GB240291A - Improvements in or relating to propellers for aircraft - Google Patents

Improvements in or relating to propellers for aircraft

Info

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
Application number
GB2215624A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB2215624A priority Critical patent/GB240291A/en
Publication of GB240291A publication Critical patent/GB240291A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02Hub construction
    • B64C11/04Blade mountings
    • B64C11/06Blade 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.
GB2215624A 1924-09-19 1924-09-19 Improvements in or relating to propellers for aircraft Expired GB240291A (en)

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 (8)

* Cited by examiner, † Cited by third party
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
WO2022018353A1 (en) * 2020-07-24 2022-01-27 Safran Aircraft Engines Aircraft turbine engine comprising variable-pitch propeller blades
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
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
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

Cited By (8)

* Cited by examiner, † Cited by third party
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
WO2022018353A1 (en) * 2020-07-24 2022-01-27 Safran Aircraft Engines Aircraft turbine engine comprising variable-pitch propeller blades
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
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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