GB226301A - Improvements in airscrews - Google Patents

Improvements in airscrews

Info

Publication number
GB226301A
GB226301A GB2447523A GB2447523A GB226301A GB 226301 A GB226301 A GB 226301A GB 2447523 A GB2447523 A GB 2447523A GB 2447523 A GB2447523 A GB 2447523A GB 226301 A GB226301 A GB 226301A
Authority
GB
United Kingdom
Prior art keywords
tube
foundation
riveted
flange
boss
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
GB2447523A
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 GB2447523A priority Critical patent/GB226301A/en
Publication of GB226301A publication Critical patent/GB226301A/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
    • B64C11/20Constructional features
    • B64C11/24Hollow blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Foundations (AREA)
  • Wind Motors (AREA)
  • Connection Of Plates (AREA)

Abstract

226,301. Leitner, H. Oct. 2, 1923. Screw propellers.-Screw propeller blades are formed with an internal foundation of high tensile material such as a steel tube around which a light metallic material is cast to form the exterior surface.. A tube a, of uniform or taper gauge, is flattened at the tip c, and carries transverse tubes d with closed ends which act as keys for the outer skin b, which is cast or moulded about the foundation. In place of the tubes d, a series of projecting studs may be riveted to the main tube. At the butt end of the tube rings f and g are formed, the part between forming a journal for fitting to the boss. One flange cnly may be used, the skin being formed with a similar flange adjacent thereto. Alternatively the butt end may have an internal thread into which a plug having a flange is screwed. The tube may extend across the boss to form a common foundation for two blades. When a box foundation is used, the plates l, Fig. 6, are riveted across the lugs m, which are staggered to form keys. Corrugated plates n, Fig. 7, riveted together as at o may be used. The girder may be made up with two semi-cylindrical members p, Fig. 8, with splayed lips which are secured by a ring q and rod r. When casting the outer surface, a core is used extending to the position s. Specification 165,548 is referred to.
GB2447523A 1923-10-02 1923-10-02 Improvements in airscrews Expired GB226301A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2447523A GB226301A (en) 1923-10-02 1923-10-02 Improvements in airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2447523A GB226301A (en) 1923-10-02 1923-10-02 Improvements in airscrews

Publications (1)

Publication Number Publication Date
GB226301A true GB226301A (en) 1924-12-24

Family

ID=10212269

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2447523A Expired GB226301A (en) 1923-10-02 1923-10-02 Improvements in airscrews

Country Status (1)

Country Link
GB (1) GB226301A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511862A (en) * 1950-06-20 Propeller
US2511858A (en) * 1943-04-23 1950-06-20 United Aircraft Corp Method of making propeller blades
US4305699A (en) * 1979-02-15 1981-12-15 Centro Ricerche Fiat S.P.A. Blade for a wind motor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511862A (en) * 1950-06-20 Propeller
US2511858A (en) * 1943-04-23 1950-06-20 United Aircraft Corp Method of making propeller blades
US4305699A (en) * 1979-02-15 1981-12-15 Centro Ricerche Fiat S.P.A. Blade for a wind motor

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