[go: up one dir, main page]

NL2034019B1 - Kite control system - Google Patents

Kite control system Download PDF

Info

Publication number
NL2034019B1
NL2034019B1 NL2034019A NL2034019A NL2034019B1 NL 2034019 B1 NL2034019 B1 NL 2034019B1 NL 2034019 A NL2034019 A NL 2034019A NL 2034019 A NL2034019 A NL 2034019A NL 2034019 B1 NL2034019 B1 NL 2034019B1
Authority
NL
Netherlands
Prior art keywords
tube
kite
kite control
control bar
control system
Prior art date
Application number
NL2034019A
Other languages
Dutch (nl)
Inventor
Dennis Brian
Original Assignee
Handelsonderneming Kubus B V
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 Handelsonderneming Kubus B V filed Critical Handelsonderneming Kubus B V
Priority to NL2034019A priority Critical patent/NL2034019B1/en
Priority to EP24153366.0A priority patent/EP4410658A1/en
Application granted granted Critical
Publication of NL2034019B1 publication Critical patent/NL2034019B1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H8/00Sail or rigging arrangements specially adapted for water sports boards, e.g. for windsurfing or kitesurfing
    • B63H8/10Kite-sails; Kite-wings; Control thereof; Safety means therefor
    • B63H8/16Control arrangements, e.g. control bars or control lines

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)

Abstract

Kite control system (1) for a kite, comprising a kite control bar (2) and a tube (3) transversal to the kite control bar (2) which at least houses trim lines of the kite inside said tube (3), wherein. the kite control bar (2) is equipped. with an aperture (4), and said tube (3) is guided through the aperture (4) of the kite control bar (2), wherein the trim lines connect to a swivel (5) provided on the tube (3) at a location distant from the kite control bar (2), and the kite control bar (2) is provided with a bearing piece (8) that is rotatably located. in the aperture (4) of the kite control bar (2), wherein said bearing piece (8) is provided with a through hole (9) that is equipped to receive and frictionally engage the 15 tube (3) that is transversal to the kite control bar (2).

