GB901820A - Improvements relating to the bladed rotors of rotary winged aircraft - Google Patents
Improvements relating to the bladed rotors of rotary winged aircraftInfo
- Publication number
- GB901820A GB901820A GB1170960A GB1170960A GB901820A GB 901820 A GB901820 A GB 901820A GB 1170960 A GB1170960 A GB 1170960A GB 1170960 A GB1170960 A GB 1170960A GB 901820 A GB901820 A GB 901820A
- Authority
- GB
- United Kingdom
- Prior art keywords
- improvements relating
- bladed rotors
- winged aircraft
- blades
- rotary winged
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
901,820. Rotary wing aircraft. SMITH, A. L. March 27, 1961 [April 2, 1960], No. 11709/60. Class 4. A rotor for a rotary wing aircraft comprises a hub a carrying four blades each sectorshape in plan, the upper and lower walls b, b<SP>1</SP> converging rearwardly to be left open at their forward edges but closed at their rear edges by a plate b<SP>3</SP>, slotted at b<SP>4</SP>, and at their outer arcuate edges by a plate b<SP>2</SP>. It is stated that during rotation of the rotor air expelled through the slots b<SP>4</SP> is ejected either into the interior of the following blade or below the blade, depending upon the angle of incidence of the blades.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1170960A GB901820A (en) | 1960-04-02 | 1960-04-02 | Improvements relating to the bladed rotors of rotary winged aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1170960A GB901820A (en) | 1960-04-02 | 1960-04-02 | Improvements relating to the bladed rotors of rotary winged aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB901820A true GB901820A (en) | 1962-07-25 |
Family
ID=9991245
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1170960A Expired GB901820A (en) | 1960-04-02 | 1960-04-02 | Improvements relating to the bladed rotors of rotary winged aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB901820A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3371718A (en) * | 1966-09-07 | 1968-03-05 | Henry S. Bacon | Rotary jet reaction motors |
US5341565A (en) * | 1993-06-15 | 1994-08-30 | William Kuryliw | Method of securing a filter element to a blade of a fan |
GB2334501A (en) * | 1997-10-08 | 1999-08-25 | Lacroix Soc E | Rotating wing device for retarding the fall of a load |
CN114590400A (en) * | 2022-03-09 | 2022-06-07 | 南京航空航天大学 | A coaxial belt sail rotor structure and its control method |
-
1960
- 1960-04-02 GB GB1170960A patent/GB901820A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3371718A (en) * | 1966-09-07 | 1968-03-05 | Henry S. Bacon | Rotary jet reaction motors |
US5341565A (en) * | 1993-06-15 | 1994-08-30 | William Kuryliw | Method of securing a filter element to a blade of a fan |
GB2334501A (en) * | 1997-10-08 | 1999-08-25 | Lacroix Soc E | Rotating wing device for retarding the fall of a load |
GB2334501B (en) * | 1997-10-08 | 2001-11-14 | Lacroix Soc E | A device for braking the fall of a load |
CN114590400A (en) * | 2022-03-09 | 2022-06-07 | 南京航空航天大学 | A coaxial belt sail rotor structure and its control method |
CN114590400B (en) * | 2022-03-09 | 2022-12-20 | 南京航空航天大学 | Coaxial sail-type rotor structure with wings and control method thereof |
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