FR2655612B1 - COMBINED HELICOPTERS. - Google Patents
COMBINED HELICOPTERS.Info
- Publication number
- FR2655612B1 FR2655612B1 FR9015337A FR9015337A FR2655612B1 FR 2655612 B1 FR2655612 B1 FR 2655612B1 FR 9015337 A FR9015337 A FR 9015337A FR 9015337 A FR9015337 A FR 9015337A FR 2655612 B1 FR2655612 B1 FR 2655612B1
- Authority
- FR
- France
- Prior art keywords
- helicopters
- combined
- combined helicopters
- 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 - Lifetime
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
- B64C27/22—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
- B64C27/82—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
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB898927784A GB8927784D0 (en) | 1989-12-08 | 1989-12-08 | Helicopters |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2655612A1 FR2655612A1 (en) | 1991-06-14 |
FR2655612B1 true FR2655612B1 (en) | 1995-06-23 |
Family
ID=10667637
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9015337A Expired - Lifetime FR2655612B1 (en) | 1989-12-08 | 1990-12-07 | COMBINED HELICOPTERS. |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE4039028A1 (en) |
FR (1) | FR2655612B1 (en) |
GB (2) | GB8927784D0 (en) |
IT (1) | IT1242175B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9114085D0 (en) * | 1991-06-29 | 1997-09-17 | Rolls Royce Plc | Improvements in or relating to helicopters |
FR2679199B1 (en) * | 1991-07-16 | 1997-01-31 | Aerospatiale | ANTICOUPLE SYSTEM FOR HELICOPTER. |
US5676335A (en) * | 1995-03-08 | 1997-10-14 | Mcdonnell Douglas Helicopter Company | Airflow control system for a helicopter |
ZA962567B (en) * | 1995-07-25 | 1996-10-07 | Denel Pty Ltd | Operation of a helicopter |
DE04822069T1 (en) | 2004-09-28 | 2008-01-03 | Bell Helicopter Textron, Inc., Fort Worth | TORQUE TORQUE DRIVE SYSTEM FOR TILT TURNERS |
NL1043177B1 (en) * | 2019-03-04 | 2020-09-17 | Pal V Ip B V | Vertical Take Off and Landing Vehicle |
CN110228585B (en) * | 2019-06-14 | 2022-11-22 | 安徽工业大学 | Combined wing aircraft |
US11584522B2 (en) * | 2020-11-30 | 2023-02-21 | Textron Innovations Inc. | Rotorcraft with cooling anti-torque system |
US11760472B2 (en) * | 2020-12-01 | 2023-09-19 | Textron Innovations Inc. | Rudders for rotorcraft yaw control systems |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2383038A (en) * | 1943-06-04 | 1945-08-21 | Bossi Enea | Airing of antitorque propellers |
US2941749A (en) * | 1955-04-06 | 1960-06-21 | United Aircraft Corp | Jet propelled convertiplane with jet driven rotor |
DE1124823B (en) * | 1959-05-02 | 1962-03-01 | Daimler Benz Ag | Propulsion for aircraft |
FR1298518A (en) * | 1961-06-02 | 1962-07-13 | Sud Aviation | Helicopter orientation control device |
GB964360A (en) * | 1961-12-12 | 1964-07-22 | Power Jets Res & Dev Ltd | Helicopter |
DE1272729B (en) * | 1965-04-22 | 1968-07-11 | Dornier Gmbh | Combination aircraft with a rotor arranged at the tail |
US4026472A (en) * | 1965-12-08 | 1977-05-31 | General Electric Company | Convergent-divergent plug nozzle |
DE1526809C3 (en) * | 1966-04-28 | 1973-12-06 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Thrust nozzle for gas turbine jet engines, preferably for afterburner engines |
US3409250A (en) * | 1966-12-27 | 1968-11-05 | Gen Electric | Movable fairing for an aircraftmounted nozzle |
US3442471A (en) * | 1966-12-27 | 1969-05-06 | Helen M Fischer | Nozzle structure |
US3612402A (en) * | 1969-12-22 | 1971-10-12 | Rohr Corp | Thrust-controlling apparatus with variable axial flow area for differing flight regimes and thrust reversal |
US3678690A (en) * | 1970-07-10 | 1972-07-25 | United Aircraft Corp | Convertible composite engine |
GB1407428A (en) * | 1971-10-20 | 1975-09-24 | Mtu Muenchen Gmbh | Gas turbine engine having a power turbine system adapted to be selectively cut in |
US3807662A (en) * | 1972-11-13 | 1974-04-30 | Lockheed Aircraft Corp | Anti-torque, propulsion, and directional control system |
DE2328460A1 (en) * | 1973-06-05 | 1975-01-02 | Motoren Turbinen Union | V/STOL. turbo-jet engine - has multi-flow and multi-drive shaft construction |
US3957226A (en) * | 1975-01-27 | 1976-05-18 | The Boeing Company | Helicopter yaw and propulsion mechanism |
US4200252A (en) * | 1977-12-21 | 1980-04-29 | Summa Corporation | Helicopter antitorque system using circulation control |
FR2501786A1 (en) * | 1981-03-13 | 1982-09-17 | Snecma | DEVICE FOR BEARING AND GUIDING AN ORIENTABLE NOZZLE OF A REACTION PROPELLER |
GB2130984B (en) * | 1982-12-01 | 1986-07-02 | Rolls Royce | Compound helicopter and power plant therefor |
IT1183880B (en) * | 1985-06-07 | 1987-10-22 | Agusta Aeronaut Costr | HELICOPTER WITH TURBINE POWER SUPPLY UNIT PROVIDED WITH EXHAUST MASK DEVICE |
GB2194597B (en) * | 1986-08-29 | 1990-07-25 | Rolls Royce Plc | A variable area exhaust nozzle for a gas turbine engine |
-
1989
- 1989-12-08 GB GB898927784A patent/GB8927784D0/en active Pending
-
1990
- 1990-12-05 GB GB9026434A patent/GB2238996B/en not_active Expired - Lifetime
- 1990-12-06 IT IT48545A patent/IT1242175B/en active IP Right Grant
- 1990-12-07 DE DE4039028A patent/DE4039028A1/en not_active Withdrawn
- 1990-12-07 FR FR9015337A patent/FR2655612B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
IT9048545A1 (en) | 1991-06-09 |
FR2655612A1 (en) | 1991-06-14 |
DE4039028A1 (en) | 1991-06-13 |
GB8927784D0 (en) | 1990-05-30 |
IT9048545A0 (en) | 1990-12-06 |
GB9026434D0 (en) | 1991-01-23 |
IT1242175B (en) | 1994-02-16 |
GB2238996B (en) | 1993-05-19 |
GB2238996A (en) | 1991-06-19 |
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