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FR3044290B1 - SINGLE-WATER TRACTION AND SUSPENSION WING - Google Patents

SINGLE-WATER TRACTION AND SUSPENSION WING Download PDF

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Publication number
FR3044290B1
FR3044290B1 FR1570083A FR1570083A FR3044290B1 FR 3044290 B1 FR3044290 B1 FR 3044290B1 FR 1570083 A FR1570083 A FR 1570083A FR 1570083 A FR1570083 A FR 1570083A FR 3044290 B1 FR3044290 B1 FR 3044290B1
Authority
FR
France
Prior art keywords
leading edge
trailing edge
wing
edge
maintaining
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.)
Active
Application number
FR1570083A
Other languages
French (fr)
Other versions
FR3044290A1 (en
Inventor
Richard Leloup
Yves Parlier
Christophe Roussel
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.)
Ocea SA
Original Assignee
Ocea SA
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 Ocea SA filed Critical Ocea SA
Priority to FR1570083A priority Critical patent/FR3044290B1/en
Priority to PCT/FR2016/000185 priority patent/WO2017093618A1/en
Publication of FR3044290A1 publication Critical patent/FR3044290A1/en
Application granted granted Critical
Publication of FR3044290B1 publication Critical patent/FR3044290B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C31/00Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/06Kites
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H9/00Marine propulsion provided directly by wind power
    • B63H9/04Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
    • B63H9/06Types of sail; Constructional features of sails; Arrangements thereof on vessels
    • B63H9/069Kite-sails for vessels

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)
  • Wind Motors (AREA)

Abstract

La présente invention concerne une aile monopeau de type pilotable, tenue par au moins deux lignes aux extrémités. Plus particulièrement, il s'agit d'une aile monopeau dont le bord d'attaque est doté d'intercaissons procurant un profil aérodynamique optimal. Il s'agit d'une aile monopeau de type pilotable comprenant au moins une paroi souple constituée d'un extrados, limité par un bord d'attaque et un bord de fuite, comprenant une portion d'intrados, délimitée par le bord d'attaque et par un bord de fuite de l'intrados distinct dudit bord de fuite, qui s'étend sensiblement le long du bord d'attaque, l'ensemble comprenant ladite portion d'intrados et une partie de l'extrados le long du bord d'attaque constitue un moyen de maintien de forme aérodynamique, ledit moyen de maintien de forme aérodynamique comprenant au moins deux moyens de séparation, le compartiment ainsi formé entre deux moyens de séparation constituant un moyen de maintien de forme aérodynamique d'une cellule, ledit bord d'attaque et ledit bord de fuite se rejoignant de part et d'autre en au moins un point d'attache d'au moins un moyen de commande à distance de ladite aile, chaque moyen de commande à distance comprenant au moins une ligne principale, ledit bord de fuite comprend au moins un moyen de mise en tension.The present invention relates to a monoskin wing of the controllable type, held by at least two lines at the ends. More specifically, it is a single-skin wing whose leading edge is equipped with interboxes providing an optimal aerodynamic profile. It is a single-skin wing of the controllable type comprising at least one flexible wall consisting of an upper surface, limited by a leading edge and a trailing edge, comprising a portion of lower surface, delimited by the leading edge. attack and by a trailing edge of the underside distinct from said trailing edge, which extends substantially along the leading edge, the assembly comprising said underside portion and a part of the upper surface along the edge attack constitutes means for maintaining the aerodynamic shape, said means for maintaining the aerodynamic shape comprising at least two separating means, the compartment thus formed between two separating means constituting a means for maintaining the aerodynamic shape of a cell, the said leading edge and said trailing edge meeting on either side at at least one attachment point of at least one remote control means of said wing, each remote control means comprising at least one line main, said trailing edge compr end at least one tensioning means.

FR1570083A 2015-11-30 2015-11-30 SINGLE-WATER TRACTION AND SUSPENSION WING Active FR3044290B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1570083A FR3044290B1 (en) 2015-11-30 2015-11-30 SINGLE-WATER TRACTION AND SUSPENSION WING
PCT/FR2016/000185 WO2017093618A1 (en) 2015-11-30 2016-11-21 Single skin wing for traction and lift

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1570083A FR3044290B1 (en) 2015-11-30 2015-11-30 SINGLE-WATER TRACTION AND SUSPENSION WING

Publications (2)

Publication Number Publication Date
FR3044290A1 FR3044290A1 (en) 2017-06-02
FR3044290B1 true FR3044290B1 (en) 2021-10-29

Family

ID=56117782

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1570083A Active FR3044290B1 (en) 2015-11-30 2015-11-30 SINGLE-WATER TRACTION AND SUSPENSION WING

Country Status (2)

Country Link
FR (1) FR3044290B1 (en)
WO (1) WO2017093618A1 (en)

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3131874A1 (en) * 1981-08-12 1983-02-24 Hartlev 5600 Wuppertal Liebchen Construction of a wing for light aircraft (hang-gliders or kites) by means of a profiled strut and sail
FR2750885A1 (en) 1996-07-11 1998-01-16 Int Technic Sails Wind Time Steerable kite in shape of parachute
WO1999059866A1 (en) * 1998-05-19 1999-11-25 Peter Robert Lynn An improved kite
FR2823711B1 (en) 2001-04-24 2007-03-30 Gilles Collee CONCEPT OF TRACTION SAILING MONOPEAU WITHOUT EDGE RIGID ATTACK
AU2003222775A1 (en) 2002-03-26 2003-10-08 Georg Koziel Tubekite with an improved aerodynamic profile
US7093803B2 (en) 2003-12-16 2006-08-22 Culp David A Apparatus and method for aerodynamic wing
FR2913951A1 (en) * 2007-03-20 2008-09-26 Alexandre Pierre Antoine Jumel Load e.g. sportsman, traction kite for use during e.g. kitesurfing, has rigid element maintaining negative dihedral at kite, and ribs formed of upper and lower parts, where lower parts of ribs and central part of aerofoil are concave
DE102008039434A1 (en) * 2008-08-25 2010-03-04 Bernhard Jochum Kite for kitesurfing, has arc-shaped sail surface extending from front edge to rear edge, connecting elements connecting kite with control system, and tensioning element adjustable in length for changing geometry of sail surface
DE102009009305B4 (en) * 2009-02-12 2018-06-28 Peter Achilles Tubekite with lower sail
DE202013009409U1 (en) * 2013-10-21 2013-12-04 Steffen Born Singleskin kite with flow element
DE202015001217U1 (en) 2015-02-11 2015-03-25 Steffen Born Singleskin kite with slat

Also Published As

Publication number Publication date
WO2017093618A1 (en) 2017-06-08
FR3044290A1 (en) 2017-06-02

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