IT1163655B - Dispositivo di sospensione multidirezionale per giroplano - Google Patents
Dispositivo di sospensione multidirezionale per giroplanoInfo
- Publication number
- IT1163655B IT1163655B IT21152/79A IT2115279A IT1163655B IT 1163655 B IT1163655 B IT 1163655B IT 21152/79 A IT21152/79 A IT 21152/79A IT 2115279 A IT2115279 A IT 2115279A IT 1163655 B IT1163655 B IT 1163655B
- Authority
- IT
- Italy
- Prior art keywords
- gyroplan
- suspension device
- multidirectional suspension
- multidirectional
- suspension
- 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
-
- 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
-
- 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
-
- 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
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7808001A FR2420825A1 (fr) | 1978-03-20 | 1978-03-20 | Dispositif de suspension multidirectionnelle pour giravion |
FR7832281A FR2441902A2 (fr) | 1978-11-15 | 1978-11-15 | Dispositif de suspension multidirectionnelle pour giravion |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7921152A0 IT7921152A0 (it) | 1979-03-20 |
IT1163655B true IT1163655B (it) | 1987-04-08 |
Family
ID=26220503
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT21152/79A IT1163655B (it) | 1978-03-20 | 1979-03-20 | Dispositivo di sospensione multidirezionale per giroplano |
Country Status (5)
Country | Link |
---|---|
US (1) | US4274510A (it) |
JP (1) | JPS54129698A (it) |
DE (1) | DE2910729C2 (it) |
GB (1) | GB2018942B (it) |
IT (1) | IT1163655B (it) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5690725A (en) * | 1979-12-20 | 1981-07-23 | Nissan Motor Co Ltd | Mounting device for engine |
JPS56124513A (en) * | 1980-02-29 | 1981-09-30 | Nissan Motor Co Ltd | Mounting device of engine |
DE3706379A1 (de) * | 1987-02-27 | 1988-09-08 | Porsche Ag | Aufhaengungssystem fuer ein antriebsaggregat eines hubschraubers |
FR2728538A1 (fr) * | 1994-12-23 | 1996-06-28 | Eurocopter France | Dispositif de suspension anti-vibratoire de rotor d'helicoptere |
US5762295A (en) * | 1996-02-23 | 1998-06-09 | Lord Corporation | Dynamically optimized engine suspension system |
FR2756542B1 (fr) * | 1996-11-29 | 1999-02-12 | Eurocopter France | Installation de montage d'un moteur sur un plancher, et de connexion de son arbre de sortie avec au moins un mecanisme entraine |
CA2496755C (en) * | 2002-09-17 | 2011-03-15 | Bell Helicopter Textron Inc. | Torsionally de-coupled engine mount system |
FR2872784B1 (fr) * | 2004-07-09 | 2007-10-12 | Eurocopter France | Systeme de suspension d'un moteur d'aeronef a voilure tournante |
DE102008021431A1 (de) * | 2008-04-29 | 2009-11-12 | Airbus Deutschland Gmbh | Flugzeug mit einer Energie-Versorgungsvorrichtung |
PT2179922E (pt) | 2008-10-21 | 2012-06-20 | Agustawestland Spa | Helicóptero |
EP2495433B1 (en) * | 2011-03-02 | 2016-03-02 | ALSTOM Renewable Technologies | Wind turbine and method for lifting a gearbox torque arm |
EP2962935B1 (en) * | 2014-07-04 | 2016-09-21 | AGUSTAWESTLAND S.p.A. | Helicopter with noise and vibration damping transmission mounting |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2129124A (en) * | 1933-09-14 | 1938-09-06 | Gen Motors Corp | Transmission mount |
DE687705C (de) * | 1935-09-29 | 1940-02-03 | Getefo Ges Fuer Tech Fortschri | ren |
US2060604A (en) * | 1935-11-16 | 1936-11-10 | Edward R Bartlett | Resilient support for engines |
US2739769A (en) * | 1954-10-22 | 1956-03-27 | Bell Aircraft Corp | Rotary wing aircraft propulsion system mounting |
FR1507306A (fr) * | 1966-11-17 | 1967-12-29 | Sud Aviation | Dispositif de liaison filtrant les vibrations entre un organe vibrant et un support,notamment un rotor et une structure d'hélicoptère |
US3698663A (en) * | 1970-12-07 | 1972-10-17 | Textron Inc | Rotary wing pylon mounting system |
GB1380710A (en) * | 1970-12-29 | 1975-01-15 | Kawasaki Heavy Ind Ltd | Rotary wing aircraft |
FR2228662B1 (it) * | 1973-05-08 | 1976-11-12 | Aerospatiale | |
FR2232481B1 (it) * | 1973-06-08 | 1976-05-07 | Aerospatiale | |
FR2270144B1 (it) * | 1974-05-09 | 1976-10-15 | Aerospatiale |
-
1979
- 1979-03-19 GB GB7909622A patent/GB2018942B/en not_active Expired
- 1979-03-19 DE DE2910729A patent/DE2910729C2/de not_active Expired
- 1979-03-19 US US06/021,778 patent/US4274510A/en not_active Expired - Lifetime
- 1979-03-20 IT IT21152/79A patent/IT1163655B/it active
- 1979-03-20 JP JP3181979A patent/JPS54129698A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
GB2018942A (en) | 1979-10-24 |
DE2910729C2 (de) | 1986-05-22 |
US4274510A (en) | 1981-06-23 |
IT7921152A0 (it) | 1979-03-20 |
JPH035359B2 (it) | 1991-01-25 |
JPS54129698A (en) | 1979-10-08 |
DE2910729A1 (de) | 1979-09-27 |
GB2018942B (en) | 1982-06-03 |
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