FR3084647B1 - Aeronef a decollage et atterissage vertical - Google Patents
Aeronef a decollage et atterissage vertical Download PDFInfo
- Publication number
- FR3084647B1 FR3084647B1 FR1857246A FR1857246A FR3084647B1 FR 3084647 B1 FR3084647 B1 FR 3084647B1 FR 1857246 A FR1857246 A FR 1857246A FR 1857246 A FR1857246 A FR 1857246A FR 3084647 B1 FR3084647 B1 FR 3084647B1
- Authority
- FR
- France
- Prior art keywords
- vertical take
- helix
- propeller
- landing aircraft
- aircraft
- 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.)
- Active
Links
Classifications
-
- 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
- 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
- B64C2027/8236—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 including pusher propellers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
L'invention concerne un aéronef (10, 11, 13, 15) à décollage et atterrissage vertical comprenant un fuselage (12) au-dessus duquel est agencé au moins un rotor (24) de sustentation, caractérisé en ce qu'il comprend au moins une première hélice (26) et une seconde hélice (28) chacune portée par une queue (16) et articulée en déplacement sur celle-ci entre au moins une première position dans laquelle elle est apte à servir de rotor d'anti-couple et au moins une seconde position dans laquelle elle est apte à permettre une poussée de propulsion de l'aéronef (10, 11, 13, 15) dans une direction d'avance, les axes (26a, 28a) de rotation desdites première hélice (26) et seconde hélice (28) étant sensiblement coaxiaux lorsque lesdites première hélice (26) et seconde hélice (28) sont dans leur première position.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1857246A FR3084647B1 (fr) | 2018-08-02 | 2018-08-02 | Aeronef a decollage et atterissage vertical |
PCT/FR2019/051848 WO2020025885A1 (fr) | 2018-08-02 | 2019-07-25 | Aeronef a decollage et atterrissage vertical |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1857246A FR3084647B1 (fr) | 2018-08-02 | 2018-08-02 | Aeronef a decollage et atterissage vertical |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3084647A1 FR3084647A1 (fr) | 2020-02-07 |
FR3084647B1 true FR3084647B1 (fr) | 2021-02-26 |
Family
ID=65200996
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1857246A Active FR3084647B1 (fr) | 2018-08-02 | 2018-08-02 | Aeronef a decollage et atterissage vertical |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3084647B1 (fr) |
WO (1) | WO2020025885A1 (fr) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009045986A (ja) * | 2007-08-17 | 2009-03-05 | Mitsubishi Heavy Ind Ltd | ヘリコプタ |
JP2009090755A (ja) * | 2007-10-05 | 2009-04-30 | Mitsubishi Heavy Ind Ltd | テールロータ |
US10377479B2 (en) * | 2016-06-03 | 2019-08-13 | Bell Helicopter Textron Inc. | Variable directional thrust for helicopter tail anti-torque system |
US10526085B2 (en) * | 2016-06-03 | 2020-01-07 | Bell Textron Inc. | Electric distributed propulsion anti-torque redundant power and control system |
-
2018
- 2018-08-02 FR FR1857246A patent/FR3084647B1/fr active Active
-
2019
- 2019-07-25 WO PCT/FR2019/051848 patent/WO2020025885A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2020025885A1 (fr) | 2020-02-06 |
FR3084647A1 (fr) | 2020-02-07 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20200207 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
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PLFP | Fee payment |
Year of fee payment: 6 |