FR2167249B1 - - Google Patents
Info
- Publication number
- FR2167249B1 FR2167249B1 FR7200751A FR7200751A FR2167249B1 FR 2167249 B1 FR2167249 B1 FR 2167249B1 FR 7200751 A FR7200751 A FR 7200751A FR 7200751 A FR7200751 A FR 7200751A FR 2167249 B1 FR2167249 B1 FR 2167249B1
- Authority
- FR
- France
- 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
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
- B64C2027/8254—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
- B64C2027/829—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 a V-tail units
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7200751A FR2167249B1 (no) | 1972-01-11 | 1972-01-11 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7200751A FR2167249B1 (no) | 1972-01-11 | 1972-01-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2167249A1 FR2167249A1 (no) | 1973-08-24 |
FR2167249B1 true FR2167249B1 (no) | 1974-06-21 |
Family
ID=9091703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7200751A Expired FR2167249B1 (no) | 1972-01-11 | 1972-01-11 |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2167249B1 (no) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2534222A1 (fr) * | 1982-10-06 | 1984-04-13 | Aerospatiale | Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement |
FR2600036B1 (fr) * | 1986-06-16 | 1988-09-16 | Aerospatiale | Dispositif directionnel et stabilisateur a rotor anti-couple carene et incline et a empennage en " v " dissymetrique, et helicoptere equipe d'un tel dispositif. |
FR2689854B1 (fr) * | 1992-04-14 | 1994-07-01 | Eurocopter France | Helicoptere monorotor a systeme anticouple mixte et procede pour contrecarrer le couple induit par ce monorotor. |
US5727757A (en) * | 1996-01-17 | 1998-03-17 | Mcdonnell Douglas Helicopter Co. | Slotted cam control system |
FR2769284B1 (fr) * | 1997-10-07 | 1999-12-03 | Eurocopter France | Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere |
FR2769285B1 (fr) * | 1997-10-07 | 1999-12-03 | Eurocopter France | Dispositif de commande d'un systeme anticouple mixte d'un helicoptere |
WO1999067130A1 (en) * | 1998-06-25 | 1999-12-29 | Sikorsky Aircraft Corporation | Horizontal stabilizer for rotorcraft |
DE102008046486A1 (de) * | 2008-09-08 | 2010-03-18 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zum Landen eines Drehflüglers und Drehflügler |
FR2995586B1 (fr) | 2012-09-17 | 2014-08-22 | Eurocopter France | Moyen de stabilisation en tangage et aeronef a voilure tournante muni d'un tel moyen |
EP3061689B1 (en) * | 2015-02-27 | 2017-09-27 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3116036A (en) * | 1961-04-17 | 1963-12-31 | Eltra Corp | Long range convertible helicopter |
FR1511006A (fr) * | 1966-12-13 | 1968-01-26 | Sud Aviation | Dispositif directionnel et propulsif pour hélicoptère |
FR1576475A (no) * | 1968-04-26 | 1969-08-01 |
-
1972
- 1972-01-11 FR FR7200751A patent/FR2167249B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2167249A1 (no) | 1973-08-24 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |