FR2697793B1 - Mounting of a reactor in a helicopter and means so that the compressor of the reactor can eject its compressed air, at the same time, towards the two lateral sides of the tail of the helicopter and / or towards the rear. - Google Patents
Mounting of a reactor in a helicopter and means so that the compressor of the reactor can eject its compressed air, at the same time, towards the two lateral sides of the tail of the helicopter and / or towards the rear.Info
- Publication number
- FR2697793B1 FR2697793B1 FR9213582A FR9213582A FR2697793B1 FR 2697793 B1 FR2697793 B1 FR 2697793B1 FR 9213582 A FR9213582 A FR 9213582A FR 9213582 A FR9213582 A FR 9213582A FR 2697793 B1 FR2697793 B1 FR 2697793B1
- Authority
- FR
- France
- Prior art keywords
- helicopter
- reactor
- towards
- eject
- compressor
- 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
- 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
-
- 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
- B64C2027/8245—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 using air jets
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9213582A FR2697793B1 (en) | 1992-11-09 | 1992-11-09 | Mounting of a reactor in a helicopter and means so that the compressor of the reactor can eject its compressed air, at the same time, towards the two lateral sides of the tail of the helicopter and / or towards the rear. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9213582A FR2697793B1 (en) | 1992-11-09 | 1992-11-09 | Mounting of a reactor in a helicopter and means so that the compressor of the reactor can eject its compressed air, at the same time, towards the two lateral sides of the tail of the helicopter and / or towards the rear. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2697793A1 FR2697793A1 (en) | 1994-05-13 |
FR2697793B1 true FR2697793B1 (en) | 1995-01-06 |
Family
ID=9435448
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9213582A Expired - Fee Related FR2697793B1 (en) | 1992-11-09 | 1992-11-09 | Mounting of a reactor in a helicopter and means so that the compressor of the reactor can eject its compressed air, at the same time, towards the two lateral sides of the tail of the helicopter and / or towards the rear. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2697793B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2853938A1 (en) * | 2003-04-17 | 2004-10-22 | Noel Gil | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB770026A (en) * | 1952-10-10 | 1957-03-13 | Snecma | Device for steering and/or stabilizing a helicopter |
FR1298518A (en) * | 1961-06-02 | 1962-07-13 | Sud Aviation | Helicopter orientation control device |
GB1557590A (en) * | 1976-10-25 | 1979-12-12 | Secr Defence | Gas thrusters |
-
1992
- 1992-11-09 FR FR9213582A patent/FR2697793B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2697793A1 (en) | 1994-05-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20060731 |