IT1065299B - Dispositivo ammortizzatore elastomero - Google Patents
Dispositivo ammortizzatore elastomeroInfo
- Publication number
- IT1065299B IT1065299B IT30613/76A IT3061376A IT1065299B IT 1065299 B IT1065299 B IT 1065299B IT 30613/76 A IT30613/76 A IT 30613/76A IT 3061376 A IT3061376 A IT 3061376A IT 1065299 B IT1065299 B IT 1065299B
- Authority
- IT
- Italy
- Prior art keywords
- shock absorber
- absorber device
- elastomer shock
- elastomer
- shock
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
-
- 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
- B64C27/51—Damping of blade movements
-
- 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
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/30—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium with solid or semi-solid material, e.g. pasty masses, as damping medium
- F16F9/306—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium with solid or semi-solid material, e.g. pasty masses, as damping medium of the constrained layer type, i.e. comprising one or more constrained viscoelastic layers
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Vibration Dampers (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2558709A DE2558709C3 (de) | 1975-12-24 | 1975-12-24 | Elastomere Dämpfungseinrichtung |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT1065299B true IT1065299B (it) | 1985-02-25 |
Family
ID=5965648
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT30613/76A IT1065299B (it) | 1975-12-24 | 1976-12-20 | Dispositivo ammortizzatore elastomero |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4097193A (it) |
| DE (1) | DE2558709C3 (it) |
| FR (1) | FR2336299A1 (it) |
| GB (1) | GB1571305A (it) |
| IT (1) | IT1065299B (it) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4828202A (en) * | 1979-09-27 | 1989-05-09 | The Boeing Company | Method and apparatus for wideband vibration damping of reinforced skin structures |
| US4293053A (en) * | 1979-12-18 | 1981-10-06 | United Technologies Corporation | Sound absorbing structure |
| DE3004451C2 (de) * | 1980-02-07 | 1985-04-04 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Elastomere Dämpfungseinrichtung |
| DE3148903C2 (de) * | 1981-12-10 | 1985-05-02 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Elastomere Dämpfungseinrichtung für ein Rotorblatt |
| US4425980A (en) | 1981-12-14 | 1984-01-17 | The Boeing Company | Beam dampers for damping the vibrations of the skin of reinforced structures |
| FR2581708B1 (fr) * | 1985-05-09 | 1989-04-28 | Snecma | Capotage pour bord d'attaque d'aube de soufflante de turboreacteur |
| FR2602739B1 (fr) * | 1986-07-28 | 1988-11-18 | Aerospatiale | Pale en materiaux composites, a structure bilongeron et bicaisson, et a revetement stratifies a sandwich de nid d'abeilles, et son procede de fabrication |
| FR2608444B1 (fr) * | 1986-12-22 | 1989-03-31 | Rossignol Sa | Raquette de tennis |
| FR2631667B1 (fr) * | 1988-05-19 | 1993-09-03 | Alsthom | Materiau amortissant se presentant sous la forme d'une plaque a coller sur un support que l'on souhaite amortir ou a coller entre deux supports que l'on souhaite isoler l'un de l'autre |
| AT391088B (de) * | 1988-05-26 | 1990-08-10 | Head Sportgeraete Gmbh | Ski mit daempfungslagen |
| US4895491A (en) * | 1988-06-17 | 1990-01-23 | Environmental Elements Corp. | Fan blade protection system |
| US4954375A (en) * | 1988-12-29 | 1990-09-04 | Westinghouse Electric Corp. | Vibration damping apparatus |
| US5108262A (en) * | 1990-03-23 | 1992-04-28 | The United States Of America As Represented By The Secretary Of The Navy | High damping flexible propeller/impleller |
| US5145320A (en) * | 1990-08-28 | 1992-09-08 | The United States Of America As Represented By The Secretary Of The Navy | Mass loaded composite rotor for vibro-acoustic application |
| US5269656A (en) * | 1992-09-30 | 1993-12-14 | The United States Of America As Represented By The Secretary Of The Navy | High damping limp propeller |
| CA2149673C (en) * | 1992-12-23 | 1998-08-18 | Francis E. Byrnes | Tubular elastomer damper |
| US5913659A (en) * | 1993-11-22 | 1999-06-22 | United Technologies Corporation | Apparatus and method for adjusting rotor blade tracking |
| US5542820A (en) * | 1994-12-23 | 1996-08-06 | United Technologies Corporation | Engineered ceramic components for the leading edge of a helicopter rotor blade |
| DE19620427C1 (de) * | 1996-05-21 | 1997-06-12 | Eurocopter Deutschland | Rotorblattanschluß |
| ITMI991124A1 (it) * | 1998-05-28 | 2000-11-21 | Eurocopter Deutschland | Pala per un rotore privo di supporto di un elicottero |
| CH695461A5 (de) * | 2002-01-22 | 2006-05-31 | Alstom Technology Ltd | Verfahren zur Frequenzveränderung von Schaufeln für thermische Strömungsmaschinen. |
| US7360997B2 (en) * | 2005-10-06 | 2008-04-22 | General Electric Company | Vibration damper coating |
| BRPI0520633A2 (pt) * | 2005-11-03 | 2009-05-19 | Vestas Wind Sys As | pá de turbina eólica, turbina eólica, meio de amortecimento de oscilações para amortecimento de oscilações ou vibrações entre bordas de uma pá de turbina eólica, método de amortecimento de oscilações de uma pá de turbina eólica, e uso de um meio de amortecimento de oscilações em uma pá de turbina eólica |
| GB2438185A (en) * | 2006-05-17 | 2007-11-21 | Rolls Royce Plc | An apparatus for preventing ice accretion |
| FR2921099B1 (fr) * | 2007-09-13 | 2013-12-06 | Snecma | Dispositif d'amortissement pour aube en materiau composite |
| FR2943102B1 (fr) * | 2009-03-12 | 2014-05-02 | Snecma | Aube en materiau composite comportant un dispositif d'amortissement. |
| US9234556B1 (en) | 2014-08-29 | 2016-01-12 | Aktiebolaget Skf | Elastomer having tear reducing contoured edges |
| WO2016118409A1 (en) * | 2015-01-20 | 2016-07-28 | Sikorsky Aircraft Corporation | Enhanced durability nickel abrasion strip |
| DE102015203868A1 (de) | 2015-03-04 | 2016-09-08 | Rolls-Royce Deutschland Ltd & Co Kg | Fanschaufel für einen Flugantrieb |
| US10371097B2 (en) * | 2016-07-07 | 2019-08-06 | General Electric Company | Non-Newtonian materials in aircraft engine airfoils |
| US10793254B2 (en) * | 2016-12-12 | 2020-10-06 | Textron Innovations Inc. | Soft-in-plane proprotor systems |
| EP3712461A1 (de) * | 2019-03-22 | 2020-09-23 | GMT Gummi-Metall-Technik GmbH | Federelement und brandhemmende deckschicht |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA545510A (en) * | 1957-08-27 | A. V. Roe Canada Limited | Blade mounting | |
| US1842178A (en) * | 1930-02-15 | 1932-01-19 | Westinghouse Electric & Mfg Co | Propeller |
| GB452841A (en) * | 1935-04-12 | 1936-08-31 | Robert Rhodius | Improvements in screw propellers for aircraft |
| US2426123A (en) * | 1943-02-27 | 1947-08-19 | United Aircraft Corp | Helicopter blade |
| US2431184A (en) * | 1943-09-23 | 1947-11-18 | United Aireraft Corp | Composite blade |
| US3357850A (en) * | 1963-05-09 | 1967-12-12 | Gen Electric | Vibration damping turbomachinery blade |
| US3327812A (en) * | 1965-10-14 | 1967-06-27 | B J Lazan | Damping means |
| US3814540A (en) * | 1972-01-27 | 1974-06-04 | B Schramm | Helicopter rotor blade |
| US3796513A (en) * | 1972-06-19 | 1974-03-12 | Westinghouse Electric Corp | High damping blades |
| US4006999A (en) * | 1975-07-17 | 1977-02-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Leading edge protection for composite blades |
-
1975
- 1975-12-24 DE DE2558709A patent/DE2558709C3/de not_active Expired
-
1976
- 1976-12-17 US US05/751,698 patent/US4097193A/en not_active Expired - Lifetime
- 1976-12-20 IT IT30613/76A patent/IT1065299B/it active
- 1976-12-20 GB GB53189/76A patent/GB1571305A/en not_active Expired
- 1976-12-20 FR FR7638388A patent/FR2336299A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| DE2558709C3 (de) | 1982-02-11 |
| GB1571305A (en) | 1980-07-16 |
| US4097193A (en) | 1978-06-27 |
| DE2558709A1 (de) | 1977-07-07 |
| FR2336299B1 (it) | 1982-09-24 |
| DE2558709B2 (de) | 1981-06-11 |
| FR2336299A1 (fr) | 1977-07-22 |
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