GB588112A - Improvements in variable-pitch airscrews - Google Patents
Improvements in variable-pitch airscrewsInfo
- Publication number
- GB588112A GB588112A GB2472244A GB2472244A GB588112A GB 588112 A GB588112 A GB 588112A GB 2472244 A GB2472244 A GB 2472244A GB 2472244 A GB2472244 A GB 2472244A GB 588112 A GB588112 A GB 588112A
- Authority
- GB
- United Kingdom
- Prior art keywords
- variable
- pitch
- tip
- blade
- pitch airscrews
- 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
- B64C11/20—Constructional features
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- General Details Of Gearings (AREA)
Abstract
588,112. Variable-pitch propellers. DE HAVILLAND AIRCRAFT CO., Ltd., and THORBURN, J. W. Dec. 9, 1944, No. 24722. [Class 114] A propeller of which the blade pitch can be adjusted by the hydraulic gear 22, and bevel gear 18. The turning moment due to centrifugal force is balanced by a torsion tube 26, secured to the blade tip at 30, and to the hub at 28. The tube section is circular at its root and is progressively flattened towards the tip.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2472244A GB588112A (en) | 1944-12-09 | 1944-12-09 | Improvements in variable-pitch airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2472244A GB588112A (en) | 1944-12-09 | 1944-12-09 | Improvements in variable-pitch airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB588112A true GB588112A (en) | 1947-05-14 |
Family
ID=10216230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2472244A Expired GB588112A (en) | 1944-12-09 | 1944-12-09 | Improvements in variable-pitch airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB588112A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3141437A (en) * | 1958-05-23 | 1964-07-21 | Scherer | Constant lift system for craft |
US3167129A (en) * | 1962-05-16 | 1965-01-26 | Enstrom Corp | Construction of airfoils having elastically-bent afterbodies |
US4274807A (en) * | 1978-07-31 | 1981-06-23 | Kenney Clarence E | Speed control system for a windmill |
US4364708A (en) * | 1981-08-27 | 1982-12-21 | David Constant V | Windmill |
WO2012047337A1 (en) * | 2010-10-08 | 2012-04-12 | Oliver Vtol, Llc | Three wing, six tilt-propulsion unit, vtol aircraft |
US8616492B2 (en) | 2009-10-09 | 2013-12-31 | Oliver Vtol, Llc | Three wing, six tilt-propulsion units, VTOL aircraft |
US8708273B2 (en) | 2009-10-09 | 2014-04-29 | Oliver Vtol, Llc | Three-wing, six tilt-propulsion unit, VTOL aircraft |
US8800912B2 (en) | 2009-10-09 | 2014-08-12 | Oliver Vtol, Llc | Three wing, six-tilt propulsion unit, VTOL aircraft |
-
1944
- 1944-12-09 GB GB2472244A patent/GB588112A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3141437A (en) * | 1958-05-23 | 1964-07-21 | Scherer | Constant lift system for craft |
US3167129A (en) * | 1962-05-16 | 1965-01-26 | Enstrom Corp | Construction of airfoils having elastically-bent afterbodies |
US4274807A (en) * | 1978-07-31 | 1981-06-23 | Kenney Clarence E | Speed control system for a windmill |
US4364708A (en) * | 1981-08-27 | 1982-12-21 | David Constant V | Windmill |
US8616492B2 (en) | 2009-10-09 | 2013-12-31 | Oliver Vtol, Llc | Three wing, six tilt-propulsion units, VTOL aircraft |
US8708273B2 (en) | 2009-10-09 | 2014-04-29 | Oliver Vtol, Llc | Three-wing, six tilt-propulsion unit, VTOL aircraft |
US8800912B2 (en) | 2009-10-09 | 2014-08-12 | Oliver Vtol, Llc | Three wing, six-tilt propulsion unit, VTOL aircraft |
WO2012047337A1 (en) * | 2010-10-08 | 2012-04-12 | Oliver Vtol, Llc | Three wing, six tilt-propulsion unit, vtol aircraft |
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