GB219477A - Improvements in screw propellers - Google Patents

Improvements in screw propellers

Info

Publication number
GB219477A
GB219477A GB1783023A GB1783023A GB219477A GB 219477 A GB219477 A GB 219477A GB 1783023 A GB1783023 A GB 1783023A GB 1783023 A GB1783023 A GB 1783023A GB 219477 A GB219477 A GB 219477A
Authority
GB
United Kingdom
Prior art keywords
plates
blade
root
riveted
faces
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
GB1783023A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1783023A priority Critical patent/GB219477A/en
Publication of GB219477A publication Critical patent/GB219477A/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

219,477. Leitner, H. July 10, 1923. Screw propellers.-Hollow metal detachable screw propeller blades are constructed from plates or tubes which are folded around one another at the butt end and decrease in width until a joint is formed along the centre of the blade. Two plates a, b, Figs. 1 and 2, are pressed to form the trailing and leading portions of the blade, the parts being riveted together at e along the middle of the faces. The plates at the root ara wide enough to be formed into complete cylinders, the cylindrical part c of the. portion a fits within the cylindrical part d on the portion b and is riveted or otherwise secured thereto. In a modification, the leading and trailing edges are straight and the blanks before pressing are formed with a V opening at the butt end, so that the root of the blade is of tapered form. Instead of plates, slightly conical tubes a, b, Fig. 8, may be used, each tube being suitably flattened to aerofoil shape and being cut away for three-quarters of the length and slightly less than half the width so that an overlapping joint at e is provided. The tubular ends are bent round and secured to a flange l on a fitting k which constitutes the cylindrical root. A longitudinal internal stiffening girder connecting the two faces may be added to the preceding constructions. In one form, the girder is constructed from strips o, p, Figs. 10, which are of channel form with abutting webs riveted at q, the flanges of the channels being enlarged and brought into curved form at the butt ends. The blade plates may be of taper gauge and/or made up of laminations.
GB1783023A 1923-07-10 1923-07-10 Improvements in screw propellers Expired GB219477A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1783023A GB219477A (en) 1923-07-10 1923-07-10 Improvements in screw propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1783023A GB219477A (en) 1923-07-10 1923-07-10 Improvements in screw propellers

Publications (1)

Publication Number Publication Date
GB219477A true GB219477A (en) 1924-07-31

Family

ID=10101943

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1783023A Expired GB219477A (en) 1923-07-10 1923-07-10 Improvements in screw propellers

Country Status (1)

Country Link
GB (1) GB219477A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450455A (en) * 1944-09-13 1948-10-05 Carl J Snyder Hollow propeller blade
US2463101A (en) * 1944-02-18 1949-03-01 Smith Corp A O Method of making airplane propellers
DE919148C (en) * 1942-07-16 1954-10-14 Messerschmitt Boelkow Blohm Hollow blade for propellers and process for their manufacture

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE919148C (en) * 1942-07-16 1954-10-14 Messerschmitt Boelkow Blohm Hollow blade for propellers and process for their manufacture
US2463101A (en) * 1944-02-18 1949-03-01 Smith Corp A O Method of making airplane propellers
US2450455A (en) * 1944-09-13 1948-10-05 Carl J Snyder Hollow propeller blade

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