IT1029612B - Perfezionamento nelle disposizioni di riduzione delle vibrazioni in rotori di aeromobili ad ala rotante - Google Patents
Perfezionamento nelle disposizioni di riduzione delle vibrazioni in rotori di aeromobili ad ala rotanteInfo
- Publication number
- IT1029612B IT1029612B IT7453396A IT5339674A IT1029612B IT 1029612 B IT1029612 B IT 1029612B IT 7453396 A IT7453396 A IT 7453396A IT 5339674 A IT5339674 A IT 5339674A IT 1029612 B IT1029612 B IT 1029612B
- Authority
- IT
- Italy
- Prior art keywords
- rotors
- improvement
- vibration reduction
- wing aircraft
- rotary wing
- 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
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/14—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
- F16F15/1407—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being limited with respect to the driving means
-
- 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
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Vibration Dampers (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4716473A GB1468359A (en) | 1973-10-09 | 1973-10-09 | Bifilar vibration dampers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT1029612B true IT1029612B (it) | 1979-03-20 |
Family
ID=10443978
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT7453396A IT1029612B (it) | 1973-10-09 | 1974-10-07 | Perfezionamento nelle disposizioni di riduzione delle vibrazioni in rotori di aeromobili ad ala rotante |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3932060A (it) |
| JP (1) | JPS5078100A (it) |
| DE (1) | DE2447454A1 (it) |
| FR (1) | FR2307190A1 (it) |
| GB (1) | GB1468359A (it) |
| IT (1) | IT1029612B (it) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3988074A (en) * | 1975-11-13 | 1976-10-26 | United Technologies Corporation | Anhedral bifilar |
| US4057363A (en) * | 1975-11-20 | 1977-11-08 | United Technologies Corporation | Extended arm bifilar and method to eliminate second order vibration excitation |
| US4111386A (en) * | 1976-12-09 | 1978-09-05 | United Technologies Corporation | Helicopter rotor and transmission mounting and vibration isolation system |
| US4550812A (en) * | 1978-08-04 | 1985-11-05 | United Technologies Corporation | Fixed position, fixed frequency pendular-type vibration absorber with frequency linearization |
| US4218187A (en) * | 1978-08-04 | 1980-08-19 | United Technologies Corporation | Constant frequency bifilar vibration absorber |
| US4239455A (en) * | 1978-09-11 | 1980-12-16 | Textron, Inc. | Blade-mounted centrifugal pendulum |
| US4739679A (en) * | 1986-01-23 | 1988-04-26 | Ford Motor Company | Bifilar pendulum vibration damper for automotive installation |
| US5495924A (en) * | 1994-07-13 | 1996-03-05 | Quiescence Engineering Corp. | Half-order centrifugal pendulum vibration absorber system |
| FR2733483B1 (fr) * | 1995-04-27 | 1997-07-04 | Eurocopter France | Dispositif d'attenuation de vibrations pour rotor d'helicoptere |
| DE19831156A1 (de) * | 1998-07-11 | 2000-01-13 | Freudenberg Carl Fa | Drehzahladaptiver Schwingungstilger |
| MXPA04006381A (es) * | 2004-06-28 | 2006-01-11 | Fernando Manuel Gil Aldrete | Multiplicador de torque. |
| US8931607B2 (en) * | 2010-01-29 | 2015-01-13 | Gm Global Technology Operations, Llc | Centrifugal pendulum vibration absorber |
| US8813604B2 (en) * | 2011-10-20 | 2014-08-26 | Chrysler Group Llc | Pendulum vibration absorber on a crankshaft |
| FR3010467B1 (fr) * | 2013-09-10 | 2016-12-09 | Valeo Embrayages | Dispositif d'absorption de vibrations |
| FR3021080B1 (fr) * | 2014-05-16 | 2020-02-21 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
| FR3021082B1 (fr) | 2014-05-16 | 2016-05-13 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
| FR3021081A1 (fr) * | 2014-05-16 | 2015-11-20 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
| US10577089B2 (en) | 2017-05-03 | 2020-03-03 | Sikorsky Aircraft Corporation | Integrated bifilar system that absorbs vibrations in both vertical and in-plane directions |
| CN110939673B (zh) * | 2019-12-04 | 2021-10-08 | 上海大学 | 一种耦合分段刚度的非线性减振装置 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3540809A (en) * | 1968-09-20 | 1970-11-17 | United Aircraft Corp | Vibration damped helicopter rotor |
| GB1443148A (en) * | 1972-10-19 | 1976-07-21 | Westland Aircraft Ltd | Bifilar vibration dampers |
-
1973
- 1973-10-09 GB GB4716473A patent/GB1468359A/en not_active Expired
-
1974
- 1974-09-20 US US05/507,933 patent/US3932060A/en not_active Expired - Lifetime
- 1974-10-04 DE DE19742447454 patent/DE2447454A1/de not_active Withdrawn
- 1974-10-07 JP JP49114787A patent/JPS5078100A/ja active Pending
- 1974-10-07 IT IT7453396A patent/IT1029612B/it active
- 1974-10-08 FR FR7433755A patent/FR2307190A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US3932060A (en) | 1976-01-13 |
| DE2447454A1 (de) | 1975-04-17 |
| FR2307190A1 (fr) | 1976-11-05 |
| FR2307190B1 (it) | 1981-02-06 |
| JPS5078100A (it) | 1975-06-25 |
| GB1468359A (en) | 1977-03-23 |
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