Description

Kite control system
The invention relates to a kite control system for a kite.
US 8,459,595 discloses a safety system for use in conjunction with a kite control bar wherein two front lines are secured by a front line swivel positioned between the kite control bar and the kite. One front line terminates at the swivel and one extension of the other front line, the center line, travels through a central aperture in the swivel. The center line is then routed through an aperture on the control bar and terminated with an end that can be secured to the user either manually or by a leash arrangement. The swivel allows any twists that may form in the front lines to unwind.
The invention in particular relates to a kite control system for a kite, comprising a kite control bar and a tube transversal to the kite control bar which at least houses trim lines of the kite inside said tube, wherein the kite control bar is equipped with an aperture, and said tube is guided through the aperture of the kite control bar, wherein the trim lines connect to a swivel provided on the tube at a location distant from the kite control bar. Also in this arrangement the swivel allows any twists that may form in the trim lines to unwind, this being referred to as the auto-swiveling function.
A problem with this known arrangement is the added friction between the kite control bar and the tube supporting the swivel, which added friction can interfere with the operation of the kite control bar. This is a problem because the kite control bar is used to modulate the pull of the kite by sliding the bar in and out, or "sheeting in / out" on the kite.
The kite control bar is also used to steer the kite by pulling asymmetrically on the kite control bar, thereby rotating the bar by a certain angle relative to the power lines connected to the extremities of the kite control bar. The higher the angle of rotation of the kite control bar, the more aggressive the steering of the kite. Accordingly a significant friction can develop between the tube and the kite control bar, when the steering angle is high. This friction hampers the ability of the user to slide the bar on the tube to sheet in or out.
This friction could be reduced by making the aperture in the kite control bar bigger. But, if the aperture is too big, the auto-swiveling function cannot work. Auto-swiveling requires a relatively tight fit between the tube and the aperture in the kite control bar.
The invention is aimed to provide a solution for at least part of this problem.
The kite control system of the invention has the features of one or more of the appended claims.
According to a first aspect of the invention the kite control bar is provided with a bearing piece that is rotatably located in the aperture of the kite control bar, wherein said bearing piece is provided with a through hole that is equipped to receive and frictionally engage the tube that is transversal to the kite control bar.
Since the bearing piece is rotatably provided in the kite control bar, the bearing piece easily accommodates a high steering angle. Further the bearing through hole fits the tube tightly enough to be able to transmit the torque required for the auto-swiveling function.
- 3 =
Preferably the through hole in the bearing piece accommodates back-and-forth sliding of the tube. For this purpose it is preferred that the bearing piece has a through hole matching the cross-sectional shape of the tube, so the tube may slide through it easily. Thus, the bearing allows for a high steering angle without compromising the low-friction sliding action required to sheet in and out.
Preferably the tube has a noncircular outer circumference, and the through hole is shaped matching the noncircular outer circumference of the tube so as to enable the transfer of torque forces between the tube and the bearing piece.
Advantageously the noncircular outer circumference of the tube is elliptical.
According to another aspect of the invention, when seen in its longitudinal direction the tube is provided with at least two chambers, each chamber running in said longitudinal direction.
This is beneficial for arranging that the trim lines are provided to run through two separate chambers of the tube.
It is also possible that in its longitudinal direction the tube is provided with three chambers, each chamber running in said longitudinal direction.
The accompanying drawing, which is incorporated into and forms a part of the specification, illustrates one or more embodiments of the present invention and, together with the description, serves to explain the principles of the invention. The drawing is only for the purpose of illustrating one or more embodiments of the invention and is not to be construed as limiting the invention.
In the drawings:
- figure 1 shows a kite control system of the invention; - figure 2 shows a detail of the kite control system of figure 1; — figure 3 shows the bearing piece together with the kite control bar and the transversal tube; and - figure 4 provides a view at the transversal tube.
Whenever in the figures the same reference numerals are applied, these numerals refer to the same parts.
Figure 1 and figure 2 show a kite control system 1 for a kite.
The kite is not depicted in the figures but is generally known, so there is no need to show the kite, in particular not since the invention does not reside in the kite but in the kite control system 1.
The kite control system 1 comprises a kite control bar 2 and a tube 3 transversal to the kite control bar 2, wherein the tube 3 at least houses trim lines (not visible) of the kite inside said tube 3. Usually the tube 3 is of polyurethane, but this is not essential.
The kite control bar 2 is equipped with an aperture 4, and the tube 3 is guided through the aperture 4 of the kite control bar 2. Further the {not visible) trim lines connect to a swivel 5 provided on the tube 3 at a location distant from the kite control bar 2.
Other features that are shown in figure 1 and figure 2 that do not directly relate to the invention are a quick release feature 6 that allows the user to disconnect the ends of the (not visible) trim lines from the harness worn by the user to release the power from the kite and avoid accidents. The connection to the harness worn by the user is through a flexible U-shaped loop 7, also called chicken loop.
According to the invention the kite control bar 2 is provided with a bearing piece 8, which is most clearly shown in exploded view in figure 3. The bearing piece 8 is rotatably located in the aperture 4 of the kite control bar 2, wherein said bearing piece 8 is provided with a through hole 9 that is equipped to receive and frictionally engage the tube 3 that is transversal to the kite control bar 2.
Figure 3 shows that the tube 3 has a noncircular outer circumference 3’. It is shown that the noncircular outer circumference 3’ of the tube 3 is elliptical. Correspondingly the through hole 4 is shaped matching the noncircular outer circumference 3’ of the tube 3 so as to enable the transfer of torque forces between the tube 3 and the bearing piece 8.
Advantageously the through hole 4 in the bearing piece 8 accommodates back-and-forth sliding of the tube 3.
With further reference to figure 4 it shows that in its longitudinal direction the tube 3 is provided with at least two and preferably three chambers 10, each chamber 10 running in said longitudinal direction of the tube 3. The (not visible) trim lines are provided to run through two separate chambers of the tube 3.
Embodiments of the present invention can include every combination of features that are disclosed herein independently from each other. Although the invention has been discussed in the foregoing with reference to an exemplary embodiment of the invention, the invention is not restricted to this particular embodiment which can be varied in many ways without departing from the invention. The discussed exemplary embodiment shall therefore not be used to construe the append- ed claims strictly in accordance therewith. On the contrary the embodiment is merely intended to explain the wording of the appended claims without intent to limit the claims to this exemplary embodiment. The scope of protection of the invention shall therefore be construed in accordance with the appended claims only, wherein a possible ambiguity in the wording of the claims shall be resolved using this exemplary embodiment.
Variations and modifications of the present invention will be obvious to those skilled in the art and it is intended to cover in the appended claims all such modifications and equivalents. The entire disclosures of all references, applications, patents, and publications cited above are hereby incorporated by reference. Unless specifically stated as being “essential” above, none of the various components or the interrelationship thereof are essential to the operation of the invention. Rather, desirable results can be achieved by substituting various components and/or reconfiguration of their relationships with one another.
Aspects of the invention are itemized in the following section. 1. Kite control system (1) for a kite, comprising a kite control bar (2) and a tube (3) transversal to the kite control bar (2) which at least houses trim lines of the kite inside said tube (3), wherein the kite control bar (2) is equipped with an aperture (4), and said tube (3) is guided through the aperture (4) of the kite control bar (2), wherein the trim lines connect to a swivel (5) provided on the tube (3) at a location distant from the kite control bar (2), characterized in that the kite control bar (2) is provided with a bearing piece (8) that is rotatably located in the aperture (4) of the kite control bar (2), wherein said bearing piece (8) is provided with a through hole {9) that is equipped to receive and frictionally engage the tube (3) that is transversal to the kite control bar (2). 2. Kite control system according to claim 1, characterized in that the tube (3) has a noncircular outer circumference (3), and the through hole (9) is shaped matching the noncircular outer circumference (3')}) of the tube (3) so as to enable the transfer of tordue forces between the tube (3) and the bearing piece (8).
3. Kite control system according to claim 1 or 2, characterized in that the through hole (9) in the bearing piece (8) accommodates back-and-forth sliding of the tube (3).
4. Kite control system according to any one of claims 1-3, characterized in that the noncircular outer circumference
{37} of the tube (3) is elliptical.
5. Kite control system according to any one of claims 1-4, characterized in that in its longitudinal direction the tube (3) is provided with at least two chambers (10), each chamber running in said longitudinal direction.
6. Kite control system according to any one of claims 1-5, characterized in that in its longitudinal direction the tube is provided with three chambers (10), each chamber running in said longitudinal direction.
7. Kite control system according to claim 5 or 6,
characterized in that the trim lines are provided to run through two separate chambers (10) of the tube (3).

