GB507408A - Improvements in or relating to screw propellers - Google Patents

Improvements in or relating to screw propellers

Info

Publication number
GB507408A
GB507408A GB24818/37A GB2481837A GB507408A GB 507408 A GB507408 A GB 507408A GB 24818/37 A GB24818/37 A GB 24818/37A GB 2481837 A GB2481837 A GB 2481837A GB 507408 A GB507408 A GB 507408A
Authority
GB
United Kingdom
Prior art keywords
rotation
pitch
plane
respect
blade
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
GB24818/37A
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 GB507408A publication Critical patent/GB507408A/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

Landscapes

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

Abstract

507,408. Screw propellers. FRASER, K. G. Sept. 11, 1937, No. 24818. Convention date. Sept. 15, 1936. [Class 114] The blades of a variable pitch screw propeller, on.which the aerodynamic and centrifugal moments co-operate to vary the pitch, have a distribution of the mass with respect to the plane of rotation ,and pivot axis is such that the centrifugal moments operate in a sense tending to increase the pitch for small values of V/n.d and in a sense tending to decrease the pitch for large values of V/n.d. The gravity axis of the blade is substantially co-incident with the pivot axis thereof but is gradually offset in a substantially straight line toward the tip so as to be lagging with respect to the pivot axis in the direction of rotation and leading with respect to the plane of rotation in the direction of travel. The blades 10 are rotatably mounted in their boss upon an axis PP and the central gravitios of the sections are disposed along a line GG having the disposition referred to above. To provide a further'balance of the moments acting upon the blade there may be disposed at the blade root weights 11 clamped thereto by bolts 13. For the purpose of setting, the blade root and the weight are given suitable markings 43. The boss driven from the shaft by a flexible means which permits a slight movement in and out of the plane of rotation as well as tangentially therein.
GB24818/37A 1936-09-15 1937-09-11 Improvements in or relating to screw propellers Expired GB507408A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US507408XA 1936-09-15 1936-09-15

Publications (1)

Publication Number Publication Date
GB507408A true GB507408A (en) 1939-06-12

Family

ID=21967120

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24818/37A Expired GB507408A (en) 1936-09-15 1937-09-11 Improvements in or relating to screw propellers

Country Status (1)

Country Link
GB (1) GB507408A (en)

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