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WO2004020284A3 - Wing structure - Google Patents

Wing structure Download PDF

Info

Publication number
WO2004020284A3
WO2004020284A3 PCT/IB2003/004336 IB0304336W WO2004020284A3 WO 2004020284 A3 WO2004020284 A3 WO 2004020284A3 IB 0304336 W IB0304336 W IB 0304336W WO 2004020284 A3 WO2004020284 A3 WO 2004020284A3
Authority
WO
WIPO (PCT)
Prior art keywords
spar
inflatable
wing structure
minor axis
lifting skin
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.)
Ceased
Application number
PCT/IB2003/004336
Other languages
French (fr)
Other versions
WO2004020284A2 (en
Inventor
Corydon C Roeseler
Mark Adam Ribkoff
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.)
GAASTRA KITEBOARDING INTERNATIONAL Ltd
GAASTRA KITEBOARDING INTERNAT
Original Assignee
GAASTRA KITEBOARDING INTERNATIONAL Ltd
GAASTRA KITEBOARDING INTERNAT
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 GAASTRA KITEBOARDING INTERNATIONAL Ltd, GAASTRA KITEBOARDING INTERNAT filed Critical GAASTRA KITEBOARDING INTERNATIONAL Ltd
Priority to AU2003265069A priority Critical patent/AU2003265069A1/en
Publication of WO2004020284A2 publication Critical patent/WO2004020284A2/en
Publication of WO2004020284A3 publication Critical patent/WO2004020284A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/036—Hang-glider-type aircraft; Microlight-type aircraft having parachute-type wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/06—Kites
    • B64C2031/065—Kites of inflatable wing type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Surgical Instruments (AREA)
  • Tents Or Canopies (AREA)

Abstract

The invention relates to a wing structure comprising a single lifting skin (5) and an inflatable elongated spar (3) located at the leading edge thereof. According to the invention, the inflatable spar has a substantially oval, elliptic or teardrop shaped cross-section, the lifting skin being substantially secured to an upper surface of the spar (3) at a point near a minor axis of the spar. The cross-section shape is defined by at least one resilient internal web (8) or rib (13) substantially parallel to the minor axis, which is provided within the inflatable spar (3).
PCT/IB2003/004336 2002-08-28 2003-08-27 Wing structure Ceased WO2004020284A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2003265069A AU2003265069A1 (en) 2002-08-28 2003-08-27 Wing structure

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US23003402A 2002-08-28 2002-08-28
US10/230,034 2002-08-28

Publications (2)

Publication Number Publication Date
WO2004020284A2 WO2004020284A2 (en) 2004-03-11
WO2004020284A3 true WO2004020284A3 (en) 2004-04-22

Family

ID=31976388

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2003/004336 Ceased WO2004020284A2 (en) 2002-08-28 2003-08-27 Wing structure

Country Status (2)

Country Link
AU (1) AU2003265069A1 (en)
WO (1) WO2004020284A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ587521A (en) * 2010-06-02 2010-10-29 Aquadria Kite Design Ltd An inflatable wing with inflatable leading edge spar and rib(s) from spar to trailing edge in form of inflatable truss(es)
ES1078661Y (en) * 2013-02-01 2013-05-20 Pernichi Marcos Pedro Teres PERFECTED COMET
US9738390B2 (en) 2015-06-12 2017-08-22 Goodrich Corporation Reinforced slide tube
DE202015005513U1 (en) * 2015-08-04 2016-11-08 Swing Flugsportgeräte GmbH Umbrella cap, in particular for a sliding, falling, flex kite or surfboard screen
CN117002724B (en) * 2023-09-28 2023-12-22 北京大学 Wings and cross-media vehicles

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4708078A (en) * 1984-11-16 1987-11-24 Legaignoux Dominique M Propulsive wing with inflatable armature
FR2762583A1 (en) * 1997-04-25 1998-10-30 Bruno Legaignoux Control system for ellipsoidal sail of spherical lune shape
EP0985601A2 (en) * 1998-07-16 2000-03-15 Wolfgang Kalkbrenner Wing unit for manned and unmanned flying devices
FR2816913A1 (en) * 2000-11-17 2002-05-24 Philippe Combeau Traction wing with rigid leading edge for kite surfing comprises sleeve composed of inflated battens connected by partitions with lines for control of incidence angle and take off and landing

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4708078A (en) * 1984-11-16 1987-11-24 Legaignoux Dominique M Propulsive wing with inflatable armature
FR2762583A1 (en) * 1997-04-25 1998-10-30 Bruno Legaignoux Control system for ellipsoidal sail of spherical lune shape
EP0985601A2 (en) * 1998-07-16 2000-03-15 Wolfgang Kalkbrenner Wing unit for manned and unmanned flying devices
FR2816913A1 (en) * 2000-11-17 2002-05-24 Philippe Combeau Traction wing with rigid leading edge for kite surfing comprises sleeve composed of inflated battens connected by partitions with lines for control of incidence angle and take off and landing

Also Published As

Publication number Publication date
AU2003265069A8 (en) 2004-03-19
WO2004020284A2 (en) 2004-03-11
AU2003265069A1 (en) 2004-03-19

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