KITE LAUNCHING AND LANDING ASSIST DEVICE AND FLOATING UNIT
20250313321 ยท 2025-10-09
Assignee
Inventors
- Tateru FUKAGAWA (Fujisawa-shi, JP)
- Tetsuyuki Oe (Koganei-shi, JP)
- Mikikane Hirohata (Sunto-gun, JP)
- Yoshiharu Saito (Gotemba-shi, JP)
- Hayato MASUKI (Fuji-shi, JP)
Cpc classification
International classification
Abstract
A kite launching and landing assist device includes a cavity support portion in which a kite is detachably secured by tension of the tether when the tether is wound with a winch, and a cavity serving as an air channel is secured in a direction intersecting with a wind receiving surface of the kite, and includes a launching and landing buoy that is detachable from or detachable from the floating unit and is floatable.
Claims
1. A kite launching and landing assist device configured to assist in launching and landing a kite attached to a distal end of a tether in a floating unit, the floating unit including a winch configured to unwind and wind the tether, the kite launching and landing assist device comprising: a launching and landing buoy to which the kite is detachably secured with a tension of the tether from the winch when the tether is wound around the winch, the launching and landing buoy including a cavity support portion in which a cavity configured to serve as an air channel is provided in a direction intersecting a wind receiving surface of the kite, and the launching and landing buoy being floatable in such a manner that the launching and landing buoy is separated or detached from the floating unit; and a drive unit configured to, before launching and landing of the kite, separate the launching and landing buoy to a position where the tether or the kite does not interfere with the floating unit, and after the landing of the kite, tow or connect the launching and landing buoy to the floating unit.
2. The kite launching and landing assist device according to claim 1, wherein the cavity support portion includes a contact surface configured to contact the wind receiving surface at a predetermined launching angle when the kite is launched.
3. The kite launching and landing assist device according to claim 1, wherein the drive unit is configured to drive the launching and landing buoy toward the floating unit until the launching and landing buoy is stored at a storage position on the floating unit.
4. The kite launching and landing assist device according to claim 1, wherein the launching and landing buoy integrally includes the cavity support portion and a buoy portion configured to float on water.
5. A floating unit comprising the kite launching and landing assist device according to claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Features, advantages, and technical and industrial significance of exemplary embodiments of the disclosure will be described below with reference to the accompanying drawings, in which like signs denote like elements, and wherein:
[0013]
[0014]
[0015]
DETAILED DESCRIPTION OF EMBODIMENTS
[0016] Referring to
[0017] As shown in
[0018] The mast 10 and the sail 11 are configured to enable the floating unit 100 to navigate as a yacht. The floating unit 100 is preferably constructed as a catamaran vessel or a multi-hull vessel having excellent navigation performance and stability. The floating unit 100 may be caused to float on the water surface 110 on any water surface, such as on a lake, a river, or the like, in addition to the sea or the ocean.
[0019] The launching and landing assist device 1 is configured to include a buoy 7 which constitutes an example of a launching and landing buoy and has a cavity support portion for securing a cavity 7a therein, a wire 8 whose leading end is connected to the buoy 7, and an auxiliary winch 9 which constitutes an example of a drive unit capable of winding up and unwinding the root side of the wire-8. In the state of
[0020] In
[0021] In the present embodiment, in particular, the buoy 7 has a cavity support portion that defines or secures a cavity 7a, and when launching the kite 101, the wind in the vicinity of the water surface 110 is passed through the cavity 7a, so that the wind can be applied to the wind receiving surface of the kite 101 through the buoy 7. Consequently, launching of the kite 101 from the buoy 7 can be smoothly performed by the wind including the wind 101a hitting the kite 101 via the cavity 7a.
[0022] From the viewpoint of effectively utilizing such wind 101a, the cavity support portion of the buoy 7 has a contact surface that contacts the wind receiving surface of the kite 101 at a predetermined launching angle when launching the kite 101, whereby the angle of the contact surface may be set so that the cavity 7a becomes a channel through the wind 101a that raises the kite 101. That is, by setting the angle of the contact surface to a predetermined angle, it is possible to easily launch the kite 101. Such an angle may be set experimentally, empirically, mathematically, or by simulation as an angle at which the kite 101 is most likely to rise. On the other hand, the contact surface may be angled such that the cavity 7a is a channel through which the air that lowers the kite 101 is passed or a channel that uses the air as fine air so that smooth landing can be performed. Alternatively, the angle of the contact surface or the shape of the cavity 7a may be set to an angle or a shape of the cavity 7a that facilitates launching of the kite 101 during launching and that facilitates landing of the kite 101 during landing.
[0023] Such a cavity 7a does not need to be one, and may be configured to include a plurality or a plurality of communication holes as long as the wind 101a is meaningfully passed therethrough, and the cavity support portion of the buoy 7 may be configured from a cleared frame or from a punched material or a mesh-like material. In addition, the tether 102 may be configured to pass through the cavity 7a, unlike the configuration of
[0024] Further, the buoy 7 may be configured to integrally include a cavity support portion and a buoy portion floating in water. For example, the buoy 7 can be integrally formed from a member having a buoyancy function, a cavity function, a function of carrying strength, and the like. That is, the launching and landing assist device 1 can be constructed to have high functionality by making it relatively easy or inexpensive. However, the buoy 7 may be composed of a plurality of components or members, for example, a component that contributes to buoyancy, a component that contributes to securing a cavity 7a, and a component that contributes to feeding and feeding the tether 102 through the launching and landing assist device 1.
[0025] Next, as shown in
[0026] As a result, the kite 101 is secured to the launching and landing assist device 1 by the tension applied from the winch 5 via the tether 102, and the launching/landing assist device 1 is secured to the floating unit 100. That is, a part of the wind receiving surface of the kite 101 comes into contact with the contact surface of the buoy 7, so that the kite 101 is secured. As previously discussed, the tether 102 may be configured to pass through the cavity 7a, unlike the configuration of
[0027] Note that the buoy 7 is not merely connected to the floating unit 100, and may be stored in a storage position, a storage space, or a storage box provided in the floating unit 100, or may be configured to be pulled up on the deck of the floating unit 100. At this time, the storage operation and the pulling operation may be performed by the driving force of the winch 5 or the auxiliary winch 9 or the driving force of both of them.
[0028] Next, as shown in
[0029] As a result, the kite 101 is separated to a position where it does not interfere with the floating unit 100, particularly the mast 10 and the sail 11. At this position, the kite 101 is smoothly launched by receiving the wind 101b blown through the cavity 7a on the wind receiving surface. As previously discussed, the tether 102 may be configured to pass through the cavity 7a, unlike the configuration of
[0030] When the launching shown in
[0031] As described above in detail with reference to
[0032] Further, since the buoy 7 floating on the water surface 110 at a position away from the floating unit 100 can launch and land the kite 101, it is possible to avoid interference during launching and landing between the tether 102 and the kite 101 and the floating unit 100 (particularly, the sail 11 and the mast 10 thereof). At the same time, since it is not necessary to secure a large space for launching and landing on the floating unit 100, it is also possible to reduce the size of the floating unit 100.
[0033] In addition, if the buoy 7 remains fluctuated and suspended at a position separated from the floating unit 100 on the water surface 110, for example, a tow operation or a navigation operation, a standby operation, a tether-type power generation operation, or the like in the floating unit 100 may be hindered. However, before launching after or after landing as shown in
Additional Remarks
[0034] With regard to the embodiments described above, the following additional notes are further disclosed.
APPENDIX 1
[0035] The kite launching and landing assist device according to Appendix 1 of the present disclosure is provided with a winch for unwinding and winding a tether. A kite launching and landing assist device for assisting launching and landing of a kite attached to a tip of the tether, wherein the tether is wound up by the winch, and a cavity support portion in which a cavity configured to serve as an air channel is provided in a direction intersecting a wind receiving surface of the kite, and a launching and landing buoy which is separated or detached from the floating unit is provided. The launching and landing buoy is landed. A drive unit is provided for separating the tether or the kite from the floating unit and pulling or connecting to the floating unit after landing of the kite.
