GB145180A - Improvements in and relating to airscrews - Google Patents
Improvements in and relating to airscrewsInfo
- Publication number
- GB145180A GB145180A GB856419A GB856419A GB145180A GB 145180 A GB145180 A GB 145180A GB 856419 A GB856419 A GB 856419A GB 856419 A GB856419 A GB 856419A GB 145180 A GB145180 A GB 145180A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- pin
- slot
- hub
- roots
- 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
- B64C11/06—Blade mountings for variable-pitch blades
- B64C11/065—Blade mountings for variable-pitch blades variable only when stationary
Abstract
145,180. Ireland, A. J. T. April 4. 1919. Screw propellers.-In screw propellers with cylindrical or cored roots adjustably engaging sockets in the boss, a multiple-part collar and uninterrupted ring are used to encircle the portions of the blade root. The blades are formed from two metal sheets welded together, and to the flanges 8 are secured the metal roots which are in two pieces and have half-cylindrical extensicns 11 with flanges 12, 13, Figs. 1, 2. The blades are kept in the bosses 14 of the propeller hub by two half-rings 15 which are encircled by the ring 16, a flange 18 holding the coned portion of the pieces 15 up against a corresponding bevel on the hub. At the inner end, a plain ring 20 is provided. For adjusting the pitch, the cap 21 carried by a pin 24 mounted in a curved slot has a projection 22 adapted to engage a slot 23 in the blade root. For ready adjustment, the pin 21 is engaged by a right-angled lug on a ring, the ring having a second pin which passes through a slot in the front face of the propeller hub. For securing the second pin, the washer of the securing-nut and the face of the hub are serrated. In a modification, the ring has teeth which engage pinions on the first pins. Further, the pins may be fixed at right-angles to the blade roots and project through the blade bosses and engage a radial slot in a disk on the propeller shaft. When wooden blades are employed, the root is coned and surrounded by a three part sleeve upon which the internally coned two part collar seats itself. Specification 132,070 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB856419A GB145180A (en) | 1919-04-04 | 1919-04-04 | Improvements in and relating to airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB856419A GB145180A (en) | 1919-04-04 | 1919-04-04 | Improvements in and relating to airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB145180A true GB145180A (en) | 1920-07-02 |
Family
ID=9854892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB856419A Expired GB145180A (en) | 1919-04-04 | 1919-04-04 | Improvements in and relating to airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB145180A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112607003A (en) * | 2020-11-25 | 2021-04-06 | 常州市长昊机械有限公司 | Easily accomodate formula aviation blade |
CN114348240A (en) * | 2020-10-14 | 2022-04-15 | 保时捷股份公司 | Ducted propeller of aircraft and aircraft |
-
1919
- 1919-04-04 GB GB856419A patent/GB145180A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114348240A (en) * | 2020-10-14 | 2022-04-15 | 保时捷股份公司 | Ducted propeller of aircraft and aircraft |
CN114348240B (en) * | 2020-10-14 | 2023-10-31 | 保时捷股份公司 | Ducted propeller of aircraft and aircraft |
CN112607003A (en) * | 2020-11-25 | 2021-04-06 | 常州市长昊机械有限公司 | Easily accomodate formula aviation blade |
CN112607003B (en) * | 2020-11-25 | 2023-06-20 | 常州市长昊机械有限公司 | Easily accomodate formula aviation blade |
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