GB569167A - Improvements in propeller hub fairings - Google Patents
Improvements in propeller hub fairingsInfo
- Publication number
- GB569167A GB569167A GB1191243A GB1191243A GB569167A GB 569167 A GB569167 A GB 569167A GB 1191243 A GB1191243 A GB 1191243A GB 1191243 A GB1191243 A GB 1191243A GB 569167 A GB569167 A GB 569167A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plate
- shank
- normal
- bulged portion
- spinner
- 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
- B64C11/14—Spinners
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Wind Motors (AREA)
Abstract
569,167. Variable-pitch airscrews. DE HAVILLAND AIRCRAFT CO., Ltd., WARDE, R. and KNIGHT, J. T. July 21, 1943, No. 11912. [Class 114] In a variable-pitch airscrew each blade shank 10 carries a circular plate 16 normal to, and having its centre on, the axis of rotation 18 of the blade, this plate lying within a circular aperture which is normal to the axis 18 and which is formed in an outwardly-bulged portion 22 of the spinner 12. The plate 16 may be flat or slightly convex outwardly, the bulged portion 22 may be formed integrally with, or separately from and secured to, the spinner 12, and the latter may be recessed slightly within its normal contour on the sides of the blades remote from its tip. The plate 16 may carry flexible sealing means to engage the edge of the aperture in the bulged portion 22. The plate 16 is secured by angles 30 to two clips 28 bolted onto the shank 10 bv bolts 26 which engage in shallow notches in, or beneath projections on, the shank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1191243A GB569167A (en) | 1943-07-21 | 1943-07-21 | Improvements in propeller hub fairings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1191243A GB569167A (en) | 1943-07-21 | 1943-07-21 | Improvements in propeller hub fairings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB569167A true GB569167A (en) | 1945-05-10 |
Family
ID=9994919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1191243A Expired GB569167A (en) | 1943-07-21 | 1943-07-21 | Improvements in propeller hub fairings |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB569167A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2793702A (en) * | 1953-05-08 | 1957-05-28 | Curtiss Wright Corp | Spinner fairing and seal |
| GB2127495A (en) * | 1982-09-28 | 1984-04-11 | Cessna Aircraft Co | Aircraft propeller and spinner arrangements |
| WO2014120384A1 (en) * | 2013-01-31 | 2014-08-07 | General Electric Company | Spinner assembly with removable fan blade leading edge fairings |
-
1943
- 1943-07-21 GB GB1191243A patent/GB569167A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2793702A (en) * | 1953-05-08 | 1957-05-28 | Curtiss Wright Corp | Spinner fairing and seal |
| GB2127495A (en) * | 1982-09-28 | 1984-04-11 | Cessna Aircraft Co | Aircraft propeller and spinner arrangements |
| WO2014120384A1 (en) * | 2013-01-31 | 2014-08-07 | General Electric Company | Spinner assembly with removable fan blade leading edge fairings |
| CN105102788A (en) * | 2013-01-31 | 2015-11-25 | 通用电气公司 | Spinner assembly with removable fan blade leading edge fairings |
| US9297257B2 (en) | 2013-01-31 | 2016-03-29 | General Electric Company | Spinner assembly with removable fan blade leading edge fairings |
| CN105102788B (en) * | 2013-01-31 | 2017-04-12 | 通用电气公司 | Spinner assembly with removable fan blade leading edge fairings |
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