GB2043574B - Pylon mounting system for reducing helicopter vibration - Google Patents
Pylon mounting system for reducing helicopter vibrationInfo
- Publication number
- GB2043574B GB2043574B GB8005968A GB8005968A GB2043574B GB 2043574 B GB2043574 B GB 2043574B GB 8005968 A GB8005968 A GB 8005968A GB 8005968 A GB8005968 A GB 8005968A GB 2043574 B GB2043574 B GB 2043574B
- Authority
- GB
- United Kingdom
- Prior art keywords
- mounting system
- helicopter vibration
- pylon mounting
- reducing helicopter
- reducing
- 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
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Sliding-Contact Bearings (AREA)
- Support Of The Bearing (AREA)
- Pivots And Pivotal Connections (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1640379A | 1979-03-01 | 1979-03-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2043574A GB2043574A (en) | 1980-10-08 |
GB2043574B true GB2043574B (en) | 1982-12-22 |
Family
ID=21776951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8005968A Expired GB2043574B (en) | 1979-03-01 | 1980-02-22 | Pylon mounting system for reducing helicopter vibration |
Country Status (12)
Country | Link |
---|---|
JP (1) | JPS55160700A (en) |
AR (1) | AR226172A1 (en) |
AU (1) | AU533359B2 (en) |
BR (1) | BR8001223A (en) |
CA (1) | CA1149360A (en) |
DE (1) | DE3007200A1 (en) |
ES (1) | ES8103707A1 (en) |
FR (1) | FR2450200A1 (en) |
GB (1) | GB2043574B (en) |
IL (1) | IL59460A (en) |
IT (1) | IT1144041B (en) |
MX (1) | MX6587E (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8480065B2 (en) | 2005-04-27 | 2013-07-09 | Textron Innovations Inc. | Elastomeric spring-damper with integral stops |
DE102009015806B4 (en) * | 2009-04-01 | 2013-04-04 | Otmar Birkner | gyrocopter |
CN109522636B (en) * | 2018-11-09 | 2022-12-30 | 中国直升机设计研究所 | Wheel type undercarriage simplifying method for helicopter crash-resistant analysis |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US322379A (en) * | 1885-07-14 | Axel jorgensen | ||
FR1334044A (en) * | 1961-09-01 | 1963-08-02 | Maschf Augsburg Nuernberg Ag | Device for suspending an engine in the chassis of a road or rail vehicle |
US3690607A (en) * | 1970-02-16 | 1972-09-12 | Kenneth C Mard | Vibration isolation system |
US4111386A (en) * | 1976-12-09 | 1978-09-05 | United Technologies Corporation | Helicopter rotor and transmission mounting and vibration isolation system |
-
1980
- 1980-02-22 GB GB8005968A patent/GB2043574B/en not_active Expired
- 1980-02-24 IL IL59460A patent/IL59460A/en unknown
- 1980-02-26 DE DE19803007200 patent/DE3007200A1/en active Granted
- 1980-02-27 AU AU55937/80A patent/AU533359B2/en not_active Ceased
- 1980-02-28 ES ES489030A patent/ES8103707A1/en not_active Expired
- 1980-02-28 CA CA000346615A patent/CA1149360A/en not_active Expired
- 1980-02-28 IT IT48034/80A patent/IT1144041B/en active
- 1980-02-29 AR AR280143A patent/AR226172A1/en active
- 1980-02-29 MX MX808674U patent/MX6587E/en unknown
- 1980-02-29 BR BR8001223A patent/BR8001223A/en not_active IP Right Cessation
- 1980-03-01 JP JP2466380A patent/JPS55160700A/en active Granted
- 1980-03-03 FR FR8004676A patent/FR2450200A1/en active Granted
Also Published As
Publication number | Publication date |
---|---|
BR8001223A (en) | 1980-11-04 |
IT1144041B (en) | 1986-10-29 |
DE3007200C2 (en) | 1989-01-26 |
ES489030A0 (en) | 1981-02-16 |
AU533359B2 (en) | 1983-11-17 |
CA1149360A (en) | 1983-07-05 |
IT8048034A0 (en) | 1980-02-28 |
AR226172A1 (en) | 1982-06-15 |
FR2450200B1 (en) | 1984-08-03 |
AU5593780A (en) | 1980-09-04 |
JPS55160700A (en) | 1980-12-13 |
ES8103707A1 (en) | 1981-02-16 |
IL59460A (en) | 1984-02-29 |
FR2450200A1 (en) | 1980-09-26 |
MX6587E (en) | 1985-07-26 |
DE3007200A1 (en) | 1980-09-11 |
JPH0253279B2 (en) | 1990-11-16 |
GB2043574A (en) | 1980-10-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2126759B (en) | Vibration compensation system | |
IL59459A (en) | Vibration suppression system | |
GB2130308B (en) | Hydraulic system for an aircraft | |
GB2151995B (en) | Apparatus for the suspension of an aircraft engine cowling | |
AU7693681A (en) | Vibration absorbing system | |
JPS56124597A (en) | Vibrationproof suspension system for helicopter | |
GB2087033B (en) | Vibration isolation system | |
EG13105A (en) | Helicopter rotor and transmission mounting and vibration isolation system | |
JPS5686898A (en) | Loadinggunloading device for aircraft | |
JPS5543696A (en) | System for damping mechanical body vibration | |
DE3371893D1 (en) | Duct means for aircraft | |
DE3260522D1 (en) | Vibration damping device for helicopter | |
GB8424426D0 (en) | Landing adjustment system | |
GB2043574B (en) | Pylon mounting system for reducing helicopter vibration | |
DE3467818D1 (en) | Damping system for micro-deflector | |
DE3370863D1 (en) | Damping means for force tranducers | |
GB2192942B (en) | Powerplant simulators for aircraft | |
DE3477425D1 (en) | Radar system for aircraft | |
GB8333508D0 (en) | Aircraft in-flight management system | |
GB2059374B (en) | Navigation system for aircraft | |
DE2967373D1 (en) | Rubber-metal shear-loaded mounting | |
JPS57130899A (en) | Takeoff accelerating auxiliary device for aircraft | |
JPS55156798A (en) | Mounting structure for transmission of helicopter | |
JPS5613295A (en) | Washer for aircraft | |
GB2135031B (en) | Device for releasing loads fixed to an aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Effective date: 20000221 |