IT1155131B - Mozzo di rotore di elicotteri - Google Patents
Mozzo di rotore di elicotteriInfo
- Publication number
- IT1155131B IT1155131B IT67302/82A IT6730282A IT1155131B IT 1155131 B IT1155131 B IT 1155131B IT 67302/82 A IT67302/82 A IT 67302/82A IT 6730282 A IT6730282 A IT 6730282A IT 1155131 B IT1155131 B IT 1155131B
- Authority
- IT
- Italy
- Prior art keywords
- rotor hub
- helicopter rotor
- helicopter
- hub
- rotor
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
- Centrifugal Separators (AREA)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT67302/82A IT1155131B (it) | 1982-03-11 | 1982-03-11 | Mozzo di rotore di elicotteri |
| DE3307311A DE3307311C2 (de) | 1982-03-11 | 1983-03-02 | Hubschrauber-Rotornabe |
| US06/471,343 US4521157A (en) | 1982-03-11 | 1983-03-02 | Helicopter rotor hub |
| GB08306342A GB2116505B (en) | 1982-03-11 | 1983-03-08 | A helicopter rotor hub |
| FR8303899A FR2523069B1 (fr) | 1982-03-11 | 1983-03-09 | Moyeu de rotor d'helicoptere |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT67302/82A IT1155131B (it) | 1982-03-11 | 1982-03-11 | Mozzo di rotore di elicotteri |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT8267302A0 IT8267302A0 (it) | 1982-03-11 |
| IT1155131B true IT1155131B (it) | 1987-01-21 |
Family
ID=11301278
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT67302/82A IT1155131B (it) | 1982-03-11 | 1982-03-11 | Mozzo di rotore di elicotteri |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4521157A (it) |
| DE (1) | DE3307311C2 (it) |
| FR (1) | FR2523069B1 (it) |
| GB (1) | GB2116505B (it) |
| IT (1) | IT1155131B (it) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1159375B (it) * | 1983-04-07 | 1987-02-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
| US4568244A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Fiber reinforced/epoxy matrix composite helicopter rotor main hub plate |
| DE3439257C2 (de) * | 1984-10-26 | 1986-10-23 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Rotor, insbesondere für ein Drehflügelflugzeug |
| IT1182448B (it) * | 1985-02-19 | 1987-10-05 | Agusta Aeronaut Costr | Mozzo metallico per un rotore di elicottero |
| US4804315A (en) * | 1987-07-30 | 1989-02-14 | United Technologies Corporation | Composite helicopter swashplate |
| US4797064A (en) * | 1987-07-30 | 1989-01-10 | United Technologies Corporation | Composite helicopter rotor hub |
| US4818179A (en) * | 1987-07-30 | 1989-04-04 | United Technologies Corporation | Composite helicopter rotor hub |
| US4930983A (en) * | 1988-09-26 | 1990-06-05 | United Technologies Corporation | Hybrid helicopter rotor hub retention plate |
| IN2014DN06523A (it) | 2012-01-25 | 2015-06-12 | Delta T Corp | |
| US10464666B2 (en) * | 2014-11-20 | 2019-11-05 | Sikorsky Aircraft Corporation | Composite reinforced swashplate |
| WO2018195539A1 (en) * | 2017-04-21 | 2018-10-25 | Evapco, Inc. | Cooling tower axial fan in a hollowed disc/ring configuration |
| USD1019492S1 (en) * | 2022-01-10 | 2024-03-26 | Fisher & Paykel Appliances Limited | Rotor hub |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3384185A (en) * | 1967-06-02 | 1968-05-21 | Aerojet General Co | Rotor hubs |
| DE2150741C3 (de) * | 1971-10-12 | 1973-11-22 | Messerschmitt Boelkow Blohm | Schlag- und schwenkgelenklose Aufhaengung der Rotorblaetter eines Drehfluegelflugzeuges am Rotorkopf |
| US3761199A (en) * | 1972-07-14 | 1973-09-25 | United Aircraft Corp | Helicopter rotor with redundant load carrying capability |
| DE2648343C3 (de) * | 1976-10-26 | 1981-06-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag- und schwenkgelenkloser Rotor für Drehflügelflugzeuge |
| DE2916727A1 (de) * | 1977-03-23 | 1980-11-06 | Messerschmitt Boelkow Blohm | Rotor eines drehfluegelflugzeugs |
| DE2722250A1 (de) * | 1977-03-23 | 1978-11-23 | Messerschmitt Boelkow Blohm | Rotor eines drehfluegelflugzeugs |
| US4156583A (en) * | 1977-07-11 | 1979-05-29 | Kaman Aerospace Corporation | Hub assembly |
| IT1117626B (it) * | 1979-02-02 | 1986-02-17 | Aereonautiche Giovanni Augusta | Rotore articolato per elicotteri |
| US4321013A (en) * | 1979-04-25 | 1982-03-23 | Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung | Headpiece support for rotor of a rotary wing aircraft |
| DE3006088A1 (de) * | 1980-02-19 | 1981-08-20 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor eines drehfluegelflugzeugs |
| IT1143358B (it) * | 1981-02-05 | 1986-10-22 | Agusta Aeronaut Costr | Mozzo composito di un rotore di elicottero |
-
1982
- 1982-03-11 IT IT67302/82A patent/IT1155131B/it active
-
1983
- 1983-03-02 US US06/471,343 patent/US4521157A/en not_active Expired - Lifetime
- 1983-03-02 DE DE3307311A patent/DE3307311C2/de not_active Expired - Lifetime
- 1983-03-08 GB GB08306342A patent/GB2116505B/en not_active Expired
- 1983-03-09 FR FR8303899A patent/FR2523069B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE3307311A1 (de) | 1983-09-22 |
| FR2523069B1 (fr) | 1986-02-21 |
| GB8306342D0 (en) | 1983-04-13 |
| GB2116505A (en) | 1983-09-28 |
| FR2523069A1 (fr) | 1983-09-16 |
| DE3307311C2 (de) | 1996-06-27 |
| IT8267302A0 (it) | 1982-03-11 |
| GB2116505B (en) | 1986-01-08 |
| US4521157A (en) | 1985-06-04 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19990330 |