GB537451A - Improvements in or relating to spinners for airscrews - Google Patents

Improvements in or relating to spinners for airscrews

Info

Publication number
GB537451A
GB537451A GB613940A GB613940A GB537451A GB 537451 A GB537451 A GB 537451A GB 613940 A GB613940 A GB 613940A GB 613940 A GB613940 A GB 613940A GB 537451 A GB537451 A GB 537451A
Authority
GB
United Kingdom
Prior art keywords
key
airscrews
spinners
hub
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
Application number
GB613940A
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.)
CONSTANT SPEED AIRSCREWS Ltd
Original Assignee
CONSTANT SPEED AIRSCREWS 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 CONSTANT SPEED AIRSCREWS Ltd filed Critical CONSTANT SPEED AIRSCREWS Ltd
Priority to GB613940A priority Critical patent/GB537451A/en
Publication of GB537451A publication Critical patent/GB537451A/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
    • B64C11/14Spinners

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Centrifugal Separators (AREA)
  • Testing Of Balance (AREA)

Abstract

537,451. Airscrew spinners. CONSTANT SPEED AIRSCREWS, Ltd., and MARSHALL, F. G. April 5, 1940, No. 6139. [Class 114] The spinner shell a is supported at the front and/or rear of the hub by spoked members d, e, radiating from the hub k and terminating in pin and socket connections f between which rubber bushes may be interposed. The spinner shell may be detachably secured by pin and key-hole connections and for this purpose a locking-ring s may be employed which may be moved in and out of its operative position by a key w. A spring u securing the locking ring in operative positions is thrust aside by the insertion of the key. Specifications 451,553 and 485,903 are referred to.
GB613940A 1940-04-05 1940-04-05 Improvements in or relating to spinners for airscrews Expired GB537451A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB613940A GB537451A (en) 1940-04-05 1940-04-05 Improvements in or relating to spinners for airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB613940A GB537451A (en) 1940-04-05 1940-04-05 Improvements in or relating to spinners for airscrews

Publications (1)

Publication Number Publication Date
GB537451A true GB537451A (en) 1941-06-23

Family

ID=9809133

Family Applications (1)

Application Number Title Priority Date Filing Date
GB613940A Expired GB537451A (en) 1940-04-05 1940-04-05 Improvements in or relating to spinners for airscrews

Country Status (1)

Country Link
GB (1) GB537451A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8529204B2 (en) 2008-02-26 2013-09-10 Rolls-Royce Plc Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8529204B2 (en) 2008-02-26 2013-09-10 Rolls-Royce Plc Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction

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