1 FR2999150 B1 FR 2999150B1
- Authority
- FR
- France
- Prior art keywords
- caren
- fuselage
- rotors
- wing
- horizontal fan
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- 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
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/31—Aircraft characterised by electric power plants within, or attached to, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/33—Hybrid electric aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
- B64C2027/8272—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising fins, or movable rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
- B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Wind Motors (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Transmission Devices (AREA)
- Emergency Lowering Means (AREA)
Priority Applications (12)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1203351A FR2999150B1 (fr) | 2012-12-10 | 2012-12-10 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
| RU2015127645A RU2015127645A (ru) | 2012-12-10 | 2013-12-09 | Конвертоплан с двумя винтами в кольцевых каналах на концах крыльев и с одним горизонтальным вентилятором на фюзеляже |
| CN201380064416.3A CN104918853A (zh) | 2012-12-10 | 2013-12-09 | 在翼尖装有两个涵道风扇并在机身上装有一个水平涵道风扇的转换式飞行器 |
| JP2015547106A JP2016501773A (ja) | 2012-12-10 | 2013-12-09 | 胴体に水平ファンおよび翼端にダクテッドファン2基を備えた転換式航空機 |
| AU2013357155A AU2013357155A1 (en) | 2012-12-10 | 2013-12-09 | Convertible aircraft provided with two ducted rotors at the wing tips and with a horizontal fan in the fuselage |
| PCT/FR2013/000326 WO2014091092A1 (fr) | 2012-12-10 | 2013-12-09 | Aéronef convertible pourvu de deux rotors carénés en bout d'aile et d'un fan horizontal dans le fuselage |
| US14/650,231 US20150314865A1 (en) | 2012-12-10 | 2013-12-09 | Convertible aircraft provided with two ducted rotors at the wing tips and with a horizontal fan in the fuselage |
| CA2894465A CA2894465A1 (fr) | 2012-12-10 | 2013-12-09 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
| KR1020157018491A KR20150086398A (ko) | 2012-12-10 | 2013-12-09 | 2개의 덕트 로터와 1개의 수평 팬이 각각 날개 끝과 동체에 장착된 전환식 항공기 |
| BR112015013009A BR112015013009A2 (pt) | 2012-12-10 | 2013-12-09 | aeronave conversível dotada de dois rotores carenados na extremidade da asa e de uma ventoinha horizontal na fuselagem |
| FR1501679A FR3024431A1 (fr) | 2012-12-10 | 2015-08-05 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
| PCT/IB2016/054705 WO2017021918A1 (fr) | 2012-12-10 | 2016-08-04 | Aéronef convertible pourvu de deux rotors carénés en bout d'aile et d'un fan horizontal dans le fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1203351A FR2999150B1 (fr) | 2012-12-10 | 2012-12-10 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2999150A1 FR2999150A1 (fr) | 2014-06-13 |
| FR2999150B1 true FR2999150B1 (fr) | 2015-10-09 |
Family
ID=48237003
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1203351A Expired - Fee Related FR2999150B1 (fr) | 2012-12-10 | 2012-12-10 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
| FR1501679A Withdrawn FR3024431A1 (fr) | 2012-12-10 | 2015-08-05 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1501679A Withdrawn FR3024431A1 (fr) | 2012-12-10 | 2015-08-05 | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US20150314865A1 (fr) |
