CA1113912A - Compound hub spring system for helicopters - Google Patents
Compound hub spring system for helicoptersInfo
- Publication number
- CA1113912A CA1113912A CA308,309A CA308309A CA1113912A CA 1113912 A CA1113912 A CA 1113912A CA 308309 A CA308309 A CA 308309A CA 1113912 A CA1113912 A CA 1113912A
- Authority
- CA
- Canada
- Prior art keywords
- mast
- flapping
- elastomeric
- rotor
- angle
- 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
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/35—Rotors having elastomeric joints
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Springs (AREA)
- Toys (AREA)
- Vibration Prevention Devices (AREA)
- Discharge By Other Means (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US82362477A | 1977-08-11 | 1977-08-11 | |
US823,624 | 1977-08-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1113912A true CA1113912A (en) | 1981-12-08 |
Family
ID=25239266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA308,309A Expired CA1113912A (en) | 1977-08-11 | 1978-07-27 | Compound hub spring system for helicopters |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS5453497A (es) |
CA (1) | CA1113912A (es) |
DE (1) | DE2833813C2 (es) |
FR (1) | FR2399945A1 (es) |
GB (1) | GB2002308B (es) |
IT (1) | IT1107202B (es) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2497173A1 (fr) * | 1980-12-26 | 1982-07-02 | Aerospatiale | Butee lamifiee de forme courbe, notamment pour rotor d'helicoptere |
BRPI0924584A2 (pt) * | 2009-06-02 | 2019-09-24 | Saab Ab | amortecedor de rotor e rotor de retaguarda com tal amortecedor de rotor |
DE102015107596B3 (de) * | 2015-05-13 | 2016-10-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Hubschrauber mit Einrichtungen zum Vermeiden des Mast Bumping |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1111541A (fr) * | 1953-07-22 | 1956-03-01 | Doman Helicopters | Rotor à libre inclinaison pour engins aériens à autosustentation |
US3804552A (en) * | 1972-07-05 | 1974-04-16 | Textron Inc | Four blade main rotor control power coupling |
US3807896A (en) * | 1972-10-10 | 1974-04-30 | Textron Inc | Concentric tube spring rotor mount |
-
1978
- 1978-07-27 CA CA308,309A patent/CA1113912A/en not_active Expired
- 1978-08-02 DE DE2833813A patent/DE2833813C2/de not_active Expired
- 1978-08-09 IT IT50673/78A patent/IT1107202B/it active
- 1978-08-11 GB GB7833011A patent/GB2002308B/en not_active Expired
- 1978-08-11 FR FR7823781A patent/FR2399945A1/fr active Granted
- 1978-08-11 JP JP9743778A patent/JPS5453497A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
GB2002308B (en) | 1982-01-06 |
DE2833813C2 (de) | 1987-01-02 |
JPS6239B2 (es) | 1987-01-06 |
IT1107202B (it) | 1985-11-25 |
FR2399945B1 (es) | 1983-02-18 |
DE2833813A1 (de) | 1979-02-22 |
IT7850673A0 (it) | 1978-08-09 |
JPS5453497A (en) | 1979-04-26 |
GB2002308A (en) | 1979-02-21 |
FR2399945A1 (fr) | 1979-03-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4333728A (en) | Compound hub spring system for helicopters | |
JP2911630B2 (ja) | ヘリコプターロータ | |
US4893988A (en) | System for damping lead-lag motion of rotor blades of helicopter | |
DE3886555T2 (de) | Drehkupplung mit Lenkern. | |
EP0221372B1 (en) | Constant velocity joint and installations | |
US5120195A (en) | Clevis joint capable of accommodating substantial pivotal motion between its joined members and loading along its axis | |
US3842945A (en) | Viscoelastic damper | |
US4886419A (en) | Elastomeric bearing for helicopter rotor having lead-lag damping | |
US3759632A (en) | Articulated helicopter rotor | |
KR101619996B1 (ko) | 회전익 항공기의 로터 시스템 | |
US2494985A (en) | Aircraft rotor damping device | |
JP2001130494A (ja) | プロップローターハブ | |
EP2519440B1 (en) | Variabale stiffness liquid inertia vibration eliminator | |
US5071319A (en) | Low maintenance, advanced technology swashplate | |
US3106965A (en) | Rotor head | |
EP0008303A1 (en) | Constant frequency bifilar vibration absorber | |
US11673659B2 (en) | Light-weight, elastic teeter bearing for a rotor and aircraft housing such bearing | |
CA1113912A (en) | Compound hub spring system for helicopters | |
US6032764A (en) | Roller guide assembly with sound isolation | |
DE102007019667B4 (de) | Lagervorrichtung | |
CN101506042A (zh) | 具有衬垫轴承的旋翼飞行器扭矩耦合件 | |
US3292711A (en) | Blade pitch change bearing | |
JPH04278897A (ja) | ヘリコプタ用斜板構造 | |
EP0722544B1 (en) | Device for damping vibration of rotor | |
US3824808A (en) | Counterbalancing device for coupling shafts for universal joints |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKEX | Expiry |