GB462904A - Improvements in spars for the wings of aircraft - Google Patents

Improvements in spars for the wings of aircraft

Info

Publication number
GB462904A
GB462904A GB2556935A GB2556935A GB462904A GB 462904 A GB462904 A GB 462904A GB 2556935 A GB2556935 A GB 2556935A GB 2556935 A GB2556935 A GB 2556935A GB 462904 A GB462904 A GB 462904A
Authority
GB
United Kingdom
Prior art keywords
spars
shells
spar
aircraft
strips
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
GB2556935A
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 GB2556935A priority Critical patent/GB462904A/en
Publication of GB462904A publication Critical patent/GB462904A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

462,904. Aircraft wing spars. VOGT, R. Sept. 14, 1935, No. 25569. [Class 4] A conical tubular spar a, Figs. 1 and 2, tor single-spar aircraft wings consists of two approximately semicircular shells d, the abutting edges of which are overlapped by cover strips e. Shells d are of uniform thickness, but the breadth of strips e is varied along the span. In a modification, Fig. 3, shells g rolled into the sections shown from sheet metal are welded together along the neutral plane of the spar. The spars may be employed as fuel containers.
GB2556935A 1935-09-14 1935-09-14 Improvements in spars for the wings of aircraft Expired GB462904A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2556935A GB462904A (en) 1935-09-14 1935-09-14 Improvements in spars for the wings of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2556935A GB462904A (en) 1935-09-14 1935-09-14 Improvements in spars for the wings of aircraft

Publications (1)

Publication Number Publication Date
GB462904A true GB462904A (en) 1937-03-15

Family

ID=10229809

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2556935A Expired GB462904A (en) 1935-09-14 1935-09-14 Improvements in spars for the wings of aircraft

Country Status (1)

Country Link
GB (1) GB462904A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2619301A (en) * 1948-02-02 1952-11-25 Theodore P Hall Flight component for ground vehicles adapted to be airborne
US2681778A (en) * 1950-09-29 1954-06-22 Landrum L Hughes Fuel storage system for aircraft
GB2315054A (en) * 1996-07-10 1998-01-21 Christos Rugeris Wing with inflatable spars and rigid ribs
WO2009080736A1 (en) * 2007-12-21 2009-07-02 Airbus España S.L. Aircraft control surface
CN102317154B (en) * 2007-04-05 2015-09-09 波音公司 A kind of method and system of composite structural truss

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2619301A (en) * 1948-02-02 1952-11-25 Theodore P Hall Flight component for ground vehicles adapted to be airborne
US2681778A (en) * 1950-09-29 1954-06-22 Landrum L Hughes Fuel storage system for aircraft
GB2315054A (en) * 1996-07-10 1998-01-21 Christos Rugeris Wing with inflatable spars and rigid ribs
CN102317154B (en) * 2007-04-05 2015-09-09 波音公司 A kind of method and system of composite structural truss
EP2139761B1 (en) * 2007-04-05 2017-01-18 The Boeing Company Methods and systems for composite structural truss
WO2009080736A1 (en) * 2007-12-21 2009-07-02 Airbus España S.L. Aircraft control surface

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