GB614623A - Improvements in and relating to rotative aerofoils with propulsive ducts - Google Patents
Improvements in and relating to rotative aerofoils with propulsive ductsInfo
- Publication number
- GB614623A GB614623A GB2215646A GB2215646A GB614623A GB 614623 A GB614623 A GB 614623A GB 2215646 A GB2215646 A GB 2215646A GB 2215646 A GB2215646 A GB 2215646A GB 614623 A GB614623 A GB 614623A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- duct
- swept
- aerofoils
- rotative
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor
Abstract
614,623. Helicopters. CIERVA AUTOGIRO CO., Ltd., SHAPIRO, J. S., and PULLIN, C. G. July 25, 1946, No. 22156. [Class 4] [Also in Group XXVI] A blade of a helicopter or like rotor is provided with a propulsive duct of the continuous flow or intermittent type at its outer extremity, the blade being generally straight, except at the portion adjacent the duct where it has a pronounced sweep-back or sweep-forward. Fig. 1 shows a blade 5 with a swept-forward portion carrying the duct 6 in an inclined position, as in Specification 614,624. In order to minimise the twisting moment on the blade, the latter may be given a curved form comprising a swept-back portion joined to the straight inner portion of the blade, continued by a swept-forward portion carrying the duct, or the reverse arrangement may be adopted.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2215646A GB614623A (en) | 1946-07-25 | 1946-07-25 | Improvements in and relating to rotative aerofoils with propulsive ducts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2215646A GB614623A (en) | 1946-07-25 | 1946-07-25 | Improvements in and relating to rotative aerofoils with propulsive ducts |
Publications (1)
Publication Number | Publication Date |
---|---|
GB614623A true GB614623A (en) | 1948-12-17 |
Family
ID=10174835
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2215646A Expired GB614623A (en) | 1946-07-25 | 1946-07-25 | Improvements in and relating to rotative aerofoils with propulsive ducts |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB614623A (en) |
-
1946
- 1946-07-25 GB GB2215646A patent/GB614623A/en not_active Expired
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