GB325465A - Cantilever spars for aircraft - Google Patents

Cantilever spars for aircraft

Info

Publication number
GB325465A
GB325465A GB24904/29A GB2490429A GB325465A GB 325465 A GB325465 A GB 325465A GB 24904/29 A GB24904/29 A GB 24904/29A GB 2490429 A GB2490429 A GB 2490429A GB 325465 A GB325465 A GB 325465A
Authority
GB
United Kingdom
Prior art keywords
spar
aircraft
shewn
apices
struts
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
GB24904/29A
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 GB24904/29A priority Critical patent/GB325465A/en
Publication of GB325465A publication Critical patent/GB325465A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)

Abstract

325,465. Chorlton, A. E. L., Haig, R. A., de H., and Stieger, H. J. Dec. 7, 1928. Divided on 325,041. Cars and cabins; framework.-A longitudinally disposed cantilever spar for fuselages or other elongated hollow bodies on aircraft, is especially designed to take torsional stresses and comprises two booms A, B, held apart by a web C, and triangular bracings E, E<1>, F, F<1>, G, G<1>, and H, H<1>, on opposite sides of the spar. The apices of these triangles are connected together in pairs as shewn and the apices on opposite sides of the spar are stayed apart one from the other by struts D, D<1> and are also stayed in line by wires J, J<1>. The tension members may be wires as shewn, or more rigid connections such as tubes may be used. Secondary auxiliary spars and/or ribs may be arranged around the struts and spar, fabric or other covering completing a streamline outline. Specification 306,220 is referred to.
GB24904/29A 1928-12-07 1928-12-07 Cantilever spars for aircraft Expired GB325465A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB24904/29A GB325465A (en) 1928-12-07 1928-12-07 Cantilever spars for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24904/29A GB325465A (en) 1928-12-07 1928-12-07 Cantilever spars for aircraft

Publications (1)

Publication Number Publication Date
GB325465A true GB325465A (en) 1930-02-20

Family

ID=10219091

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24904/29A Expired GB325465A (en) 1928-12-07 1928-12-07 Cantilever spars for aircraft

Country Status (1)

Country Link
GB (1) GB325465A (en)

Similar Documents

Publication Publication Date Title
GB353257A (en) Improvements in gangways for loading and unloading ships
GB325465A (en) Cantilever spars for aircraft
GB329963A (en) Improvements in and relating to fronts for furnaces
GB259068A (en) Improvements in screw propellers for air-ships, aeroplanes, boats, and other vehicles
US1712812A (en) Wing for aircraft
GB393445A (en) Improvements in or relating to aircraft landing gear
US1861902A (en) Strut construction
GB127665A (en) Improvements in the Construction of Girders, Beams, Struts and the like for Air Craft and other purposes.
GB286482A (en) Improvements in or relating to skeleton structures such as aircraft fuselages
GB456632A (en) Landing gear for aeroplanes
GB264626A (en) Improvements in or relating to light metal structures
GB346244A (en) Improvements in or relating to collapsible or folding aeroplane wings
GB360170A (en) Improvements in metal spars suitable for aircraft
GB364534A (en) Improvements in aircraft
GB334405A (en) Improvements in or connected with frame structures particularly suitable in aircraft construction
GB339486A (en) Improvements in the structure of monoplanes with thick wings
GB246598A (en) Improvements in the construction of thin tubular bodies
GB431595A (en) Improvements in or relating to wing structures for aircraft
GB210591A (en) Improvements in girders and the like of box-like or similar section for use upon aircraft
GB123902A (en) Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.
GB224408A (en) Improvements in rigid air-ships
GB306220A (en) Improvements in or connected with wings for aircraft
GB418066A (en) Improvements in or connected with biplane wing structures for aircraft
GB157265A (en) Improvements relating to the construction of hollow bodies for aircraft
GB274085A (en) Improvements in sheet metal wall and like structures