CA1015342A - Nodal beam inertial flexure - Google Patents
Nodal beam inertial flexureInfo
- Publication number
- CA1015342A CA1015342A CA228,012A CA228012A CA1015342A CA 1015342 A CA1015342 A CA 1015342A CA 228012 A CA228012 A CA 228012A CA 1015342 A CA1015342 A CA 1015342A
- Authority
- CA
- Canada
- Prior art keywords
- flexure
- nodal
- beam inertial
- inertial
- nodal beam
- 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
-
- 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
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/40—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
- B64C2027/005—Vibration damping devices using suspended masses
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/475,824 US3945628A (en) | 1973-12-26 | 1974-06-03 | Nodal beam inertial flexure |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1015342A true CA1015342A (en) | 1977-08-09 |
Family
ID=23889313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA228,012A Expired CA1015342A (en) | 1974-06-03 | 1975-05-29 | Nodal beam inertial flexure |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS591639B2 (de) |
CA (1) | CA1015342A (de) |
DE (1) | DE2523599C2 (de) |
FR (1) | FR2275696A1 (de) |
GB (1) | GB1498222A (de) |
IT (1) | IT1035859B (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2474996A1 (fr) * | 1980-02-05 | 1981-08-07 | Aerospatiale | Dispositif de suspension antiresonnante pour helicoptere |
FR2623583B2 (fr) * | 1987-06-23 | 1990-04-20 | Hutchinson | Supports elastiques |
FR2617258B1 (fr) * | 1987-06-23 | 1989-11-17 | Hutchinson | Supports elastiques |
FR2728539A1 (fr) * | 1994-12-23 | 1996-06-28 | Eurocopter France | Dispositif de suspension anti-vibratoire bidirectionnelle pour rotor d'helicoptere |
US20090212475A1 (en) | 2005-07-03 | 2009-08-27 | Hermann Tropf | Fastening Means Preventing The Transmission of Shocks and Vibrations |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
BE790113A (fr) * | 1971-10-18 | 1973-04-13 | Textron Inc | Dispositif isolateur a l'egard des vibrations dans un helicoptere |
-
1975
- 1975-05-23 GB GB2267775A patent/GB1498222A/en not_active Expired
- 1975-05-27 IT IT4980975A patent/IT1035859B/it active
- 1975-05-28 DE DE19752523599 patent/DE2523599C2/de not_active Expired
- 1975-05-29 CA CA228,012A patent/CA1015342A/en not_active Expired
- 1975-06-03 JP JP50066118A patent/JPS591639B2/ja not_active Expired
- 1975-06-03 FR FR7517227A patent/FR2275696A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
AU8149575A (en) | 1976-11-25 |
FR2275696B1 (de) | 1979-06-08 |
DE2523599A1 (de) | 1975-12-11 |
FR2275696A1 (fr) | 1976-01-16 |
DE2523599C2 (de) | 1984-03-29 |
JPS5124000A (ja) | 1976-02-26 |
GB1498222A (en) | 1978-01-18 |
JPS591639B2 (ja) | 1984-01-13 |
IT1035859B (it) | 1979-10-20 |
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