GB518626A - Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller blades - Google Patents
Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller bladesInfo
- Publication number
- GB518626A GB518626A GB2532538A GB2532538A GB518626A GB 518626 A GB518626 A GB 518626A GB 2532538 A GB2532538 A GB 2532538A GB 2532538 A GB2532538 A GB 2532538A GB 518626 A GB518626 A GB 518626A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- moment
- centre
- centrifugal
- propeller blades
- 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
- B64C11/18—Aerodynamic features
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
518,626. Screw propellers. TENNANT, W. J. (Aviation Patents, Inc.). Aug. 29, 1938, No. 25325. Drawings to Specification. [Class 114] Screw propeller blades intended to be mounted for pitch adjustment are arranged so that the blade axis lies within the confines of the blade throughout the major length and the centre of gravity of the blade is located toward the leading edge of the blade from the blade axis whilst the centre of pressure of each blade section is closer to the leading edge than the centre of gravity, whereby there is 'substantial balance between the centrifugal and aerodynamic moments about the blade axis. The centre of pressure is selected so that the net blade torque at the extreme limits of the normal range of operation will be in opposite directions, and also the aerodynamic movement exceeds the centrifugal moment under take off conditions, whilst the reverse occurs at maximum flight conditions. At the time when the centrifugal moment equals the aerodynamic moment for a selected flight condition, the centrifugal, moment predominates in an inner radial zone of the blade whilst aerodynamic moment predominates in an outer zone and the two moments are locally equal at the junction of the two zones.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2532538A GB518626A (en) | 1938-08-29 | 1938-08-29 | Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2532538A GB518626A (en) | 1938-08-29 | 1938-08-29 | Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB518626A true GB518626A (en) | 1940-03-04 |
Family
ID=10225852
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2532538A Expired GB518626A (en) | 1938-08-29 | 1938-08-29 | Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB518626A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5057696A (en) * | 1991-01-25 | 1991-10-15 | Wind Harvest Co., Inc. | Vertical windmill with omnidirectional diffusion |
-
1938
- 1938-08-29 GB GB2532538A patent/GB518626A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5057696A (en) * | 1991-01-25 | 1991-10-15 | Wind Harvest Co., Inc. | Vertical windmill with omnidirectional diffusion |
WO1992013192A1 (en) * | 1991-01-25 | 1992-08-06 | Wind Harvest Co., Inc. | Self-braking windmill |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3127093A (en) | Ducted sustaining rotor for aircraft | |
US3297094A (en) | Aircraft propelling assembly | |
GB618475A (en) | Improvements in or relating to aircraft of the gyroplane type | |
US3101917A (en) | Ducted rotor with pressure balancing and lift augmenting means | |
GB1391940A (en) | Helicopter rotor blades | |
US2352186A (en) | Variable pitch propeller | |
GB518626A (en) | Improvements in or relating to aeronautical propeller blades and methods of locating the pitch axis of variable-pitch propeller blades | |
GB521868A (en) | Improvements in or relating to propelling or impelling apparatus of the axial flow type | |
GB588112A (en) | Improvements in variable-pitch airscrews | |
US2308477A (en) | Aircraft | |
GB948881A (en) | Airscrew with automatically variable pitch, especially for light aircraft | |
GB858706A (en) | Drag-reducing devices for aircraft propellers | |
US2365214A (en) | Screw propeller, particularly for aircraft | |
US2263449A (en) | Airplane | |
US1971820A (en) | Helicopter airscrew | |
US1777630A (en) | Lifting air screw for air vehicles | |
US2421692A (en) | Propulsion device | |
SU63835A1 (en) | Multiple Multiple Air Bleed Screw | |
US2406921A (en) | Aircraft | |
GB424140A (en) | Improvements relating to air-craft of the gyroplane type | |
GB596971A (en) | Improvements in automatic variable pitch propeller | |
GB536904A (en) | Aeroplanes | |
GB601952A (en) | Improvements in aircraft with sustaining airscrews | |
GB523357A (en) | Improved propulsion for aircraft | |
US1800439A (en) | Airplane |