IT1074433B - Raccordo di pala su un mozzo di rotore per rotori non snodati di elicotteri - Google Patents
Raccordo di pala su un mozzo di rotore per rotori non snodati di elicotteriInfo
- Publication number
- IT1074433B IT1074433B IT27257/76A IT2725776A IT1074433B IT 1074433 B IT1074433 B IT 1074433B IT 27257/76 A IT27257/76 A IT 27257/76A IT 2725776 A IT2725776 A IT 2725776A IT 1074433 B IT1074433 B IT 1074433B
- Authority
- IT
- Italy
- Prior art keywords
- jointed
- rotor hub
- helicopter rotors
- shovel
- fitting
- 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
- B64C27/473—Constructional features
- B64C27/48—Root attachment to rotor head
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/51—Damping of blade movements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Harvester Elements (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2541998A DE2541998C2 (de) | 1975-09-20 | 1975-09-20 | Hubschrauberrotornabe mit schlag- und schwenkgelenklosem Blattanschluß |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT1074433B true IT1074433B (it) | 1985-04-20 |
Family
ID=5956983
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT27257/76A IT1074433B (it) | 1975-09-20 | 1976-09-16 | Raccordo di pala su un mozzo di rotore per rotori non snodati di elicotteri |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4086024A (it) |
| JP (1) | JPS5241399A (it) |
| DE (1) | DE2541998C2 (it) |
| FR (1) | FR2324512A1 (it) |
| GB (1) | GB1563312A (it) |
| IT (1) | IT1074433B (it) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2648343C3 (de) * | 1976-10-26 | 1981-06-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag- und schwenkgelenkloser Rotor für Drehflügelflugzeuge |
| DE2722250A1 (de) * | 1977-03-23 | 1978-11-23 | Messerschmitt Boelkow Blohm | Rotor eines drehfluegelflugzeugs |
| FR2397326A2 (fr) * | 1977-07-13 | 1979-02-09 | Aerospatiale | Rotor sans articulations, en particulier pour un giravion |
| FR2397327A1 (fr) * | 1977-07-13 | 1979-02-09 | Aerospatiale | Rotor a pas variable, en particulier pour un giravion |
| FR2516891A1 (fr) * | 1981-11-25 | 1983-05-27 | Aerospatiale | Rotor pour giravions, a articulations integrees dans le pied de pale |
| US4466774A (en) * | 1982-08-30 | 1984-08-21 | United Technologies Corporation | Composite flexbeam joint |
| FR2542695B1 (fr) * | 1983-03-18 | 1985-07-26 | Aerospatiale | Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees |
| WO2009100377A1 (en) | 2008-02-07 | 2009-08-13 | Wind Innovatins Ip, Llc | Rotor hub maintenance system |
| EP2653383B1 (en) * | 2012-04-18 | 2016-04-13 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An airfoil blade of a bearingless rotor of a helicopter |
| GB2631699B (en) * | 2023-07-07 | 2025-10-15 | Certo Aerospace Ltd | Rotor damping mechanism |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA527572A (en) * | 1956-07-10 | H. Stanley Paul | Aircraft rotor with tilting hub and damper control of blade swinging | |
| DE585108C (de) * | 1931-06-29 | 1933-10-02 | Cierva Autogiro Co Ltd | Flugzeug mit Tragflaechenrotor |
| US1948457A (en) * | 1931-06-29 | 1934-02-20 | Autogiro Co Of America | Aircraft sustaining rotor |
| FR737360A (fr) * | 1931-06-29 | 1932-12-10 | Cierva Autogiro Co Ltd | Perfectionnements dans les rotors de sustentation des aéronefs |
| US1971016A (en) * | 1931-09-05 | 1934-08-21 | Autogiro Co Of America | Aircraft having sustaining rotors |
| US1950080A (en) * | 1931-09-10 | 1934-03-06 | Autogiro Co Of America | Aircraft of the rotative wing type |
| US1995460A (en) * | 1931-10-07 | 1935-03-26 | Autogiro Co Of America | Aircraft rotative wing mounting |
| US2122450A (en) * | 1934-07-06 | 1938-07-05 | Autogiro Co Of America | Aircraft with rotatable sustaining means |
| US2311247A (en) * | 1941-09-24 | 1943-02-16 | Autogiro Co Of America | Blade mounting for rotary wing aircraft |
| US3106965A (en) * | 1961-10-02 | 1963-10-15 | Lord Mfg Co | Rotor head |
| DE1531375C3 (de) * | 1967-09-14 | 1974-04-11 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Schlag- und schwenkgelenkloser, aber nicht starrer Rotor |
| US3556673A (en) * | 1968-10-11 | 1971-01-19 | Bolkow Gmbh | Rotor mounting |
| DE1963928A1 (de) * | 1969-12-20 | 1970-07-02 | Messerschmitt Boelkow Blohm | Lagerung der Rotorblaetter von Drehfluegelflugzeugen |
| US3700352A (en) * | 1971-03-05 | 1972-10-24 | Lord Corp | Rotor system |
| US3790302A (en) * | 1972-10-10 | 1974-02-05 | Textron Inc | Tail rotor mounting for coning relief |
| GB1432117A (en) * | 1973-05-10 | 1976-04-14 | Aerospatiale | Rotor for rotating wing type aircraft |
| US3862812A (en) * | 1973-07-18 | 1975-01-28 | Lord Corp | Rotor blade retention system |
-
1975
- 1975-09-20 DE DE2541998A patent/DE2541998C2/de not_active Expired
-
1976
- 1976-09-15 US US05/723,440 patent/US4086024A/en not_active Expired - Lifetime
- 1976-09-15 GB GB38241/76A patent/GB1563312A/en not_active Expired
- 1976-09-16 IT IT27257/76A patent/IT1074433B/it active
- 1976-09-17 FR FR7628061A patent/FR2324512A1/fr active Granted
- 1976-09-20 JP JP51111902A patent/JPS5241399A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE2541998C2 (de) | 1981-10-15 |
| FR2324512A1 (fr) | 1977-04-15 |
| FR2324512B1 (it) | 1982-10-22 |
| JPS5241399A (en) | 1977-03-30 |
| DE2541998A1 (de) | 1977-03-24 |
| US4086024A (en) | 1978-04-25 |
| GB1563312A (en) | 1980-03-26 |
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