GB637238A - Improvements in or relating to variable-pitch propellers - Google Patents
Improvements in or relating to variable-pitch propellersInfo
- Publication number
- GB637238A GB637238A GB181447A GB181447A GB637238A GB 637238 A GB637238 A GB 637238A GB 181447 A GB181447 A GB 181447A GB 181447 A GB181447 A GB 181447A GB 637238 A GB637238 A GB 637238A
- Authority
- GB
- United Kingdom
- Prior art keywords
- race
- variable
- blade root
- bearing
- flange
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
637,238. Variable-pitch propellers. ROTOL, Ltd., and DANVERS, E. Jan. 20, 1947, 1814. [Class 114] In a variable-pitch propeller 5 wherein each blade 6 is mounted for pitch-change movements on an anti-friction bearing 10 clamped to the blade root 18 between a shoulder 19 thereon and the flange 12 of a member 13 secured to the blade root, a race 9 of the bearing 10 is screwed directly into the hub boss 7 of the propeller and held stationary therein. The member 13 may be screwed into the blade root 18 and the flange 12 arranged to engage directly the lower race 11 of a two row tapered roller bearing 10. Relative rotation between the lower race 11 and the flange 12 and the blade root 18 may be prevented by means of tooth fastenings 14 and 22 respectively and blade movement achieved by oscillating a pin 27 secured to the lower race 11 and actuated as by a hydraulic piston and connecting rod 25. The central race 9 of the bearing may be locked in the hub boss by a tooth fastening 30, 31.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB181447A GB637238A (en) | 1947-01-20 | 1947-01-20 | Improvements in or relating to variable-pitch propellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB181447A GB637238A (en) | 1947-01-20 | 1947-01-20 | Improvements in or relating to variable-pitch propellers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB637238A true GB637238A (en) | 1950-05-17 |
Family
ID=9728492
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB181447A Expired GB637238A (en) | 1947-01-20 | 1947-01-20 | Improvements in or relating to variable-pitch propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB637238A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3040817A (en) * | 1957-04-15 | 1962-06-26 | Rotol Ltd | Variable pitch propellers |
US4540341A (en) * | 1983-01-17 | 1985-09-10 | Escher Wyss Gmbh | Adjustable propeller for marine vessel drive |
US4630999A (en) * | 1983-10-14 | 1986-12-23 | James Howden & Company Limited | Axial fan |
US4844696A (en) * | 1987-04-10 | 1989-07-04 | Novenco A/S | Blade angle control device for use in an axial flow fan the blades of which are adjustable during operation |
GB2226604A (en) * | 1988-11-24 | 1990-07-04 | Mtu Muenchen Gmbh | Blade-base attachment for a fibre rotor blade |
US5015150A (en) * | 1988-05-31 | 1991-05-14 | Mtu Munchen Gmbh | Arrangement for mounting a pivotable propfan blade |
GB2244525A (en) * | 1990-04-04 | 1991-12-04 | Dowty Aerospace Gloucester | Propeller blade hub assembly |
US5263898A (en) * | 1988-12-14 | 1993-11-23 | General Electric Company | Propeller blade retention system |
GB2409708A (en) * | 2003-11-21 | 2005-07-06 | Roulements Soc Nouvelle | Mounting a blade with a variable angle of attack |
-
1947
- 1947-01-20 GB GB181447A patent/GB637238A/en not_active Expired
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3040817A (en) * | 1957-04-15 | 1962-06-26 | Rotol Ltd | Variable pitch propellers |
US4540341A (en) * | 1983-01-17 | 1985-09-10 | Escher Wyss Gmbh | Adjustable propeller for marine vessel drive |
US4630999A (en) * | 1983-10-14 | 1986-12-23 | James Howden & Company Limited | Axial fan |
AU566957B2 (en) * | 1983-10-14 | 1987-11-05 | James Howden & Co. Ltd. | Variable pitch fan blade mounting |
US4844696A (en) * | 1987-04-10 | 1989-07-04 | Novenco A/S | Blade angle control device for use in an axial flow fan the blades of which are adjustable during operation |
US5015150A (en) * | 1988-05-31 | 1991-05-14 | Mtu Munchen Gmbh | Arrangement for mounting a pivotable propfan blade |
GB2226604A (en) * | 1988-11-24 | 1990-07-04 | Mtu Muenchen Gmbh | Blade-base attachment for a fibre rotor blade |
GB2226604B (en) * | 1988-11-24 | 1992-10-21 | Mtu Muenchen Gmbh | The combination of a blade-base attachment and a rotor blade. |
US5263898A (en) * | 1988-12-14 | 1993-11-23 | General Electric Company | Propeller blade retention system |
GB2244525A (en) * | 1990-04-04 | 1991-12-04 | Dowty Aerospace Gloucester | Propeller blade hub assembly |
GB2244525B (en) * | 1990-04-04 | 1994-09-21 | Dowty Aerospace Gloucester | A propeller hub assembly |
GB2409708A (en) * | 2003-11-21 | 2005-07-06 | Roulements Soc Nouvelle | Mounting a blade with a variable angle of attack |
GB2409708B (en) * | 2003-11-21 | 2008-06-11 | Roulements Soc Nouvelle | Device for mounting a blade with a variable angle of attack |
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