GB439407A - Improvements in the manufacture of screw propellers - Google Patents

Improvements in the manufacture of screw propellers

Info

Publication number
GB439407A
GB439407A GB13788/35A GB1378835A GB439407A GB 439407 A GB439407 A GB 439407A GB 13788/35 A GB13788/35 A GB 13788/35A GB 1378835 A GB1378835 A GB 1378835A GB 439407 A GB439407 A GB 439407A
Authority
GB
United Kingdom
Prior art keywords
ribs
blade
screw
rests
blades
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
GB13788/35A
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.)
DURALUMIN SOC DU
Original Assignee
DURALUMIN SOC DU
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 DURALUMIN SOC DU filed Critical DURALUMIN SOC DU
Publication of GB439407A publication Critical patent/GB439407A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)

Abstract

439,407. Screw propellers. SOC. DU DURALUMIN, 23<bis>, Rue de Balzac, Paris. May 10, 1935, No. 13788. Convention date, May 14, 1934. [Class 114] Screw - propeller blades are constituted by a mono - block framework or skeleton with ribs extending over the whole length of the blade connected by a continuous sheet. A screw propeller blade f is formed with ribs l<1>, l<2>, united by the continuous surface forming the driving face of the blade. The rear face is completed by a metal sheet t which rests on the apices n<1>, n2, n3 and is riveted to the following edge of the blade and anchored at the front edge in a filler material o. Instead of maintaining hollow spaces between the ribs a suitable filler of material such as a resin product may be utilized and the cover t then rests upon this filler material. In an alternative form the ribs are disposed toward the leading and following edges only and the intermediate ribs are dispensed with. The ribs may in section be broader at the tips than at the roots thereof and the spaces a, b between the ribs l<1>, l<2>, l<3>, may be wider at the middle and narrow toward the tip and root of the blades.
GB13788/35A 1934-05-14 1935-05-10 Improvements in the manufacture of screw propellers Expired GB439407A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE439407X 1934-05-14

Publications (1)

Publication Number Publication Date
GB439407A true GB439407A (en) 1935-12-05

Family

ID=6507308

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13788/35A Expired GB439407A (en) 1934-05-14 1935-05-10 Improvements in the manufacture of screw propellers

Country Status (1)

Country Link
GB (1) GB439407A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE740608C (en) * 1937-04-29 1943-10-25 Rheinmetall Borsig Ag Inside stiffened propeller hollow blade
US2506992A (en) * 1945-02-26 1950-05-09 Curtiss Wright Corp Blade construction and propeller blade
US2652897A (en) * 1950-03-31 1953-09-22 Curtiss Wright Corp Propeller blade construction
GB2264755A (en) * 1992-03-04 1993-09-08 Snecma Stator blade construction

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE740608C (en) * 1937-04-29 1943-10-25 Rheinmetall Borsig Ag Inside stiffened propeller hollow blade
US2506992A (en) * 1945-02-26 1950-05-09 Curtiss Wright Corp Blade construction and propeller blade
US2652897A (en) * 1950-03-31 1953-09-22 Curtiss Wright Corp Propeller blade construction
GB2264755A (en) * 1992-03-04 1993-09-08 Snecma Stator blade construction
GB2264755B (en) * 1992-03-04 1995-05-03 Snecma Turbomachine flow-straightener blade

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