IT1182769B - PROCEDURE AND APPARATUS TO REDUCE VIBRATIONS IN HELICOPTER FUSELAGES - Google Patents
PROCEDURE AND APPARATUS TO REDUCE VIBRATIONS IN HELICOPTER FUSELAGESInfo
- Publication number
- IT1182769B IT1182769B IT48290/85A IT4829085A IT1182769B IT 1182769 B IT1182769 B IT 1182769B IT 48290/85 A IT48290/85 A IT 48290/85A IT 4829085 A IT4829085 A IT 4829085A IT 1182769 B IT1182769 B IT 1182769B
- Authority
- IT
- Italy
- Prior art keywords
- procedure
- reduce vibrations
- fuselages
- helicopter
- helicopter fuselages
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
-
- 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
- B64C27/001—Vibration damping devices
- B64C2027/002—Vibration damping devices mounted between the rotor drive and the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8416679 | 1984-06-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8548290A0 IT8548290A0 (en) | 1985-06-27 |
IT1182769B true IT1182769B (en) | 1987-10-05 |
Family
ID=10563212
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT48290/85A IT1182769B (en) | 1984-06-29 | 1985-06-27 | PROCEDURE AND APPARATUS TO REDUCE VIBRATIONS IN HELICOPTER FUSELAGES |
Country Status (5)
Country | Link |
---|---|
DE (1) | DE3522662A1 (en) |
FR (1) | FR2566862B1 (en) |
GB (1) | GB2160840B (en) |
IT (1) | IT1182769B (en) |
SG (1) | SG76488G (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2680848B1 (en) * | 1991-08-29 | 1995-03-17 | Aerospatiale Ste Nat Indle | METHOD AND DEVICE FOR FILTERING THE VIBRATORY EXCITATIONS TRANSMITTED BETWEEN TWO PARTS, IN PARTICULAR BETWEEN THE ROTOR AND THE FUSELAGE OF A HELICOPTER. |
GB9124081D0 (en) * | 1991-11-13 | 1992-09-23 | Westland Helicopters | Strut assemblies |
GB2267470B (en) * | 1992-06-03 | 1995-12-13 | Westland Helicopters | Method and apparatus for in-flight shake testing of an aircraft fuselage |
GB9211719D0 (en) * | 1992-06-03 | 1992-07-15 | Westland Helicopters | Method & apparatus for in-flight shake testing of an aircraft fuselage |
FR2731405B1 (en) * | 1995-03-10 | 1997-05-09 | Eurocopter France | SYSTEM FOR MINIMIZING DYNAMIC EXCITATION OF A HELICOPTER |
FR2749901B1 (en) * | 1996-06-12 | 2000-12-08 | Eurocopter France | DEVICE FOR REDUCING THE VIBRATION GENERATED BY A LIFT ROTOR OF A TURNED AIRCRAFT |
DE10001159A1 (en) * | 2000-01-13 | 2001-07-26 | Liebherr Aerospace Gmbh | Vibration insulator for helicopter; has two force conduction points connected by insulator that generates dynamic counter oscillations, which are transmitted by spring system |
DE10304336B4 (en) * | 2003-02-03 | 2011-02-24 | Eurocopter Deutschland Gmbh | A method for damping tail boom vibrations of rotary-wing aircraft and rotary-wing aircraft with a tail boom vibration damping device |
FR2975668B1 (en) | 2011-05-27 | 2013-07-05 | Eurocopter France | METHOD AND AIRCRAFT PROVIDED WITH DEVICE FOR VIBRATION REDUCTION |
GB2492965B (en) * | 2011-07-15 | 2018-05-02 | Agustawestland Ltd | A system and method for reducing the transmission of vibration from a first vibrating body to a second body |
WO2016057215A1 (en) | 2014-09-26 | 2016-04-14 | Sikorsky Aircraft Corporation | Anti-vibration moment generating aircraft actuation system |
FR3040691A1 (en) | 2015-09-08 | 2017-03-10 | Airbus Helicopters | AIRCRAFT AND AIRCRAFT ENGINEERING GROUP |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3144082A (en) * | 1962-11-13 | 1964-08-11 | Hughes Tool Co | Vibration damping mechanism |
US3216679A (en) * | 1963-02-06 | 1965-11-09 | Mechanical Tech Inc | Active vibration isolator |
FR1506385A (en) * | 1966-09-16 | 1967-12-22 | Sud Aviation | Method of attenuation and electro-hydraulic vibration attenuator for rotary wing aerodyne |
US3514054A (en) * | 1967-06-05 | 1970-05-26 | United Aircraft Corp | Vibration isolation system |
US3701499A (en) * | 1968-04-08 | 1972-10-31 | Wright Barry Corp | Active fluid isolation system |
US3606233A (en) * | 1968-04-22 | 1971-09-20 | Bolt Beranek & Newman | Vibration isolation system |
US3635427A (en) * | 1969-05-06 | 1972-01-18 | Textron Inc | Aircraft vibration compensation system |
US3638885A (en) * | 1970-03-09 | 1972-02-01 | Boeing Co | Lag frequency selective damper |
US3635429A (en) * | 1970-03-27 | 1972-01-18 | Textron Inc | Aircraft vibration compensation system |
US3617020A (en) * | 1970-04-27 | 1971-11-02 | Boeing Co | Vibration control system |
JPS5638438B1 (en) * | 1971-03-08 | 1981-09-07 | ||
US3845917A (en) * | 1971-10-18 | 1974-11-05 | Textron Inc | Helicopter vibration isolation |
JPS5511954A (en) * | 1978-07-14 | 1980-01-28 | Hitachi Ltd | Method and device for controlling vibration of vehicle |
US4199989A (en) * | 1978-09-18 | 1980-04-29 | Hughes Aircraft Company | Cold damping of mechanical structures |
EP0067548A1 (en) * | 1981-06-02 | 1982-12-22 | M.L. Aviation Company Limited | Vibration suppressor |
US4453378A (en) * | 1982-04-19 | 1984-06-12 | Chandler Evans, Inc. | Torsional mode suppressor |
US4600863A (en) * | 1982-04-19 | 1986-07-15 | Sound Attenuators Limited | Method of and apparatus for active vibration isolation |
GB2149473B (en) * | 1983-11-08 | 1987-03-11 | Lucas Ind Plc | Actuator system |
-
1985
- 1985-06-17 GB GB08515295A patent/GB2160840B/en not_active Expired
- 1985-06-25 DE DE19853522662 patent/DE3522662A1/en not_active Withdrawn
- 1985-06-27 IT IT48290/85A patent/IT1182769B/en active
- 1985-06-28 FR FR8509858A patent/FR2566862B1/en not_active Expired
-
1988
- 1988-11-16 SG SG764/88A patent/SG76488G/en unknown
Also Published As
Publication number | Publication date |
---|---|
SG76488G (en) | 1990-07-06 |
DE3522662A1 (en) | 1986-01-09 |
FR2566862B1 (en) | 1987-11-27 |
FR2566862A1 (en) | 1986-01-03 |
IT8548290A0 (en) | 1985-06-27 |
GB8515295D0 (en) | 1985-07-17 |
GB2160840A (en) | 1986-01-02 |
GB2160840B (en) | 1987-12-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19970628 |