[0036] According to the kite launching and landing assist device according to Appendix 1 of the present disclosure, the launching and landing buoy is separated from the floating unit by a drive unit for launching and landing of the kite, and floats on water or the ocean at a position away from the floating unit. Here, the cavity support portion included in the launching and landing buoy has a cavity that serves as an air channel in a direction intersecting the wind receiving surface of the kite, and thus launching/landing can be performed in a state where the wind receiving surface of the kite receives wind through the cavity. In particular, during launching, a state in which the kite is likely to float in the air due to the wind can be quickly secured by the air flowing through the cavity to launch the kite.
[0037] Further, since the launching and landing buoy floating on the water at a position away from the floating unit allows launching and landing of the kite, it is possible to avoid interference at the time of launching and landing between the tether or the kite and the floating unit. At the same time, since it is not necessary to secure a large space on the floating unit for launching and landing, it is also possible to reduce the size of the floating unit.
[0038] In addition, if the launching and landing buoy remains floating at a position separated from the floating unit on the water, for example, towing operation or navigation operation in the floating unit may be hindered. However, before or after a launching, or after a launching where the kite is flying high, the drive unit pulls or connects the launching and landing buoy to the floating unit, so that the floating unit and the launching and landing buoy become a single unit or an integral unit, thereby preventing problems as described above.
APPENDIX 2
[0039] The kite launching and landing assist device according to Appendix 2 of the present disclosure is the kite launching and landing assist device according to Appendix 1, wherein the cavity support portion has a contact surface that contacts the wind receiving surface at a predetermined launching angle when launching the kite.
[0040] According to the kite launching and landing assist device according to Appendix 2 of the present disclosure, the angle of the contact surface is set so that the cavity becomes a channel through which the wind for raising the kite is passed, that is, the contact surface is set to a predetermined launching angle, so that the kite can be easily launched.
APPENDIX 3
[0041] The kite launching and landing assist device according to Appendix 3 of the present disclosure is the kite launching and landing assist device according to Appendix 1 or 2, wherein the drive unit is configured to be capable of driving the launching and landing buoy toward the floating unit until the launching and landing buoy is stored at the storage position of the floating unit.
[0042] According to the rollover prevention device described in Appendix 3 of the present disclosure, if there is a launching and landing buoy separated from the floating unit on the water surface, the power generation operation, the towing operation, the standby operation, and the like in the floating unit may be hindered. However, according to the device described in Appendix 3, by storing the launching and landing buoy in the storage position or the storage space provided behind the floating unit by the drive unit, such trouble can be prevented in advance.
APPENDIX 4
[0043] The kite launching and landing assist device according to Appendix 4 of the present disclosure is the kite launching and landing assist device according to any one of Appendices 1 to 3, wherein the launching and landing buoy integrally has the cavity support portion and a buoy portion configured to float on water.
[0044] According to the rolling prevention device described in Appendix 4 of the present disclosure, the launching and landing buoy can be integrally formed from a component or a member having a buoyancy function, a cavity function, a function of carrying strength, and the like. That is, the launching and landing assist device can be constructed to have high functionality by making it relatively easy or inexpensive.
APPENDIX 5
[0045] The floating unit according to Appendix 5 of the present disclosure includes the kite launching and landing assist device according to any one of Appendices 1 to 4.
[0046] According to the floating unit described in Appendix 5 of the present disclosure, since it has the kite launching and landing assist device according to any one of Appendices 1 to 4 described above, without interfering with the floating unit, it is possible to smoothly launch and land the kite, and it is also possible to reduce the size of the floating unit.
[0047] The present disclosure can be modified as appropriate within the scope and spirit of the disclosure that can be read from the claims and the specification as a whole, and a kite launching and landing assist device base or a floating unit with such a modification is also included in the technical idea of the present disclosure.