Claims (7)

CONCLUSIESCONCLUSIONS 1. Vliegerbesturingssysteem (1) voor een vlieger, omvattend een vliegerbedieningsstang (2) en een buis (3) dwars op de vliegerbedieningsstang (2) die ten minste de trimlijnen van de vlieger in genoemde buis (3) herbergt, waarbij de vliegerbedieningsstang (2) is voorzien van een opening (4), en genoemde buis (3) door de opening (4) van de vliegerbedieningsstang (2) is geleid, waarbij de trimlijnen aansluiten op een wartel (5) die op een afstand van de vliegerbedieningsstang (2) op de buis (3) is aangebracht, met het kenmerk, dat de vliegerbedieningsstang (2) is voorzien van een lagerstuk (8) dat draaibaar in de opening (4) van de vliegerbedieningsstang (2) is opgenomen, waarbij het lagerstuk {8) is voorzien van een doorgaand gat (9) dat is uitgerust om de buis (3) die dwars op de vliegerbedieningsstang (2) staat op te nemen en met wrijving aan te grijpen.1. Kite control system (1) for a kite, comprising a kite control rod (2) and a tube (3) transverse to the kite control rod (2) accommodating at least the trim lines of the kite in said tube (3), the kite control rod (2) being provided with an opening (4), and said tube (3) being guided through the opening (4) of the kite control rod (2), the trim lines connecting to a swivel (5) arranged on the tube (3) at a distance from the kite control rod (2), characterised in that the kite control rod (2) is provided with a bearing piece (8) rotatably accommodated in the opening (4) of the kite control rod (2), the bearing piece (8) being provided with a through hole (9) adapted to receive and frictionally engage the tube (3) extending transversely to the kite control rod (2). 2. Vliegerbesturingssysteem volgens conclusie 1, met het kenmerk, dat de buis (3) een niet-cirkelvormige buitenomtrek (3') heeft en het doorgaande gat (2) is gevormd passend bij de niet-cirkelvormige buitenomtrek (3') van de buis (3) om de overdracht van torsiekrachten tussen de buis {3) en het lagerstuk (8) mogelijk te maken.2. A kite control system according to claim 1, characterised in that the tube (3) has a non-circular outer circumference (3') and the through hole (2) is formed to fit the non-circular outer circumference (3') of the tube (3) to allow the transmission of torsional forces between the tube (3) and the bearing piece (8). 3. Vliegerbesturingssysteem volgens conclusie 1 of 2, met het kenmerk, dat het doorlopende gat (9) in het lagerstuk (8) het heen en weer schuiven van de buis (3) toelaat.3. Kite control system according to claim 1 or 2, characterised in that the through hole (9) in the bearing piece (8) allows the tube (3) to slide back and forth. 4. Vliegerbesturingssysteem volgens een van de conclusies 1-3, met het kenmerk, dat de niet-cirkelvormige buitenomtrek (3') van de buis (3) elliptisch is.4. A kite control system according to any one of claims 1 to 3, characterised in that the non-circular outer circumference (3') of the tube (3) is elliptical. 5. Vliegerbesturingssysteem volgens een van de conclusies 1-4, met het kenmerk, dat de buis (3) in zijn lengterichting is voorzien van ten minste twee kamers (10), waarbij elke kamer in die lengterichting verloopt.5. Kite control system according to any one of claims 1 to 4, characterised in that the tube (3) is provided with at least two chambers (10) in its longitudinal direction, each chamber extending in said longitudinal direction. 6. Vliegerbesturingssysteem volgens een van de conclusies 1-5, met het kenmerk, dat de buis in zijn6. Kite control system according to any one of claims 1 to 5, characterised in that the tube in its - Gg - lengterichting is voorzien van drie kamers (10), waarbij elke kamer in die lengterichting verloopt.- Gg - longitudinal direction is provided with three chambers (10), each chamber running in that longitudinal direction. 7. Vliegerbesturingssysteem volgens conclusie 5 of 6, met het kenmerk, dat de trimlijnen zijn voorzien om door twee gescheiden kamers (10) van de buis (3) te lopen.7. Kite control system according to claim 5 or 6, characterised in that the trim lines are provided to pass through two separate chambers (10) of the tube (3).
NL2034019A 2023-01-24 2023-01-24 Kite control system NL2034019B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
NL2034019A NL2034019B1 (en) 2023-01-24 2023-01-24 Kite control system
EP24153366.0A EP4410658A1 (en) 2023-01-24 2024-01-23 Kite control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL2034019A NL2034019B1 (en) 2023-01-24 2023-01-24 Kite control system

