GB557120A - Improvements in or relating to spinners and the like for the hubs of airscrews - Google Patents

Improvements in or relating to spinners and the like for the hubs of airscrews

Info

Publication number
GB557120A
GB557120A GB906742A GB906742A GB557120A GB 557120 A GB557120 A GB 557120A GB 906742 A GB906742 A GB 906742A GB 906742 A GB906742 A GB 906742A GB 557120 A GB557120 A GB 557120A
Authority
GB
United Kingdom
Prior art keywords
spinner
hub
ribs
plate
grooves
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
GB906742A
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 GB906742A priority Critical patent/GB557120A/en
Publication of GB557120A publication Critical patent/GB557120A/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)
  • Harvester Elements (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Clamps And Clips (AREA)

Abstract

557,120. Airscrew spinners. CONSTANT SPEED AIRSCREWS, Ltd., MARSHALL, F. G., PAUL, P., and BURTON, P. July 1, 1942, No. 9067. [Class 114] A spinner is secured to the front and/or rear of the hub of an airscrew by fastening devices which automatically move into and out of their locking position when the spinner is moved axially onto and off the hub. In the form shown in Fig. 1, the spinner 5 carries a number of spring-pressed pivoted catches 2 to co-operate with openings 9 in the back plate 8 of the hub, the catches being connected by rods or cables 11 with a spring-pressed nose-cap 12 for releasing purposes. In the form shown in Fig. 2, the free edge 21 of an annular plate 22 on the spinner 5 has one or more annular ribs or grooves 23 to snap into one or more similar grooves or ribs 24 in the free edge 25 of a flanged plate 26 on the hub. The flange of plate 26 is slit axially to form tongues 29 which carry weights 28 for holding the ribs and grooves in engagement by centrifugal force. The spinner may be angularly located and driven by means of pins and sockets 17, 19, Fig. 1, or 30, 31, Fig. 2.
GB906742A 1942-07-01 1942-07-01 Improvements in or relating to spinners and the like for the hubs of airscrews Expired GB557120A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB906742A GB557120A (en) 1942-07-01 1942-07-01 Improvements in or relating to spinners and the like for the hubs of airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB906742A GB557120A (en) 1942-07-01 1942-07-01 Improvements in or relating to spinners and the like for the hubs of airscrews

Publications (1)

Publication Number Publication Date
GB557120A true GB557120A (en) 1943-11-04

Family

ID=9864751

Family Applications (1)

Application Number Title Priority Date Filing Date
GB906742A Expired GB557120A (en) 1942-07-01 1942-07-01 Improvements in or relating to spinners and the like for the hubs of airscrews

Country Status (1)

Country Link
GB (1) GB557120A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4863354A (en) * 1987-10-07 1989-09-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Nose cowl for a turbojet engine shaft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4863354A (en) * 1987-10-07 1989-09-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Nose cowl for a turbojet engine shaft

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