GB175111A - Improvements in sheet metal girders, struts or other members - Google Patents

Improvements in sheet metal girders, struts or other members

Info

Publication number
GB175111A
GB175111A GB33273/20A GB3327320A GB175111A GB 175111 A GB175111 A GB 175111A GB 33273/20 A GB33273/20 A GB 33273/20A GB 3327320 A GB3327320 A GB 3327320A GB 175111 A GB175111 A GB 175111A
Authority
GB
United Kingdom
Prior art keywords
members
sheet
sheet metal
struts
metal
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
GB33273/20A
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 GB33273/20A priority Critical patent/GB175111A/en
Publication of GB175111A publication Critical patent/GB175111A/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
    • B64C1/064—Stringers; Longerons
    • 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

175,111. Wylie, H. N. Nov. 25, 1920. Frame components, applying and combining; sheet-metal frames.-A girder, strut, or other member, applicable to motor vehicles and the like, is composed of thin sheet-metal members, such as A, B, connected longitudinally near their edges, each member being bent in longitudinal oppositely-directed curves, which meet at an angle to each other or run into each other by other curves of small radius. This angular junction, as shown at E and C, or the small radius connection, as shown at D, is stated to resist crinkling. The structure may be further strengthened by transverse stiffening-frames, such as G, and, where these are riveted together, a longitudinal groove may be formed in the sheet metal to prevent crinkling near the rivets.
GB33273/20A 1920-11-25 1920-11-25 Improvements in sheet metal girders, struts or other members Expired GB175111A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33273/20A GB175111A (en) 1920-11-25 1920-11-25 Improvements in sheet metal girders, struts or other members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33273/20A GB175111A (en) 1920-11-25 1920-11-25 Improvements in sheet metal girders, struts or other members

Publications (1)

Publication Number Publication Date
GB175111A true GB175111A (en) 1922-02-16

Family

ID=10350777

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33273/20A Expired GB175111A (en) 1920-11-25 1920-11-25 Improvements in sheet metal girders, struts or other members

Country Status (1)

Country Link
GB (1) GB175111A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3735547A (en) * 1970-09-21 1973-05-29 Unarco Industries Hollow beam
EP0004346A1 (en) * 1978-03-27 1979-10-03 Eugene W. Sivachenko Box beam for use as a load carrying member and structures incorporating such box beams
US4769968A (en) * 1987-03-05 1988-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Truss-core corrugation for compressive loads

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3735547A (en) * 1970-09-21 1973-05-29 Unarco Industries Hollow beam
EP0004346A1 (en) * 1978-03-27 1979-10-03 Eugene W. Sivachenko Box beam for use as a load carrying member and structures incorporating such box beams
US4769968A (en) * 1987-03-05 1988-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Truss-core corrugation for compressive loads

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