GB460513A - Improvements in or relating to blades for airscrews and the like - Google Patents
Improvements in or relating to blades for airscrews and the likeInfo
- Publication number
- GB460513A GB460513A GB2934136A GB2934136A GB460513A GB 460513 A GB460513 A GB 460513A GB 2934136 A GB2934136 A GB 2934136A GB 2934136 A GB2934136 A GB 2934136A GB 460513 A GB460513 A GB 460513A
- Authority
- GB
- United Kingdom
- Prior art keywords
- slot
- blade
- screws
- leading edge
- fairey
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
460,513. Air-screws. FAIREY, C. R., and FAIREY AVIATION CO., Ltd. April 4, 1936, No. 29341. Divided out of and addition to 457,823. [Class 114] In front of the leading edge of an airscrew blade and along the part near the boss a slot is provided for controlling the flow of fluid over the blade. A slat member e provided with brackets f is mounted in front of the leading edge b of a blade a, being secured thereto by screws. The slot between the two parts a and e may be straight or simple curved or compound curved. In place of a single slat member e a number of discontinuous slats may be substituted. The width of the slot at the front surface is from 5-12 per cent of the chord.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2934136A GB460513A (en) | 1936-04-04 | 1936-04-04 | Improvements in or relating to blades for airscrews and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2934136A GB460513A (en) | 1936-04-04 | 1936-04-04 | Improvements in or relating to blades for airscrews and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB460513A true GB460513A (en) | 1937-01-28 |
Family
ID=10290015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2934136A Expired GB460513A (en) | 1936-04-04 | 1936-04-04 | Improvements in or relating to blades for airscrews and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB460513A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3721295C1 (en) * | 1987-06-27 | 1988-12-08 | Deutsche Forsch Luft Raumfahrt | Propeller, the blades of which are provided with a wing |
US6602054B1 (en) | 2001-10-08 | 2003-08-05 | Norman Sherman | Fluid motor apparatus for amplifying thrust |
EP2660150A3 (en) * | 2012-05-04 | 2013-11-27 | Sikorsky Aircraft Corporation | Multi-element rotor blade |
-
1936
- 1936-04-04 GB GB2934136A patent/GB460513A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3721295C1 (en) * | 1987-06-27 | 1988-12-08 | Deutsche Forsch Luft Raumfahrt | Propeller, the blades of which are provided with a wing |
EP0297321A1 (en) * | 1987-06-27 | 1989-01-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Propeller with slat equipped blades |
US4840540A (en) * | 1987-06-27 | 1989-06-20 | Deutsche Forchungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. | Propeller whose blades are provided with slats |
US6602054B1 (en) | 2001-10-08 | 2003-08-05 | Norman Sherman | Fluid motor apparatus for amplifying thrust |
EP2660150A3 (en) * | 2012-05-04 | 2013-11-27 | Sikorsky Aircraft Corporation | Multi-element rotor blade |
US9211950B2 (en) | 2012-05-04 | 2015-12-15 | Sikorsky Aircraft Corporation | Multi-element rotor blade |
EP3103718A1 (en) * | 2012-05-04 | 2016-12-14 | Sikorsky Aircraft Corporation | Multi-element rotor blade |
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