WO2016062238A1 - 水面机翼船 - Google Patents

水面机翼船 Download PDF

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Publication number
WO2016062238A1
WO2016062238A1 PCT/CN2015/092292 CN2015092292W WO2016062238A1 WO 2016062238 A1 WO2016062238 A1 WO 2016062238A1 CN 2015092292 W CN2015092292 W CN 2015092292W WO 2016062238 A1 WO2016062238 A1 WO 2016062238A1
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WIPO (PCT)
Prior art keywords
hull
side edge
rear side
edge
pontoon
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Ceased
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PCT/CN2015/092292
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English (en)
French (fr)
Inventor
林建兴
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Individual
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Individual
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Priority to CN201580057271.3A priority Critical patent/CN107074323B/zh
Publication of WO2016062238A1 publication Critical patent/WO2016062238A1/zh
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/248—Shape, hydrodynamic features, construction of the foil
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/02—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
    • B63B1/10—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls
    • B63B1/107—Semi-submersibles; Small waterline area multiple hull vessels and the like, e.g. SWATH
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/26—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type having more than one hydrofoil
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
    • B63B1/322—Other means for varying the inherent hydrodynamic characteristics of hulls using aerodynamic elements, e.g. aerofoils producing a lifting force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H7/00—Propulsion directly actuated on air
    • B63H7/02—Propulsion directly actuated on air using propellers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00—Maritime or waterways transport
    • Y02T70/10—Measures concerning design or construction of watercraft hulls

Definitions

  • This invention relates to a surface wing ship, and more particularly to a surface wing ship that is more smoothly deployed on the surface of the water by its pontoon structure.
  • Hydrofoil is a high speed craft with a bracket at the bottom of the hull to install the hydrofoil. As the speed of the ship gradually increases, the hydrofoil can provide buoyancy to lift the hull off the surface of the water, forming a so-called hydrofoil or hydrofoil, thereby greatly reducing the resistance of the water and increasing the speed of navigation.
  • a water surface wing vessel 10 previously proposed by the inventor of the present invention, which includes a hull 11 having a corresponding number of wings 12 on both sides of the hull 11 and each of the wings 12
  • the rim is provided with a propeller 121, and a pontoon device 13 is disposed at the bottom of the hull 11.
  • the pontoon device 13 has a plurality of elongated first pontoons 131, and a propeller 135 is disposed at each end of the first pontoon 131, and passes through an edge.
  • the first pontoon 131 extends a sheet-like connecting portion 132 that is connected to the bottom of the hull 11.
  • the pontoon device 13 is provided with two second pontoons 133 adjacent to the bottom of the hull 11 on both sides of the hull 11. Each of the second pontoons 133 is bent by two The joint 134 is connected to the hull 11, whereby, as shown in FIG. 2, when the surface winger 10 is known to be stationary on the water surface, the first pontoon 131 is completely submerged under the water surface, and the second pontoon 133 is floated on the water surface in contact with the water surface to float the hull 11 above the water surface, and when the surface wing ship 10 is known to fly on the water surface, the connecting portion 132 of the first pontoon 131 and the second portion are made The pontoon 133 completely leaves the water surface and makes a steady flight in the air.
  • the pontoons of the pontoon device 13 of the surface wing vessel 10 are elongated structures extending along the hull 11, regardless of whether the surface wingcraft 10 is stationary or in a running state, as long as the waves are hit by the sides of the hull 11. It will hit the first pontoon 131 or the second pontoon 133 over a large area, and it is easy to cause the hull 11 to sway and shift; in particular, in the case of a pontoon that can slightly shunt the waves in a long cylindrical shape, on the surface of the water When the wing boat 10 is driving fast, the waves struck on both sides not only hit the first pontoon 131, but also the first pontoon 131.
  • the sheet-like connecting portion 132 strikes the contact to form a force that more significantly turbulates the hull 11.
