GB448249A - Improvements relating to internally trussed structures which are capable of flexing longitudinally - Google Patents

Improvements relating to internally trussed structures which are capable of flexing longitudinally

Info

Publication number
GB448249A
GB448249A GB34816/34A GB3481634A GB448249A GB 448249 A GB448249 A GB 448249A GB 34816/34 A GB34816/34 A GB 34816/34A GB 3481634 A GB3481634 A GB 3481634A GB 448249 A GB448249 A GB 448249A
Authority
GB
United Kingdom
Prior art keywords
worm
wing
panels
section
rib
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
GB34816/34A
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.)
CHARLES HAMPSON GRANT
Original Assignee
CHARLES HAMPSON GRANT
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 CHARLES HAMPSON GRANT filed Critical CHARLES HAMPSON GRANT
Publication of GB448249A publication Critical patent/GB448249A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/48Varying camber by relatively-movable parts of wing structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

448,249. Aeroplane wings. GRANT, C. H., 51, Prospect Street, New Rochelle, New York, U.S.A. Dec. 4, 1934, No. 34816. Convention date, Dec. 9, 1933. [Class 4] A trussed structure particularly for an aeroplane wing comprises a series of interconnected panels and links, the panels being pivotally connected for rotation and adjacent links being pivoted together and pivotally engaged by adjacent panels to guide the motion of the panels in unified flexure of the truss. The wing spars 1, 2 are fixed relatively to one another by channels 21, 22 which carry a wormwheel 33 mounted in a casing 26 slidable in guides 28 on the channels. The worm-wheel 33 is driven by a worm 34 connected by a flexible coupling 36 to a shaft 35 operated by a worm gear from a shaft 40. A screw-strut 31 passes through the worm-wheel 33 and is raised or lowered to alter the camber of the wing when the worm-wheel is rotated. The wing ribs are jointed and comprise a front section 3, Fig. 3, rotatably mounted on the front spar 1 and a rear section 5 slidably mounted on the roar spar 2. Triangular sections are mounted between the spars, the bases being pivoted at 9 to the upper portion of the rib and their lower ends being slidable in slots 11 in the lower portion of the rib. The apex of each section is slotted at 16 to accommodate the pivot points of diagonal braces 14 and each end triangular section is anchored to the front and rear section of the rib by links 17. The covering 29 of the undersurface of the wing is provided with overlapping portions 30 to enable the surface to expand and contract.
GB34816/34A 1933-12-09 1934-12-04 Improvements relating to internally trussed structures which are capable of flexing longitudinally Expired GB448249A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US448249XA 1933-12-09 1933-12-09

Publications (1)

Publication Number Publication Date
GB448249A true GB448249A (en) 1936-06-04

Family

ID=21934536

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34816/34A Expired GB448249A (en) 1933-12-09 1934-12-04 Improvements relating to internally trussed structures which are capable of flexing longitudinally

Country Status (1)

Country Link
GB (1) GB448249A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2208635A (en) * 1987-07-08 1989-04-12 Robert Irwin Hill Variable lift wing
GB2386884A (en) * 2002-03-28 2003-10-01 Richard Linsley-Hood Aerofoil with variable camber
EP1674389A1 (en) * 2004-12-22 2006-06-28 Airbus Deutschland GmbH (HRB 43527) Structure, in particular spar box, for forming aerodynamically active surfaces of air vehicles
US7517198B2 (en) 2006-03-20 2009-04-14 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US8475133B2 (en) 2008-12-05 2013-07-02 Modular Wind Energy, Inc. Efficient wind turbine blades, wind turbine blade structures, and associated systems and methods of manufacture, assembly and use
US9500179B2 (en) 2010-05-24 2016-11-22 Vestas Wind Systems A/S Segmented wind turbine blades with truss connection regions, and associated systems and methods

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2208635A (en) * 1987-07-08 1989-04-12 Robert Irwin Hill Variable lift wing
GB2386884A (en) * 2002-03-28 2003-10-01 Richard Linsley-Hood Aerofoil with variable camber
GB2386884B (en) * 2002-03-28 2005-09-14 Richard Linsley-Hood Aerofoil with variable camber
US7909292B2 (en) 2004-12-22 2011-03-22 Airbus Deutschland Gmbh Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane
US7607617B2 (en) 2004-12-22 2009-10-27 Airbus Deutschland Gmbh Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane
EP1674389A1 (en) * 2004-12-22 2006-06-28 Airbus Deutschland GmbH (HRB 43527) Structure, in particular spar box, for forming aerodynamically active surfaces of air vehicles
US7517198B2 (en) 2006-03-20 2009-04-14 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US7891950B2 (en) 2006-03-20 2011-02-22 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US7891948B2 (en) 2006-03-20 2011-02-22 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US7891949B2 (en) 2006-03-20 2011-02-22 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US8475133B2 (en) 2008-12-05 2013-07-02 Modular Wind Energy, Inc. Efficient wind turbine blades, wind turbine blade structures, and associated systems and methods of manufacture, assembly and use
US8480370B2 (en) 2008-12-05 2013-07-09 Modular Wind Energy, Inc. Efficient wind turbine blades, wind turbine blade structures, and associated systems and methods of manufacture, assembly and use
US9500179B2 (en) 2010-05-24 2016-11-22 Vestas Wind Systems A/S Segmented wind turbine blades with truss connection regions, and associated systems and methods

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