JPS5097100A - - Google Patents
Info
- Publication number
- JPS5097100A JPS5097100A JP50004159A JP415975A JPS5097100A JP S5097100 A JPS5097100 A JP S5097100A JP 50004159 A JP50004159 A JP 50004159A JP 415975 A JP415975 A JP 415975A JP S5097100 A JPS5097100 A JP S5097100A
- Authority
- JP
- Japan
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/003—Variable-diameter propellers; Mechanisms therefor
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Catching Or Destruction (AREA)
- Braking Arrangements (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US428480A US3884594A (en) | 1973-12-26 | 1973-12-26 | Variable length blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5097100A true JPS5097100A (ja) | 1975-08-01 |
Family
ID=23699077
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP50004159A Pending JPS5097100A (ja) | 1973-12-26 | 1974-12-25 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3884594A (ja) |
| JP (1) | JPS5097100A (ja) |
| CA (1) | CA1001144A (ja) |
| DE (1) | DE2453039A1 (ja) |
| FR (1) | FR2256332A1 (ja) |
| GB (1) | GB1491253A (ja) |
| IT (1) | IT1028036B (ja) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5253979A (en) * | 1992-06-01 | 1993-10-19 | United Technologies Corporation | Variable diameter rotor having an offset twist |
| US5299912A (en) * | 1992-07-28 | 1994-04-05 | United Technologies Corporation | Drive system for changing the diameter of a variable diameter rotor |
| US5636969A (en) * | 1995-03-28 | 1997-06-10 | Sikorsky Aircraft Corporation | Torque tube/spar assembly for variable diameter helicopter rotors |
| US5655879A (en) * | 1995-03-28 | 1997-08-12 | Sikorsky Aircraft Corporation | Mounting arrangement for variable diameter rotor blade assemblies |
| US5642982A (en) * | 1995-12-11 | 1997-07-01 | Sikorsky Aircraft Corporation | Retraction/extension mechanism for variable diameter rotors |
| US5620303A (en) * | 1995-12-11 | 1997-04-15 | Sikorsky Aircraft Corporation | Rotor system having alternating length rotor blades for reducing blade-vortex interaction (BVI) noise |
| US5735670A (en) * | 1995-12-11 | 1998-04-07 | Sikorsky Aircraft Corporation | Rotor system having alternating length rotor blades and positioning means therefor for reducing blade-vortex interaction (BVI) noise |
| US5620304A (en) * | 1995-12-11 | 1997-04-15 | Sikorsky Aircraft Corporation | Rotor system having alternating length rotor blades and positioning means therefor for reducing blade-vortex interaction (BVI) noise |
| US6030177A (en) | 1998-12-18 | 2000-02-29 | Sikorsky Aircraft Corporation | Drive system for a variable diameter tilt rotor |
| US6019578A (en) | 1998-12-18 | 2000-02-01 | Sikorsky Aircraft Corporation | Variable diameter rotor blade actuation system |
| US6132329A (en) * | 1999-07-07 | 2000-10-17 | Meritor Heavy Vehicle Systems, Llc | Axle assembly lubricant temperature reduction apparatus |
| RU2258638C2 (ru) * | 2003-07-29 | 2005-08-20 | Лебедев Виктор Борисович | Способ изменения диаметра несущего винта и несущий винт |
| US8152466B2 (en) * | 2008-04-30 | 2012-04-10 | Agustawestland North America, Inc. | Centrifugal force actuated variable span helicopter rotor |
| RU2569165C1 (ru) * | 2014-09-09 | 2015-11-20 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" (АО "ВПК "НПО машиностроения") | Самолет |
| US10604247B2 (en) | 2015-06-11 | 2020-03-31 | Sikorsky Aircraft Corporation | Tension torsion strap |
| CN112607003B (zh) * | 2020-11-25 | 2023-06-20 | 常州市长昊机械有限公司 | 一种易收纳式航空叶片 |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2163482A (en) * | 1936-01-01 | 1939-06-20 | Cameron Peter | Aircraft having rotative sustaining means |
| US2145413A (en) * | 1936-12-16 | 1939-01-31 | William A Belfield | Propeller |
| US3297094A (en) * | 1965-10-20 | 1967-01-10 | Boeing Co | Aircraft propelling assembly |
| US3768923A (en) * | 1969-09-18 | 1973-10-30 | United Aircraft Corp | Variable length blade |
| US3713751A (en) * | 1970-10-29 | 1973-01-30 | United Aircraft Corp | Aerodynamic blade with high stiffness-to-weight ratio |
-
1973
- 1973-12-26 US US428480A patent/US3884594A/en not_active Expired - Lifetime
-
1974
- 1974-10-07 CA CA210,930A patent/CA1001144A/en not_active Expired
- 1974-11-08 GB GB48455/74A patent/GB1491253A/en not_active Expired
- 1974-11-08 DE DE19742453039 patent/DE2453039A1/de active Pending
- 1974-11-13 FR FR7437366A patent/FR2256332A1/fr not_active Withdrawn
- 1974-12-24 IT IT31003/74A patent/IT1028036B/it active
- 1974-12-25 JP JP50004159A patent/JPS5097100A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| IT1028036B (it) | 1979-01-30 |
| FR2256332A1 (ja) | 1975-07-25 |
| US3884594A (en) | 1975-05-20 |
| GB1491253A (en) | 1977-11-09 |
| DE2453039A1 (de) | 1975-07-10 |
| CA1001144A (en) | 1976-12-07 |