GB2149473B - Actuator system - Google Patents
Actuator systemInfo
- Publication number
- GB2149473B GB2149473B GB08329799A GB8329799A GB2149473B GB 2149473 B GB2149473 B GB 2149473B GB 08329799 A GB08329799 A GB 08329799A GB 8329799 A GB8329799 A GB 8329799A GB 2149473 B GB2149473 B GB 2149473B
- Authority
- GB
- United Kingdom
- Prior art keywords
- actuator system
- actuator
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B06—GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS IN GENERAL
- B06B—METHODS OR APPARATUS FOR GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS OF INFRASONIC, SONIC, OR ULTRASONIC FREQUENCY, e.g. FOR PERFORMING MECHANICAL WORK IN GENERAL
- B06B1/00—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency
- B06B1/18—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency wherein the vibrator is actuated by pressure fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
-
- 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
- B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
- B64C27/64—Transmitting means, e.g. interrelated with initiating means or means acting on blades using fluid pressure, e.g. having fluid power amplification
-
- 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
- B64C27/72—Means acting on blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08329799A GB2149473B (en) | 1983-11-08 | 1983-11-08 | Actuator system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08329799A GB2149473B (en) | 1983-11-08 | 1983-11-08 | Actuator system |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2149473A GB2149473A (en) | 1985-06-12 |
GB2149473B true GB2149473B (en) | 1987-03-11 |
Family
ID=10551438
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08329799A Expired GB2149473B (en) | 1983-11-08 | 1983-11-08 | Actuator system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2149473B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2160840B (en) * | 1984-06-29 | 1987-12-02 | Westland Plc | Method and apparatus for reducing vibration of a helicopter fuselage |
FR2675558A1 (en) * | 1991-04-22 | 1992-10-23 | Hutchinson | ELASTIC BINDING BAR WITH ACTIVE VIBRATION CONTROL SYSTEM. |
FR2678578B1 (en) * | 1991-07-02 | 1993-10-22 | Aerospatiale Ste Nationale Indle | PROCESS AND DEVICE FOR REDUCING DIFFERENCES IN THE FUSELAGE OF A HELICOPTER. |
JP2758374B2 (en) * | 1995-02-28 | 1998-05-28 | 株式会社コミュータヘリコプタ先進技術研究所 | Helicopter rotor harmonic controller |
FR2737181B1 (en) * | 1995-07-27 | 1997-09-19 | Eurocopter France | METHOD AND DEVICE FOR REDUCING VIBRATIONS GENERATED ON THE STRUCTURE OF A HELICOPTER |
FR2747099B1 (en) * | 1996-04-04 | 1998-06-12 | Eurocopter France | METHOD AND DEVICE FOR REDUCING THE EFFECT OF VIBRATIONS GENERATED BY THE DRIVE CHAIN OF A HELICOPTER |
DE102011014019B4 (en) * | 2011-03-15 | 2019-01-10 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | TPP-splitting |
EP2687440B1 (en) * | 2012-07-16 | 2017-10-11 | Airbus Defence and Space GmbH | Apparatus and method for reducing, avoiding or eliminating lateral vibrations of a helicopter |
DE102013223508B4 (en) * | 2013-11-19 | 2021-07-08 | Zf Friedrichshafen Ag | Control device of a helicopter main rotor |
-
1983
- 1983-11-08 GB GB08329799A patent/GB2149473B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2149473A (en) | 1985-06-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19921108 |