GB642126A - Improvements in aeroplane and like propellers - Google Patents

Improvements in aeroplane and like propellers

Info

Publication number
GB642126A
GB642126A GB16357/47A GB1635747A GB642126A GB 642126 A GB642126 A GB 642126A GB 16357/47 A GB16357/47 A GB 16357/47A GB 1635747 A GB1635747 A GB 1635747A GB 642126 A GB642126 A GB 642126A
Authority
GB
United Kingdom
Prior art keywords
blades
aeroplane
secured
plates
propellers
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
GB16357/47A
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
Publication of GB642126A publication Critical patent/GB642126A/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
    • B64C11/005Spiral-shaped propellers

Landscapes

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

Abstract

642,126. Screw propellers. ALEXANDRE, M. June 20,1947, No. 16357. Convention date, July 26, 1946. [Class 114] In an aeroplane or like propeller comprising a plurality of helical blades 1 secured at one end to a hub, narrow helical plates 5 are supported at their ends by two consecutive blades 1, each plate 5 starting from one side of one blade 1 and extending in a curve to the opposite side of the next blade 1. The plates 5 are secured to the ends of cylindrical cross-pieces 3 in the middle of which are bearings 4 which support the tips of the blades 1.
GB16357/47A 1946-07-26 1947-06-20 Improvements in aeroplane and like propellers Expired GB642126A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BR642126X 1946-07-26

Publications (1)

Publication Number Publication Date
GB642126A true GB642126A (en) 1950-08-30

Family

ID=3966377

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16357/47A Expired GB642126A (en) 1946-07-26 1947-06-20 Improvements in aeroplane and like propellers

Country Status (1)

Country Link
GB (1) GB642126A (en)

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