Publications (1)

Publication Number Publication Date
NL2034019B1 true NL2034019B1 (en) 2024-07-30

Family

ID=85726387

Family Applications (1)

Application Number Title Priority Date Filing Date
NL2034019A NL2034019B1 (en) 2023-01-24 2023-01-24 Kite control system

Country Status (2)

Country Link
EP (1) EP4410658A1 (en)
NL (1) NL2034019B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102024103964A1 (en) * 2024-02-13 2025-08-14 Boards & More Gmbh Bar for controlling a kite, control system for a kite and kite system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202011109507U1 (en) * 2011-12-23 2012-02-01 Pure Action Sports Europe S.L. Control rod for stunt kites
DE202012101875U1 (en) * 2011-11-10 2012-06-15 Boards & More Gmbh Bar and insert
US20130048791A1 (en) * 2011-05-25 2013-02-28 Neil Pryde Limited Device for coupling of kite lines
US8459595B2 (en) 2007-10-17 2013-06-11 Tony Logosz Kite control device with free rotation

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8459595B2 (en) 2007-10-17 2013-06-11 Tony Logosz Kite control device with free rotation
US20130048791A1 (en) * 2011-05-25 2013-02-28 Neil Pryde Limited Device for coupling of kite lines
DE202012101875U1 (en) * 2011-11-10 2012-06-15 Boards & More Gmbh Bar and insert
DE202011109507U1 (en) * 2011-12-23 2012-02-01 Pure Action Sports Europe S.L. Control rod for stunt kites

Also Published As

Publication number Publication date
EP4410658A1 (en) 2024-08-07

Similar Documents

Publication Publication Date Title
NL2034019B1 (en) Kite control system
AU6851800A (en) Device for guiding at least a flexible elongated element such as a cable or the like, with substantially closed contour
EP3257725B1 (en) Telescopic steering column and steering device
CN109512369B (en) Bending part of endoscope and endoscope
US7574942B2 (en) Cable guide for an articulated joint
EP1650373B1 (en) Articulated arm for awnings
EP3257722B1 (en) Steering device
JP7135814B2 (en) roller unit
US20070245705A1 (en) Energy guiding chain
CA2474022A1 (en) Dolly
WO2020135362A1 (en) Bending part of endoscope, and endoscope
CZ148398A3 (en) Control device, controlled by a cable
CN104540722B (en) Tilt steering device
US6206353B1 (en) Clamping device for structural components
US12227981B2 (en) Spindle drive for a closure element of a motor vehicle
ATE449027T1 (en) HAND CABLE REEL
EP2020946B1 (en) Angled hose connection for dental handpiece
CZ289148B6 (en) Protective device for propeller shaft
KR20000010850A (en) Device for pouring out concrete
EP1495968B1 (en) Ergonomic cable tie installation tool
EP3501902B1 (en) Load carrier foot
US10843766B2 (en) Straddle vehicle
US4954119A (en) Sliding universal joint having cylindrical holder positioning means
ATE280298T1 (en) INTERMEDIATE GEAR FOR WINDOW OR DOOR FITTINGS
EP0922540B1 (en) Portable power tool with a power supply line support device