GB577524A - Improvement in airing of anti-torque propeller - Google Patents
Improvement in airing of anti-torque propellerInfo
- Publication number
- GB577524A GB577524A GB10510/44A GB1051044A GB577524A GB 577524 A GB577524 A GB 577524A GB 10510/44 A GB10510/44 A GB 10510/44A GB 1051044 A GB1051044 A GB 1051044A GB 577524 A GB577524 A GB 577524A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- air
- airing
- improvement
- june
- 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
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8245—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft using air jets
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
577,524. Propellers; helicopters. BOSSI, E. June 1, 1944, No. 10510. Convention date, June 4, 1943. [Class 4] An anti-torque propeller for a rotary wing aircraft rotatable about a horizontal shaft 5 laterally of and close to a side wall of the tail end of the fuselage, has air supplied to the sector covered by the fuselage from an outlet 11 in the fuselage. The air may be forced into the fuselage from the blades 3 of the rotary wing system. The air-inlet port 13 is adjustable by the pilot.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US577524XA | 1943-06-04 | 1943-06-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB577524A true GB577524A (en) | 1946-05-21 |
Family
ID=22012543
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10510/44A Expired GB577524A (en) | 1943-06-04 | 1944-06-01 | Improvement in airing of anti-torque propeller |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB577524A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3065933A (en) * | 1960-05-20 | 1962-11-27 | Frank Krause Jr A | Helicopter |
DE4039027A1 (en) * | 1989-12-08 | 1991-06-13 | Westland Helicopters | COMPOSITE HELICOPTER |
GB2249770A (en) * | 1990-11-19 | 1992-05-20 | Thomas Thomson Gardner | Helicopter downdraught controls |
EP2460720A1 (en) | 2010-12-06 | 2012-06-06 | Eurocopter | Structural element of a rotorcraft for reducing aerodynamic drag |
-
1944
- 1944-06-01 GB GB10510/44A patent/GB577524A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3065933A (en) * | 1960-05-20 | 1962-11-27 | Frank Krause Jr A | Helicopter |
DE4039027A1 (en) * | 1989-12-08 | 1991-06-13 | Westland Helicopters | COMPOSITE HELICOPTER |
GB2249770A (en) * | 1990-11-19 | 1992-05-20 | Thomas Thomson Gardner | Helicopter downdraught controls |
EP2460720A1 (en) | 2010-12-06 | 2012-06-06 | Eurocopter | Structural element of a rotorcraft for reducing aerodynamic drag |
FR2968272A1 (en) * | 2010-12-06 | 2012-06-08 | Eurocopter France | IMPROVED STRUCTURE ELEMENT OF A GIRAVION TO DECREASE AERODYNAMIC TRAINING. |
US8827201B2 (en) | 2010-12-06 | 2014-09-09 | Airbus Helicopters | Rotorcraft structural element for reducing aerodynamic drag |
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