  • the difficulty in controlling the surface crane 10 to remain horizontal is extremely high, and the hull 11 can only be connected by the connecting portion 132, and then the wing 12 can be kept in a horizontal state.
  • the wing 12 when the wing 12 is in contact with the unstable airflow, it will cause the first pontoon 131 to move upward or downward along with the surface wingcraft 10 as a whole, so that the circumferential side of the first pontoon 131 is changed from the average force to Face contact in a single direction produces unpredictable path changes after high-speed water flow impact.
  • the reaction force of water is much larger than that of air. Therefore, the faster the speed or the larger the angle, the more obvious the impact will be.
  • the entire surface wing vessel 10 will be quickly moved up or down, resulting in an unstable navigation.
  • the surface crane 10 has a space for further improvement in how to improve the running stability to increase the safety and comfort of the ride.
  • An object of the present invention is to provide a surface wing ship comprising a hull, even-numbered wings disposed on opposite sides of the hull, and even-numbered pontoons disposed on both sides of the bottom of the hull, each of the pontoons being formed into a hollow flat shape.
  • a propeller is arranged on the rear side edge, whereby the pontoon structure design at the bottom of the hull causes the waves from both sides of the hull to mainly hit the connection portion of each pontoon, thereby reducing the wave from the hull on the pontoon.
  • the resulting reaction force achieves the purpose of improving the stability of the hull driving and increasing the safety and comfort of the ride.
  • the present invention provides a surface crane ship comprising: a hull having an opposite front end and a rear end, the bottom connection between the front and rear ends; an even number of buoys, Paired in the bottom of the hull, each of the pontoons is formed into a hollow flat shape having an inner side surface and an outer side surface corresponding to the two sides of the hull, and a front side edge and a bottom edge between the inner and outer side surfaces a rear side edge is connected, and a propeller is disposed on a rear side edge of each of the buoys to generate a propulsive force in the water; and an even number of wings are disposed in pairs on opposite sides of the hull, and each of the wings is provided At least one propeller acts to generate propulsion in the air.
  • each of the buoys connects the inner and outer sides through a front side edge, a bottom edge and a rear side edge, and defines a set of connecting portions disposed at the bottom of the hull.
  • a buoyancy portion that is expanded into the shape of a wafer from the connection the wafer-shaped buoyancy portion of the float has a center along which the extension extends toward the bottom of the hull, and the connection portion can be erected toward the bottom of the hull. Or inclined toward the rear end of the hull to further reduce the forward resistance generated by the pontoon.
  • the propeller of the pontoon has a shaft portion
  • the rear side edge of the pontoon is provided with a mounting seat
  • the mounting seat is disposed at a tangent to the rear side edge and a tangent perpendicular to the bottom of the hull, so that the propeller shaft
  • the portion is coupled to the mount parallel to the bottom of the hull to provide better driving performance of the hull.
  • the pontoon in the surface wing ship of the present invention, can be formed into a flat shape with the front and rear side edges thereof, and the bottom edge of the pontoon is formed in a flat oblique shape which is inclined from the front to the rear toward the bottom of the hull.
  • the angle of inclination between the bottom edge and the bottom of the hull is adjusted to reduce the resistance of the pontoon in the water.
  • the front side edge section of the pontoon can be shaped into a V shape to utilize the pointed front end to allow water to flow to both sides of the pontoon, thereby achieving the purpose of reducing the resistance in the water.
  • each of the wings may be a sheet-like body or a wheel-shaped body, and the wing can adjust the set angle by rotating to control the deflection angle, so that the bottom of the hull is away from the water surface. Fly at a predetermined altitude.
  • Figure 1 is a schematic perspective view of a known surface sailor.
  • Fig. 2 is a schematic front view showing the structure of a known surface ship on a water surface.
  • Fig. 3 is a perspective view showing the structure of a surface crane of the present invention.
  • Figure 4 is a side elevational view showing the surface wing ship of the present invention.
  • Fig. 5 is a front view showing the structure of the surface crane of the present invention when it is stationary on the water surface.
