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GB232732A - Improvements in lifting and propelling devices for aircraft - Google Patents

Improvements in lifting and propelling devices for aircraft

Info

Publication number
GB232732A
GB232732A GB447624A GB447624A GB232732A GB 232732 A GB232732 A GB 232732A GB 447624 A GB447624 A GB 447624A GB 447624 A GB447624 A GB 447624A GB 232732 A GB232732 A GB 232732A
Authority
GB
United Kingdom
Prior art keywords
propeller
blades
ordinary
aircraft
lifting
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
GB447624A
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 GB447624A priority Critical patent/GB232732A/en
Publication of GB232732A publication Critical patent/GB232732A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

232,732. Short, H. O. Feb. 21, 1924. Screw propellers.-In screw propellers, the blades are wholly or partly constituted by serrated cylinders which are rotated on their own axes in addition to the rotary motion about the propeller axis. Serrated rollers 5, Fig. 1, which replace the ordinary blades of a screw propeller are radially mounted with respect to the hollow propeller shaft 1 and are rotated on their own axes from a shaft 8 through gearing 6, 7. In a modification, the roller 5, Fig. 3, is placed along the, leading edge of an ordinary blade 11. Alternatively the propeller may be made up with a number of radial rollers and a number of ordinary blades.
GB447624A 1924-02-21 1924-02-21 Improvements in lifting and propelling devices for aircraft Expired GB232732A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB447624A GB232732A (en) 1924-02-21 1924-02-21 Improvements in lifting and propelling devices for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB447624A GB232732A (en) 1924-02-21 1924-02-21 Improvements in lifting and propelling devices for aircraft

Publications (1)

Publication Number Publication Date
GB232732A true GB232732A (en) 1925-04-30

Family

ID=9777896

Family Applications (1)

Application Number Title Priority Date Filing Date
GB447624A Expired GB232732A (en) 1924-02-21 1924-02-21 Improvements in lifting and propelling devices for aircraft

Country Status (1)

Country Link
GB (1) GB232732A (en)

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