GB590511A - Improvements in or relating to aircraft and other hollow bodies - Google Patents

Improvements in or relating to aircraft and other hollow bodies

Info

Publication number
GB590511A
GB590511A GB20069/44A GB2006944A GB590511A GB 590511 A GB590511 A GB 590511A GB 20069/44 A GB20069/44 A GB 20069/44A GB 2006944 A GB2006944 A GB 2006944A GB 590511 A GB590511 A GB 590511A
Authority
GB
United Kingdom
Prior art keywords
aircraft
attachments
openings
wing
side walls
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
GB20069/44A
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.)
ThyssenKrupp Budd Co
Original Assignee
Edward G Budd Manufacturing Co
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 Edward G Budd Manufacturing Co filed Critical Edward G Budd Manufacturing Co
Publication of GB590511A publication Critical patent/GB590511A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0081Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)

Abstract

590,511. Aircraft. BUDD MANUFACTURING CO., E. G. Oct. 17, 1944, No. 20069. Convention date, June 23, 1943. [Class 4] In a hollow body, such as the body 20 of an aircraft shown in Fig. 1 and particularly one with side wall openings 31 giving access to the body cargo space, members, such as the wings 19, span the openings and provide reinforcement to the side walls, which are liable on landing of the aircraft to bulge at the curved parts of the side walls as shown at f in Fig. 3. The primary wing attachments through spars 39, 40 shown in plan, Fig. 4, are constructed in the manner described in Specification 590,510, these attachments being forward of the openings 31 ; the lighter secondary attachments for the trailing wing portions span the door openings 31 to serve as external reinforcements, The wing 19, Fig. 8, with reinforced upper and lower skins 38 is connected by the reinforcing stringers 42 to the curved wall members 35, the skins 38 being connected by filler sections 47<1> to the body skin 33. The two sets of attachments are indicated by shading in Fig. 4 to show the C-shaped reinforcing member formed by them.
GB20069/44A 1943-06-23 1944-10-17 Improvements in or relating to aircraft and other hollow bodies Expired GB590511A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US590511XA 1943-06-23 1943-06-23

Publications (1)

Publication Number Publication Date
GB590511A true GB590511A (en) 1947-07-21

Family

ID=22020513

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20069/44A Expired GB590511A (en) 1943-06-23 1944-10-17 Improvements in or relating to aircraft and other hollow bodies

Country Status (1)

Country Link
GB (1) GB590511A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009003870A2 (en) * 2007-06-29 2009-01-08 Airbus Operations Gmbh Structural component with rib and cross member element
CN104015916A (en) * 2014-06-13 2014-09-03 韩世宇 Unmanned plane

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009003870A2 (en) * 2007-06-29 2009-01-08 Airbus Operations Gmbh Structural component with rib and cross member element
WO2009003870A3 (en) * 2007-06-29 2009-03-12 Airbus Gmbh Structural component with rib and cross member element
US8439307B2 (en) 2007-06-29 2013-05-14 Airbus Operations Gmbh Structural component with rib and cross member element
CN104015916A (en) * 2014-06-13 2014-09-03 韩世宇 Unmanned plane

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