GB128663A - Improvements in Metal Construction for Aircraft. - Google Patents

Improvements in Metal Construction for Aircraft.

Info

Publication number
GB128663A
GB128663A GB12406/17A GB1240617A GB128663A GB 128663 A GB128663 A GB 128663A GB 12406/17 A GB12406/17 A GB 12406/17A GB 1240617 A GB1240617 A GB 1240617A GB 128663 A GB128663 A GB 128663A
Authority
GB
United Kingdom
Prior art keywords
members
webs
secured
shows
flanges
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
GB12406/17A
Inventor
Edward Eugene Brown
Dermot Joseph Mooney
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 GB12406/17A priority Critical patent/GB128663A/en
Priority to GB20897/18A priority patent/GB128846A/en
Publication of GB128663A publication Critical patent/GB128663A/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
    • 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
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

128,663. Brown, E. E., and Mooney, D. J. Aug. 29, 1917. Framework.-Struts, spars, girders, &c. for aircraft wings, fuselages, &c. are made of thin steel or aluminium alloy and comprise members composed of webs b and triangular flanges a bent and secured as shown in Figs. 1 to 4, the members being used singly or combined together in pairs. The webs may be ribbed and perforated as shown in Fig. 5, which also shows two members similar to Fig. 1 secured back to back. Two members may be spaced apart by continuous upper and lower plates overlapping the flanges; or discontinuous plates may be used integral with vertical pieces extending between the webs. Cross-ribs may be secured to the members by saddle-pieces. Fig. 9 shows a modified member having vertical ribs n stamped in the web, either the rib n or the flange a being cut away where they meet. Specifications 126,391 and 126,674 are referred to.
GB12406/17A 1917-08-29 1917-08-29 Improvements in Metal Construction for Aircraft. Expired GB128663A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB12406/17A GB128663A (en) 1917-08-29 1917-08-29 Improvements in Metal Construction for Aircraft.
GB20897/18A GB128846A (en) 1917-08-29 1918-12-14 Improvements in Metal Construction for Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12406/17A GB128663A (en) 1917-08-29 1917-08-29 Improvements in Metal Construction for Aircraft.

Publications (1)

Publication Number Publication Date
GB128663A true GB128663A (en) 1919-07-03

Family

ID=32345477

Family Applications (2)

Application Number Title Priority Date Filing Date
GB12406/17A Expired GB128663A (en) 1917-08-29 1917-08-29 Improvements in Metal Construction for Aircraft.
GB20897/18A Expired GB128846A (en) 1917-08-29 1918-12-14 Improvements in Metal Construction for Aircraft.

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB20897/18A Expired GB128846A (en) 1917-08-29 1918-12-14 Improvements in Metal Construction for Aircraft.

Country Status (1)

Country Link
GB (2) GB128663A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452163A (en) * 1944-11-01 1948-10-26 Standard Railway Equipment Mfg Drop endgate for railway cars
US6131362A (en) * 1998-02-04 2000-10-17 Buecker Machine & Iron Works, Inc. Sheet metal beam

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452163A (en) * 1944-11-01 1948-10-26 Standard Railway Equipment Mfg Drop endgate for railway cars
US6131362A (en) * 1998-02-04 2000-10-17 Buecker Machine & Iron Works, Inc. Sheet metal beam

Also Published As

Publication number Publication date
GB128846A (en) 1919-07-03

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