GB240291A - Improvements in or relating to propellers for aircraft - Google Patents
Improvements in or relating to propellers for aircraftInfo
- Publication number
- GB240291A GB240291A GB2215624A GB2215624A GB240291A GB 240291 A GB240291 A GB 240291A GB 2215624 A GB2215624 A GB 2215624A GB 2215624 A GB2215624 A GB 2215624A GB 240291 A GB240291 A GB 240291A
- Authority
- GB
- United Kingdom
- Prior art keywords
- splines
- sleeve
- socket
- root
- hub
- 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)
- Mounting Of Bearings Or Others (AREA)
- Rolling Contact Bearings (AREA)
Abstract
240,291. Napier & Son, Ltd., D., and Wilkinson, G. S. Sept. 19, 1924. Screw propellers.-In variable pitch air screws, each blade has a metal sleeve at its root with external splines which engage internal splines in a metal socket which is rotatably mounted in the hub and has its inner end of smaller diameter than the outer end, a nut locking the sleeve and socket together. The root of the blade A has a sleeve B riveted thereto, the sleeve having external splines B<3> and an upper conical face B'. The splines engage splines D<1> on a socket D which has an external thread carrying the locking nut E, the end E<1> being drawn up on to the conical face B<2>, and at the same time the root C is held firm against the conical shoulder D<3>. The socket has ball thrust bearings M and roller journal bearings J, J<1>, in conjunction with a member F which is rigidly held in the hub G' by the collar H screwed on to the flange G<2>. Plain bearings may be substituted for the rollers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2215624A GB240291A (en) | 1924-09-19 | 1924-09-19 | Improvements in or relating to propellers for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2215624A GB240291A (en) | 1924-09-19 | 1924-09-19 | Improvements in or relating to propellers for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB240291A true GB240291A (en) | 1925-10-01 |
Family
ID=10174829
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2215624A Expired GB240291A (en) | 1924-09-19 | 1924-09-19 | Improvements in or relating to propellers for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB240291A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2523651A (en) * | 1945-09-26 | 1950-09-26 | Doussain Robert | Propelling means |
CN107985586A (en) * | 2017-12-29 | 2018-05-04 | 江苏方阔航空科技有限公司 | A kind of life-cycle pulp hub structure |
WO2022018354A1 (en) * | 2020-07-24 | 2022-01-27 | Safran Aircraft Engines | System for controlling the pitch of a propeller blade for an aircraft turbine engine |
WO2022018353A1 (en) * | 2020-07-24 | 2022-01-27 | Safran Aircraft Engines | Aircraft turbine engine comprising variable-pitch propeller blades |
FR3112820A1 (en) * | 2020-07-24 | 2022-01-28 | Safran Aircraft Engines | AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE |
FR3120660A1 (en) * | 2021-03-15 | 2022-09-16 | Safran Aircraft Engines | PROPELLER BLADE ANGULAR PITCH CONTROL SYSTEM FOR AN AIRCRAFT TURBOMACHINE |
US20220372884A1 (en) * | 2021-05-24 | 2022-11-24 | General Electric Company | Preload sleeve for a collet-mounted blade dovetail |
-
1924
- 1924-09-19 GB GB2215624A patent/GB240291A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2523651A (en) * | 1945-09-26 | 1950-09-26 | Doussain Robert | Propelling means |
CN107985586A (en) * | 2017-12-29 | 2018-05-04 | 江苏方阔航空科技有限公司 | A kind of life-cycle pulp hub structure |
WO2022018354A1 (en) * | 2020-07-24 | 2022-01-27 | Safran Aircraft Engines | System for controlling the pitch of a propeller blade for an aircraft turbine engine |
WO2022018353A1 (en) * | 2020-07-24 | 2022-01-27 | Safran Aircraft Engines | Aircraft turbine engine comprising variable-pitch propeller blades |
FR3112820A1 (en) * | 2020-07-24 | 2022-01-28 | Safran Aircraft Engines | AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE |
US12030615B2 (en) | 2020-07-24 | 2024-07-09 | Safran Aircraft Engines | System for controlling the pitch of a propeller vane for an aircraft turbine engine |
FR3120660A1 (en) * | 2021-03-15 | 2022-09-16 | Safran Aircraft Engines | PROPELLER BLADE ANGULAR PITCH CONTROL SYSTEM FOR AN AIRCRAFT TURBOMACHINE |
US20220372884A1 (en) * | 2021-05-24 | 2022-11-24 | General Electric Company | Preload sleeve for a collet-mounted blade dovetail |
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