GB320365A - Improvements in or relating to hollow metal air-screw propeller blades - Google Patents

Improvements in or relating to hollow metal air-screw propeller blades

Info

Publication number
GB320365A
GB320365A GB1342828A GB1342828A GB320365A GB 320365 A GB320365 A GB 320365A GB 1342828 A GB1342828 A GB 1342828A GB 1342828 A GB1342828 A GB 1342828A GB 320365 A GB320365 A GB 320365A
Authority
GB
United Kingdom
Prior art keywords
diaphragms
flanges
blade
relating
spar
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
GB1342828A
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.)
Vickers Ltd
Original Assignee
Vickers 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 Vickers Ltd filed Critical Vickers Ltd
Priority to GB1342828A priority Critical patent/GB320365A/en
Publication of GB320365A publication Critical patent/GB320365A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/78—Making other particular articles propeller blades; turbine blades

Abstract

320,365. Vickers, Ltd., and Pierson, R. K. May 7, 1928. Screw propellers.- Hollow airscrews formed with a central spar or rod carrying transverse diaphragms to which the thin sheet covering is secured are constructed with flanges on the diaphragms for securing them to the central spar and the blade sheets. The diaphragms may be conical. The central spar A, Fig. 1, tapers from root to tip and the diaphragms B have internal flanges B' pinned to the spar and external flanges B<3> to which the sheets F are secured, the outer sheet D being continued over to form the top and the leading edge C, Fig. 2, also being continued over to line up with the front and back plate sections. One face of the blade may be constituted by a single plate. Instead of the diaphragm flanges being parallel to the length of the blade they may be transversely disposed.
GB1342828A 1928-05-07 1928-05-07 Improvements in or relating to hollow metal air-screw propeller blades Expired GB320365A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1342828A GB320365A (en) 1928-05-07 1928-05-07 Improvements in or relating to hollow metal air-screw propeller blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1342828A GB320365A (en) 1928-05-07 1928-05-07 Improvements in or relating to hollow metal air-screw propeller blades

Publications (1)

Publication Number Publication Date
GB320365A true GB320365A (en) 1929-10-07

Family

ID=10022783

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1342828A Expired GB320365A (en) 1928-05-07 1928-05-07 Improvements in or relating to hollow metal air-screw propeller blades

Country Status (1)

Country Link
GB (1) GB320365A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3096826A (en) * 1961-08-07 1963-07-09 Hughes Tool Co Rotor blade for rotary-winged aircraft
US3400904A (en) * 1966-12-19 1968-09-10 James R. Bede Airfoil construction

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3096826A (en) * 1961-08-07 1963-07-09 Hughes Tool Co Rotor blade for rotary-winged aircraft
US3400904A (en) * 1966-12-19 1968-09-10 James R. Bede Airfoil construction

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