  • Figure 6 is a cross-sectional view showing the first embodiment of the surface crane pontoon structure of the present invention.
  • Fig. 7 is a perspective view showing the other embodiment of the wing of the surface machine wing of the present invention.
  • Figure 8 is a side elevational view showing another embodiment of the wing of a surface machine wing of the present invention.
  • Figure 9 is a front elevational view showing another embodiment of the surface wing wing of the present invention when it is stationary on the water surface.
  • Figure 10 is a cross-sectional view showing a second embodiment of the surface crane pontoon structure of the present invention.
  • Figure 11 is a cross-sectional view showing a third embodiment of the surface crane pontoon structure of the present invention.
  • Figure 12 is a cross-sectional view showing a fourth embodiment of the surface crane pontoon structure of the present invention.
  • Figure 13 is a cross-sectional view showing a fifth embodiment of the surface crane pontoon structure of the present invention.
  • Figure 14 is a perspective view showing the appearance of a sixth embodiment of the surface crane pontoon structure of the present invention.
  • Figure 15 is a cross-sectional view showing a sixth embodiment of the surface crane pontoon structure of the present invention.
  • the surface winger of the present invention includes a hull 20, even pontoons 30 disposed on opposite sides of the bottom 23 of the hull 20, and even-numbered lobes 40 disposed on opposite sides of the hull 20, wherein:
  • the hull 20 has a front end 21 and a rear end 22, and a bottom 23 is connected between the front and rear ends 21, 22.
  • the hull 20 can be in a predetermined shape, and the inside is provided with a seat.
  • the shape of the transport space, and the bottom 23 of the hull 20 can be slightly in contact with the waves on the water surface in a stationary state, and completely exit the water surface by a predetermined height at the time of flight.
  • each of the buoys 30 is formed into a hollow flat shape, and is disposed in a direction in which the flat peripheral edge corresponds to the front and rear ends 21 and 22 of the hull 20 .
  • the bottom portion 23 of the hull 20 has the effect of reducing the forward resistance of the hull 20 while providing the required buoyancy of the hull 20.
  • Each of the buoys 30 has an inner side 31 and an outer side 32 corresponding to both sides of the hull 20.
  • a front side edge 33, a bottom edge 34 and a rear side edge 35 are connected between the outer side surfaces 31 and 32, and a spiral 36 is disposed on the rear side edge 35 of each of the buoys 30 to generate a propulsive force in the water.
  • the front side edge 33, the bottom edge 34 and the rear side edge 35 of each of the buoys 30 The cross section is curved, and the inner and outer sides 31, 32 are connected at both ends of the curved shape.
  • the front side edge 33 and the rear side edge 35 are correspondingly formed into a straight section 331, 351 and a circular arc section 332.
  • the bottom edge 34 is formed into a circular arc shape and is connected to the arc segments 332, 352 of the two front and rear side edges 33, 35 at both ends of the arc, so that the two straight segments 331, 351 and the inner,
  • the outer side surfaces 31, 32 collectively define a connecting portion 301 assembled to the bottom portion 23 of the hull 20, and the two circular arc segments 332, 352, the bottom edge 34 and the inner and outer side surfaces 31, 32 together define a round cake shape.
  • the buoyancy portion 302 is disposed on the arc segment 352 of the rear side edge 35; as shown in FIG. 5, when the buoy 30 is in a stationary state, the connecting portion 301 is almost entirely below the water surface, when flying, The buoyancy portion 302 is located below the water surface and the connection portion 301 is located on the water surface.
  • the propeller 36 of the pontoon 30 of the present invention has a shaft portion 361, the rear side edge 35 of the pontoon 30 is provided with a mounting seat 353, and the mounting seat 353 is disposed at the rear side edge 35 of the arc segment 352 and perpendicular to the hull
  • the tangent of the tangent of the bottom 23 of the 20 is such that the shaft portion 361 of the propeller 36 is brought into contact with the mount 353 parallel to the bottom 23 of the hull 20.