| JP (1) | JP2016501773A (fr) |
| KR (1) | KR20150086398A (fr) |
| CN (1) | CN104918853A (fr) |
| AU (1) | AU2013357155A1 (fr) |
| BR (1) | BR112015013009A2 (fr) |
| CA (1) | CA2894465A1 (fr) |
| FR (2) | FR2999150B1 (fr) |
| RU (1) | RU2015127645A (fr) |
| WO (2) | WO2014091092A1 (fr) |
Families Citing this family (88)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2999150B1 (fr) * | 2012-12-10 | 2015-10-09 | Bermond Gerome Maurice Paul | Aeronef convertible pourvu de deux rotors carenes en bout d'aile et d'un fan horizontal dans le fuselage |
| ITRM20130473A1 (it) * | 2013-08-12 | 2013-11-11 | Unit 1 Srl | Convertiplano con nuove soluzionitecniche ed aerodinamiche atte a rendere sicuro e fruibile il mezzo anche in soluzioni di velivolo ultraleggero |
| BR112016025875B1 (pt) * | 2014-05-07 | 2022-08-23 | XTI Aircraft Company | Aeronave de vtol |
| WO2016074182A1 (fr) | 2014-11-12 | 2016-05-19 | SZ DJI Technology Co., Ltd. | Procédé et système pour le recyclage de la puissance moteur d'un objet mobile |
| CN105775121A (zh) * | 2014-12-26 | 2016-07-20 | 深圳智航无人机有限公司 | 一种变翼式无人机及其方法 |
| JP2017015527A (ja) | 2015-06-30 | 2017-01-19 | 株式会社トプコン | 広域センサシステム、飛行検出方法およびプログラム |
| CH711670A2 (de) * | 2015-10-21 | 2017-04-28 | Niederberger-Engineering Ag | Multikopter-Fluggerät mit mehreren Antriebsrotoren. |
| CN105270625A (zh) * | 2015-10-23 | 2016-01-27 | 庆安集团有限公司 | 一种多用途垂直起降无人机 |
| CN105346719B (zh) * | 2015-11-18 | 2017-11-03 | 珠海磐磊智能科技有限公司 | 垂直起降飞行器 |
| CN106934074B (zh) * | 2015-12-29 | 2020-07-31 | 中国航发商用航空发动机有限责任公司 | 全局最优涡扇发动机进气道减噪设计方法 |
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| CN105947192A (zh) * | 2016-06-01 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | 一种倾转双涵道无人机 |
| CN107585294A (zh) * | 2016-07-08 | 2018-01-16 | 袁洪跃 | 一种内旋翼飞行器结构 |
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-
2012
- 2012-12-10 FR FR1203351A patent/FR2999150B1/fr not_active Expired - Fee Related
-
2013
- 2013-12-09 WO PCT/FR2013/000326 patent/WO2014091092A1/fr not_active Ceased
- 2013-12-09 CA CA2894465A patent/CA2894465A1/fr not_active Abandoned
- 2013-12-09 BR BR112015013009A patent/BR112015013009A2/pt not_active IP Right Cessation
- 2013-12-09 AU AU2013357155A patent/AU2013357155A1/en not_active Abandoned
- 2013-12-09 US US14/650,231 patent/US20150314865A1/en not_active Abandoned
- 2013-12-09 RU RU2015127645A patent/RU2015127645A/ru not_active Application Discontinuation
- 2013-12-09 JP JP2015547106A patent/JP2016501773A/ja active Pending
- 2013-12-09 KR KR1020157018491A patent/KR20150086398A/ko not_active Ceased
- 2013-12-09 CN CN201380064416.3A patent/CN104918853A/zh active Pending
-
2015
- 2015-08-05 FR FR1501679A patent/FR3024431A1/fr not_active Withdrawn
-
2016
- 2016-08-04 WO PCT/IB2016/054705 patent/WO2017021918A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014091092A1 (fr) | 2014-06-19 |
| JP2016501773A (ja) | 2016-01-21 |
| US20150314865A1 (en) | 2015-11-05 |
| WO2017021918A1 (fr) | 2017-02-09 |
| FR3024431A1 (fr) | 2016-02-05 |
| RU2015127645A (ru) | 2017-01-16 |
| BR112015013009A2 (pt) | 2017-07-11 |
| KR20150086398A (ko) | 2015-07-27 |
| FR2999150A1 (fr) | 2014-06-13 |
| AU2013357155A1 (en) | 2015-07-30 |
| CN104918853A (zh) | 2015-09-16 |
| CA2894465A1 (fr) | 2014-06-09 |
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