GB551140A - Improvements in or relating to airscrews - Google Patents

Improvements in or relating to airscrews

Info

Publication number
GB551140A
GB551140A GB1593441A GB1593441A GB551140A GB 551140 A GB551140 A GB 551140A GB 1593441 A GB1593441 A GB 1593441A GB 1593441 A GB1593441 A GB 1593441A GB 551140 A GB551140 A GB 551140A
Authority
GB
United Kingdom
Prior art keywords
blade
root
resin
tip
gap
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
GB1593441A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB1593441A priority Critical patent/GB551140A/en
Publication of GB551140A publication Critical patent/GB551140A/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
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/24Hollow blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

551,140. Propeller blades. FAIREY AVIATION CO., Ltd., and FORSYTH, A. G. Dec. 10, 1941, No. 15934. [Class 114] [Also in Group XXII] A propeller blade is made from a sheet metal blank a Fig. 1, having such profile that when the marginal positions are retroversed along the lines b, the marginal portions meet at the tip and root so that they may be welded together at c, Fig. 3, leaving a gap d, Figs. 3 and 5, extending over the greater part of the length and breadth of the blade. The root. which is of hollow circular section may be externally threaded or flanged to withstand the centrifugal force on the blade, and the hollow blade is then filled with a mouldable material such as a synthetic resin. The resin &c. may be reinforced by a backbone g, Fig. 10, of moulded plastic material anchored to the root of the blade and to reduce the weight of resin tubes of circular or semi-circular section may be embedded therein. The edges of the gap may be serrated or otherwise formed to key into the moulded material. The blank a preferably tapers in thickness from the root to the tip.
GB1593441A 1941-12-10 1941-12-10 Improvements in or relating to airscrews Expired GB551140A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1593441A GB551140A (en) 1941-12-10 1941-12-10 Improvements in or relating to airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1593441A GB551140A (en) 1941-12-10 1941-12-10 Improvements in or relating to airscrews

Publications (1)

Publication Number Publication Date
GB551140A true GB551140A (en) 1943-02-09

Family

ID=10068169

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1593441A Expired GB551140A (en) 1941-12-10 1941-12-10 Improvements in or relating to airscrews

Country Status (1)

Country Link
GB (1) GB551140A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428970A (en) * 1943-06-16 1947-10-14 Marquette Metal Products Co Propeller blade
US2566701A (en) * 1946-10-23 1951-09-04 Curtiss Wright Corp Reinforcement for filled hollow steel blades

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428970A (en) * 1943-06-16 1947-10-14 Marquette Metal Products Co Propeller blade
US2566701A (en) * 1946-10-23 1951-09-04 Curtiss Wright Corp Reinforcement for filled hollow steel blades

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