GB267313A - Improvements in aeronautical propellers - Google Patents
Improvements in aeronautical propellersInfo
- Publication number
- GB267313A GB267313A GB714526A GB714526A GB267313A GB 267313 A GB267313 A GB 267313A GB 714526 A GB714526 A GB 714526A GB 714526 A GB714526 A GB 714526A GB 267313 A GB267313 A GB 267313A
- Authority
- GB
- United Kingdom
- Prior art keywords
- boss
- keyways
- liner
- keyed
- thickness
- 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
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forging (AREA)
Abstract
267,313. Reed, S. A. March 15, 1926. Screw propellers.-Metal air screws with thin blades are forged with a central boss enlargement, the blades being of such thickness that they would deflect at speeds without the compensation of centrifugal forces. The central boss is formed by hot die forging, the blade portions being finished by cold working. An alloy of aluminium or magnesium is the preferred material. The thickness of the blade at one-tenth the length from the root does not exceed one-fiftyfourth of the length. The boss may be bolted or keyed to the engine shaft direct or may be provided with liner 6 of hard metal keyed by keys 12 to the boss and having keyways 9 and an internal cone 8 for fitting on the coned end of the engine shaft. In a modification, the 'liner has integral fins in place of separate keys which slide in keyways in the boss and when in position are pinned. Specifications 163,714, 199,708, 223,838, and 240,594 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB714526A GB267313A (en) | 1926-03-15 | 1926-03-15 | Improvements in aeronautical propellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB714526A GB267313A (en) | 1926-03-15 | 1926-03-15 | Improvements in aeronautical propellers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB267313A true GB267313A (en) | 1927-03-17 |
Family
ID=9827466
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB714526A Expired GB267313A (en) | 1926-03-15 | 1926-03-15 | Improvements in aeronautical propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB267313A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6393701B1 (en) * | 1997-12-19 | 2002-05-28 | Robert Bosch Gmbh | Manually operated electric machine tool |
CN106081096A (en) * | 2016-07-27 | 2016-11-09 | 上海未来伙伴机器人有限公司 | Paddle device, paddle device manufacture method and multi-rotor aerocraft |
-
1926
- 1926-03-15 GB GB714526A patent/GB267313A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6393701B1 (en) * | 1997-12-19 | 2002-05-28 | Robert Bosch Gmbh | Manually operated electric machine tool |
CN106081096A (en) * | 2016-07-27 | 2016-11-09 | 上海未来伙伴机器人有限公司 | Paddle device, paddle device manufacture method and multi-rotor aerocraft |
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