FR2132466B1 - - Google Patents
Info
- Publication number
- FR2132466B1 FR2132466B1 FR7211968A FR7211968A FR2132466B1 FR 2132466 B1 FR2132466 B1 FR 2132466B1 FR 7211968 A FR7211968 A FR 7211968A FR 7211968 A FR7211968 A FR 7211968A FR 2132466 B1 FR2132466 B1 FR 2132466B1
- 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
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2123771A JPS5614519B1 (fr) | 1971-04-06 | 1971-04-06 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2132466A1 FR2132466A1 (fr) | 1972-11-17 |
| FR2132466B1 true FR2132466B1 (fr) | 1975-03-21 |
Family
ID=12049424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7211968A Expired FR2132466B1 (fr) | 1971-04-06 | 1972-04-05 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3799695A (fr) |
| JP (1) | JPS5614519B1 (fr) |
| DE (1) | DE2216414C3 (fr) |
| FR (1) | FR2132466B1 (fr) |
| GB (1) | GB1353564A (fr) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1519380A (en) * | 1975-11-13 | 1978-07-26 | United Technologies Corp | Method and apparatus to control aircraft having dual rigid rotors |
| US4008979A (en) * | 1975-11-13 | 1977-02-22 | United Technologies Corporation | Control for helicopter having dual rigid rotors |
| US4027999A (en) * | 1975-11-13 | 1977-06-07 | United Technologies Corporation | Analog mixer to vary helicopter rotor phase angle in flight |
| DE2658828C3 (de) * | 1976-12-24 | 1982-02-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor für ein Drehflügelflugzeug |
| US4525123A (en) * | 1982-05-06 | 1985-06-25 | Alfred Curci | Rotary wing aircraft |
| US4697986A (en) * | 1984-03-26 | 1987-10-06 | David Constant V | Helicopter blade cyclic pitch control system |
| US4688993A (en) * | 1985-03-21 | 1987-08-25 | United Technologies Corporation | Tangential link swashplate centering member |
| US4930988A (en) * | 1989-01-02 | 1990-06-05 | Honeywell Inc | Individual blade control system for helicopters |
| US5165854A (en) * | 1990-07-12 | 1992-11-24 | Industrias Cicare S.R.L. | Mechanism for controlling pitch change in helicopter blades |
| AU659491B2 (en) * | 1992-09-23 | 1995-05-18 | Elisport Helicopters S.R.L | A control mechanism for helicopter rotor blades |
| US5826822A (en) * | 1996-04-19 | 1998-10-27 | Rehm; Rehm N. | System and method for providing cyclic and collective pitch control in a rotary wing aircraft |
| JP2000225277A (ja) * | 1999-02-05 | 2000-08-15 | Futaba Corp | ラジオコントロールヘリコプター |
| BR0313895A (pt) * | 2002-09-24 | 2005-08-30 | Bell Helicopter Textron Inc | Sistema de controle de aeronave de rotor com ligação de mistura escalonada |
| US7262712B2 (en) * | 2004-04-12 | 2007-08-28 | Safe Flight Instrument Corporation | Helicopter tactile exceedance warning system |
| FR2946317B1 (fr) * | 2009-06-04 | 2011-06-17 | Eurocopter France | Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante |
| FR2959205B1 (fr) * | 2010-04-27 | 2012-04-13 | Eurocopter France | Procede de commande et de regulation de l'angle de braquage d'un empennage d'helicoptere hybride |
| CN106802659A (zh) * | 2017-01-13 | 2017-06-06 | 清华大学 | 变桨距多旋翼飞行器的控制方法 |
| WO2023277847A1 (fr) * | 2021-06-29 | 2023-01-05 | Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi | Mécanisme de commande |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR995459A (fr) * | 1945-03-06 | 1951-12-03 | Procédé et dispositif permettant d'améliorer la maniabilité des appareils d'aviation à voilures tournantes articulées | |
| US2599690A (en) * | 1945-06-16 | 1952-06-10 | United Aircraft Corp | Helicopter control |
| US2748876A (en) * | 1951-01-12 | 1956-06-05 | Vertol Aircraft Corp | Means for controlling tip-path of rotors |
| FR1131074A (fr) * | 1954-12-24 | 1957-02-15 | Diretor Geral Do Ct Tecnico De | Perfectionnements aux dispositifs de stabilisation des hélicoptères |
| US2978037A (en) * | 1958-02-12 | 1961-04-04 | Ministerio Da Aeronautica Dire | Stabilizing means for helicopter aircraft |
| US3199601A (en) * | 1962-02-02 | 1965-08-10 | United Aircraft Corp | Flight control system |
| US3217809A (en) * | 1963-02-28 | 1965-11-16 | Kaman Aircraft Corp | Rotor blade pitch changing mechanism for rotary wing aircraft |
| US3589831A (en) * | 1969-11-10 | 1971-06-29 | Kaman Corp | Control system for rotary wing vehicle |
-
1971
- 1971-04-06 JP JP2123771A patent/JPS5614519B1/ja active Pending
-
1972
- 1972-03-17 US US00235645A patent/US3799695A/en not_active Expired - Lifetime
- 1972-03-30 GB GB1522272A patent/GB1353564A/en not_active Expired
- 1972-04-05 DE DE2216414A patent/DE2216414C3/de not_active Expired
- 1972-04-05 FR FR7211968A patent/FR2132466B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5614519B1 (fr) | 1981-04-04 |
| FR2132466A1 (fr) | 1972-11-17 |
| DE2216414C3 (de) | 1975-03-27 |
| GB1353564A (en) | 1974-05-22 |
| DE2216414A1 (de) | 1972-10-19 |
| US3799695A (en) | 1974-03-26 |
| DE2216414B2 (de) | 1974-08-08 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |