GB578570A - Improvements in or relating to variable-pitch propellers - Google Patents
Improvements in or relating to variable-pitch propellersInfo
- Publication number
- GB578570A GB578570A GB1124744A GB1124744A GB578570A GB 578570 A GB578570 A GB 578570A GB 1124744 A GB1124744 A GB 1124744A GB 1124744 A GB1124744 A GB 1124744A GB 578570 A GB578570 A GB 578570A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pitch
- variable
- propellers
- attached
- pin
- 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
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Support Of The Bearing (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
578,570. Variable - pitch propellers. NEWPORT, H., GODDEN, T. E., and MORRIS, E. H. June 12, 1944, No. 11247. [Class 114] In counter rotating coaxial variable-pitch propellers, the link connecting the pitchvarying mechanisms of the two propellers is formed with universally-jointed ends. The pitch-varying rod 13 of the forward propeller is attached to the inner race 17 of a thrust bearing slidable axially on the shaft 10. The outer race 20 is linked to the crank-pin 23 of the pitch-varying gear of the second propeller by a rod 29, 30 having spherical ends 27, 28 and provided with a length adjustment nut 33. This nut slides in a tube 35 mounted on a rubber bush in the hub casing 15. To overcome the oblique thrust of the link 29, 30, a pin 41 (Fig. 5), is rigidly attached to the hub casing 15 and passes through a rubber bushed fork 40 attached to the outer race of the bearing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1124744A GB578570A (en) | 1944-06-12 | 1944-06-12 | Improvements in or relating to variable-pitch propellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1124744A GB578570A (en) | 1944-06-12 | 1944-06-12 | Improvements in or relating to variable-pitch propellers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB578570A true GB578570A (en) | 1946-07-03 |
Family
ID=9982707
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1124744A Expired GB578570A (en) | 1944-06-12 | 1944-06-12 | Improvements in or relating to variable-pitch propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB578570A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4132503A (en) * | 1976-03-27 | 1979-01-02 | Schaffran Propeller Lehne & Co. | Variable-pitch propeller |
FR3055001A1 (en) * | 2016-08-10 | 2018-02-16 | Safran Aircraft Engines | PASTE CHANGE SYSTEM EQUIPPED WITH MEANS FOR ADJUSTING THE STEP OF THE BLADES AND CORRESPONDING TURBOMACHINE |
-
1944
- 1944-06-12 GB GB1124744A patent/GB578570A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4132503A (en) * | 1976-03-27 | 1979-01-02 | Schaffran Propeller Lehne & Co. | Variable-pitch propeller |
FR3055001A1 (en) * | 2016-08-10 | 2018-02-16 | Safran Aircraft Engines | PASTE CHANGE SYSTEM EQUIPPED WITH MEANS FOR ADJUSTING THE STEP OF THE BLADES AND CORRESPONDING TURBOMACHINE |
GB2554986A (en) * | 2016-08-10 | 2018-04-18 | Safran Aircraft Engines | Pitch-change system equipped with means for adjusting blade pitch and corresponding turbine engine |
US10766603B2 (en) | 2016-08-10 | 2020-09-08 | Safran Aircraft Engines | Pitch-change system equipped with means for adjusting blade pitch and corresponding turbine engine |
GB2554986B (en) * | 2016-08-10 | 2021-04-07 | Safran Aircraft Engines | Pitch-change system equipped with means for adjusting blade pitch and corresponding turbine engine |
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