GB320365A - Improvements in or relating to hollow metal air-screw propeller blades - Google Patents
Improvements in or relating to hollow metal air-screw propeller bladesInfo
- Publication number
- GB320365A GB320365A GB1342828A GB1342828A GB320365A GB 320365 A GB320365 A GB 320365A GB 1342828 A GB1342828 A GB 1342828A GB 1342828 A GB1342828 A GB 1342828A GB 320365 A GB320365 A GB 320365A
- Authority
- GB
- United Kingdom
- Prior art keywords
- diaphragms
- flanges
- blade
- relating
- spar
- 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
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/78—Making other particular articles propeller blades; turbine blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Wind Motors (AREA)
Abstract
320,365. Vickers, Ltd., and Pierson, R. K. May 7, 1928. Screw propellers.- Hollow airscrews formed with a central spar or rod carrying transverse diaphragms to which the thin sheet covering is secured are constructed with flanges on the diaphragms for securing them to the central spar and the blade sheets. The diaphragms may be conical. The central spar A, Fig. 1, tapers from root to tip and the diaphragms B have internal flanges B' pinned to the spar and external flanges B<3> to which the sheets F are secured, the outer sheet D being continued over to form the top and the leading edge C, Fig. 2, also being continued over to line up with the front and back plate sections. One face of the blade may be constituted by a single plate. Instead of the diaphragm flanges being parallel to the length of the blade they may be transversely disposed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1342828A GB320365A (en) | 1928-05-07 | 1928-05-07 | Improvements in or relating to hollow metal air-screw propeller blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1342828A GB320365A (en) | 1928-05-07 | 1928-05-07 | Improvements in or relating to hollow metal air-screw propeller blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB320365A true GB320365A (en) | 1929-10-07 |
Family
ID=10022783
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1342828A Expired GB320365A (en) | 1928-05-07 | 1928-05-07 | Improvements in or relating to hollow metal air-screw propeller blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB320365A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3096826A (en) * | 1961-08-07 | 1963-07-09 | Hughes Tool Co | Rotor blade for rotary-winged aircraft |
US3400904A (en) * | 1966-12-19 | 1968-09-10 | James R. Bede | Airfoil construction |
-
1928
- 1928-05-07 GB GB1342828A patent/GB320365A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3096826A (en) * | 1961-08-07 | 1963-07-09 | Hughes Tool Co | Rotor blade for rotary-winged aircraft |
US3400904A (en) * | 1966-12-19 | 1968-09-10 | James R. Bede | Airfoil construction |
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