FR3044290B1 - SINGLE-WATER TRACTION AND SUSPENSION WING - Google Patents
SINGLE-WATER TRACTION AND SUSPENSION WING Download PDFInfo
- 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
Links
- 239000000725 suspension Substances 0.000 title 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title 1
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
- B64C31/06—Kites
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H9/00—Marine propulsion provided directly by wind power
- B63H9/04—Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
- B63H9/06—Types of sail; Constructional features of sails; Arrangements thereof on vessels
- B63H9/069—Kite-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.
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)
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 |
-
2015
- 2015-11-30 FR FR1570083A patent/FR3044290B1/en active Active
-
2016
- 2016-11-21 WO PCT/FR2016/000185 patent/WO2017093618A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2017093618A1 (en) | 2017-06-08 |
FR3044290A1 (en) | 2017-06-02 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20170602 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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RN | Application for restoration |
Effective date: 20190807 |
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FC | Decision of inpi director general to approve request for restoration |
Effective date: 20191017 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |