GB462390A - Improved construction of wings, aerofoils and the like for aeronautical machines - Google Patents

Improved construction of wings, aerofoils and the like for aeronautical machines

Info

Publication number
GB462390A
GB462390A GB24138/35A GB2413835A GB462390A GB 462390 A GB462390 A GB 462390A GB 24138/35 A GB24138/35 A GB 24138/35A GB 2413835 A GB2413835 A GB 2413835A GB 462390 A GB462390 A GB 462390A
Authority
GB
United Kingdom
Prior art keywords
ribs
flats
booms
straps
secured
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
GB24138/35A
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 GB24138/35A priority Critical patent/GB462390A/en
Publication of GB462390A publication Critical patent/GB462390A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Landscapes

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

Abstract

462,390. Aircraft structures. MAYROW, J. J. Aug. 29, 1935, No. 24138. [Class 4] Aircraft structures and in particular thick wing structures comprise ribs 2 of zigzag formation, Fig. 2, assembled in such manner as to form upper and lower reticulated frames which are spaced apart by posts 4 and are directly secured to the outer covering or skin 1 of the wing or other structure. Longitudinal booms 3 are also secured to the outer covering and to the ribs at the points of inter-attachment thereof, Fig. 6. Ribs 2 are of channel section shaped at the bends to form flats 2a and to form recesses to allow passage of the booms 3. Adjacent ribs are attached to each other and to the booms at each junction by straps 5, Fig. 5, bent to the shape of the rib angle at 5a, and to that of the underside of the boom at 5b. Parts 5a of opposed straps are introduced between flats 2a of the ribs, the strap extending under the rib channel and then upwardly to connect with the boom, Fig. 6. Tubular posts 4 are secured to flats 5c, Fig. 5, of straps 5 by flanges 6, Fig. 2 ; the joints may be stiffened by additional gussets such as 7.
GB24138/35A 1935-08-29 1935-08-29 Improved construction of wings, aerofoils and the like for aeronautical machines Expired GB462390A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB24138/35A GB462390A (en) 1935-08-29 1935-08-29 Improved construction of wings, aerofoils and the like for aeronautical machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24138/35A GB462390A (en) 1935-08-29 1935-08-29 Improved construction of wings, aerofoils and the like for aeronautical machines

Publications (1)

Publication Number Publication Date
GB462390A true GB462390A (en) 1937-03-01

Family

ID=10206983

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24138/35A Expired GB462390A (en) 1935-08-29 1935-08-29 Improved construction of wings, aerofoils and the like for aeronautical machines

Country Status (1)

Country Link
GB (1) GB462390A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007020069A1 (en) * 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Support structure for a wing

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007020069A1 (en) * 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Support structure for a wing
US8205834B2 (en) 2005-08-17 2012-06-26 Airbus Deutschland Gmbh Support structure for a wing

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