FR1473921A - Device for absorbing vibrations, in particular for aircraft with rotary wings and aircraft equipped with such a device - Google Patents
Device for absorbing vibrations, in particular for aircraft with rotary wings and aircraft equipped with such a deviceInfo
- Publication number
- FR1473921A FR1473921A FR40316A FR40316A FR1473921A FR 1473921 A FR1473921 A FR 1473921A FR 40316 A FR40316 A FR 40316A FR 40316 A FR40316 A FR 40316A FR 1473921 A FR1473921 A FR 1473921A
- Authority
- FR
- France
- Prior art keywords
- aircraft
- rotary wings
- absorbing vibrations
- aircraft equipped
- vibrations
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
-
- 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
- F16F15/22—Compensation of inertia forces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
- B64C2027/003—Vibration damping devices mounted on rotor hub, e.g. a rotary force generator
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Combined Devices Of Dampers And Springs (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US422830A US3219120A (en) | 1964-12-31 | 1964-12-31 | Vibration absorbing system |
US422741A US3298443A (en) | 1964-12-31 | 1964-12-31 | Vibration absorbing system |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1473921A true FR1473921A (en) | 1967-03-24 |
Family
ID=27025732
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR40316A Expired FR1473921A (en) | 1964-12-31 | 1965-11-30 | Device for absorbing vibrations, in particular for aircraft with rotary wings and aircraft equipped with such a device |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1456013A1 (en) |
FR (1) | FR1473921A (en) |
GB (1) | GB1120193A (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2768995B1 (en) * | 1997-10-01 | 1999-12-03 | Eurocopter France | PENDULUM ROTOR HEAD RESONATOR |
US8435002B2 (en) | 2004-08-30 | 2013-05-07 | Lord Corporation | Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations |
CN101022994B (en) | 2004-08-30 | 2012-07-04 | 洛德公司 | Helicopter vibration control system and rotary force generator for canceling vibrations |
US8162606B2 (en) | 2004-08-30 | 2012-04-24 | Lord Corporation | Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
US7722322B2 (en) | 2004-08-30 | 2010-05-25 | Lord Corporation | Computer system and program product for controlling vibrations |
US8267652B2 (en) | 2004-08-30 | 2012-09-18 | Lord Corporation | Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
US8474745B2 (en) | 2007-04-24 | 2013-07-02 | Textron Innovations Inc. | Rotor hub vibration attenuator |
US10526076B2 (en) | 2007-04-24 | 2020-01-07 | Textron Innovations Inc. | Rotor hub vibration attenuator |
US9452828B2 (en) | 2007-04-24 | 2016-09-27 | Textron Innovations Inc. | Rotor hub vibration attenuator |
DE07861293T1 (en) * | 2007-04-24 | 2011-01-27 | Bell Helicopter Textron, Inc., Fort Worth | ROTOR HUB VIBRATION |
KR101486721B1 (en) | 2007-10-25 | 2015-01-28 | 로드코포레이션 | Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations |
WO2009126626A2 (en) * | 2008-04-07 | 2009-10-15 | Lord Corporation | Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
EP2670661B1 (en) | 2011-02-04 | 2015-01-14 | Lord Corporation | Rotary wing aircraft vibration control system with resonant inertial actuators |
US10065730B2 (en) | 2014-01-22 | 2018-09-04 | Bell Helicopter Textron Inc. | Active vibration control system with non-concentric revolving masses |
US10906636B2 (en) | 2014-10-21 | 2021-02-02 | Sikorsky Aircraft Corporation | Vibration control assembly for an aircraft and method of controlling aircraft vibration |
EP3421359B1 (en) | 2017-06-30 | 2019-08-21 | LEONARDO S.p.A. | Rotor for a hover-capable aircraft |
EP3766778B1 (en) | 2019-07-19 | 2021-11-24 | LEONARDO S.p.A. | Rotor for a hover-capable aircraft |
EP3766779B1 (en) | 2019-07-19 | 2023-11-01 | LEONARDO S.p.A. | Rotor for a hover-capable aircraft |
CN112407252A (en) * | 2020-10-30 | 2021-02-26 | 中国直升机设计研究所 | Helicopter embedded type accurate balance weight system and weight method |
CN114524096B (en) * | 2022-03-10 | 2023-07-18 | 广州一诺智能信息工程有限公司 | Water conservancy is with automatic obstacle avoidance survey and drawing unmanned aerial vehicle |
-
1965
- 1965-10-12 GB GB4331765A patent/GB1120193A/en not_active Expired
- 1965-11-30 FR FR40316A patent/FR1473921A/en not_active Expired
- 1965-12-29 DE DE19651456013 patent/DE1456013A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE1456013A1 (en) | 1969-05-29 |
GB1120193A (en) | 1968-07-17 |
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