GB239323A - Improvements in or relating to propellers for aerial vessels - Google Patents

Improvements in or relating to propellers for aerial vessels

Info

Publication number
GB239323A
GB239323A GB1709824A GB1709824A GB239323A GB 239323 A GB239323 A GB 239323A GB 1709824 A GB1709824 A GB 1709824A GB 1709824 A GB1709824 A GB 1709824A GB 239323 A GB239323 A GB 239323A
Authority
GB
United Kingdom
Prior art keywords
propellers
rotates
groove
relating
shoot
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
GB1709824A
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 GB1709824A priority Critical patent/GB239323A/en
Publication of GB239323A publication Critical patent/GB239323A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C35/00Flying-boats; Seaplanes
    • B64C35/006Flying-boats; Seaplanes with lift generating devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

239,323. Bowie, J. July 17, 1924. Screw propellers. - Screw propellers for helicopters are formed with one or more convolutions with a horizontal flange which rotates in a groove on a discharge shoot, the latter projecting through the hull and tapering toward a controlled outlet. The lifting propellers are arranged in groups of five, driven by an engine 7, Figs. 1 and 3, propellers 2, 3, 4, 5 being at the sides and at a lower level than 1 which is on the centre line. The side propellers have a bottom flange 6, Fig. 5, which rotates in a groove 7 at the top of a tapered shoot 8, the lower end of which is closed by a counter-weighted flap 9 when the helicopter alights on the water. Propellers 10, 11, 12, 13 are provided for horizontal propulsion. Air and water rudders 14, 15 are provided. The central propellers 1 are constucted as descibed in Specification 26140/10.
GB1709824A 1924-07-17 1924-07-17 Improvements in or relating to propellers for aerial vessels Expired GB239323A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1709824A GB239323A (en) 1924-07-17 1924-07-17 Improvements in or relating to propellers for aerial vessels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1709824A GB239323A (en) 1924-07-17 1924-07-17 Improvements in or relating to propellers for aerial vessels

Publications (1)

Publication Number Publication Date
GB239323A true GB239323A (en) 1925-09-10

Family

ID=10089201

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1709824A Expired GB239323A (en) 1924-07-17 1924-07-17 Improvements in or relating to propellers for aerial vessels

Country Status (1)

Country Link
GB (1) GB239323A (en)

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