  • the wafer-shaped buoyancy portion 302 of the pontoon 30 has a center P which extends along the center P toward the bottom portion 23 of the hull 20, and the connecting portion 301 faces the rear end 22 of the hull 20.
  • the inclined arrangement defines an angle ⁇ 1 between the connecting portion 301 and the bottom portion 23 of the hull 20, the angle ⁇ 1 being between 40 degrees and 90 degrees and less than 90 degrees being greater than 40 degrees (90° ⁇ ⁇ 1 ⁇ 40°).
  • the airfoil 40 is provided with at least one propeller 41.
  • the airfoil wing is provided with four wings 40, each of which is provided with four wings 40.
  • the wing 40 is provided with two propellers 41 to generate propulsive force in the air, but the number of the wing 40 and the propeller 41 is not limited thereto, and may be increased or decreased according to specific needs; wherein, as shown in FIG. 3 to FIG. As shown in FIG. 5, each of the wings 40 may be in the form of a sheet having a side edge 401 facing the rear end 22 of the hull 20.
  • the propeller 41 is disposed on the side edge 401, as shown in FIGS. 7-9.
  • the wing 40 can also be formed as a wheel body and has a rim portion 402 and a joint portion 403 connecting the rim portion 402 and the hull 20.
  • the propeller 41 is disposed in the rim portion 402.
  • the wing 40 of the surface winger of the present invention can control the deflection angle by rotational adjustment so that the bottom 23 of the hull 20 can fly at a predetermined height from the water surface.
  • the hull 20 is buoyed by the pontoon 30, so that the bottom 23 is slightly in contact with the wave of the water surface, and the buoyant portion 302 is completely under the water surface, and the connecting portion 301 is only
  • the joint of the hull 20 is located on or adjacent to the surface of the water.
  • the wings 40 extending from both sides of the hull 20 are substantially horizontal. After the pontoons 30 and the propellers 36 and 41 of the wing 40 are driven, the hull 20 can travel forward by the propellers 36 and 41 by the action of water and air.
  • the hull 20 can adjust the deflection angle of the wing 40 by rotation, thereby generating a force forcing the hull 20 to push up in the height direction, and adding a dynamic airflow to the bottom surface 23 of the hull 20 and the water flow surface, so that the bottom of the hull 20 23 Lift up and completely leave the water and fly stably in the air.
  • the present invention allows the pontoon 30 and the hull 20 to have only the connecting portion 32 connected by the structural arrangement of the pontoon 30 described above.
  • the wave will only come into contact with the connecting portion 301 of the pontoon 30, greatly reducing the contact area between the wave and the pontoon 30, thereby reducing the reaction force caused by the wave from both sides of the hull 20 on the pontoon 30, so that the hull 20 can be driven while traveling. More stable, to increase ride safety and comfort.
  • the form of the float 30 of the surface wing ship of the present invention is not limited to the form shown in Figs. 3 to 11, and may be in the form of the second to sixth embodiments shown in Figs. 10 to 15 .
  • a second embodiment of the pontoon 30 is illustrated.
  • the wafer-shaped buoyancy portion 302 of the pontoon 30 has a center P such that the connecting portion 301 extends perpendicularly toward the bottom 23 of the hull 20 along the center P.
  • Each of the pontoons 30 is placed upright on the bottom 23 of the hull 20, that is, the angle ⁇ 1 between the connecting portion 301 and the bottom portion 23 of the hull 20 is 90 degrees or 90 degrees.
  • a third embodiment of the pontoon 30 is illustrated.
  • the front side edge 33, the bottom edge 34 and the rear side edge 35 of each of the pontoons 30 are curved in cross section, and are connected at both ends of the curved shape.
  • the outer side surfaces 31, 32, and the front side edge 33 and the rear side edge 35 are correspondingly formed into a straight shape perpendicular to the bottom portion 23 of the hull 20, and the bottom edge 34 is formed into a circular arc shape. Reduce the resistance of the pontoon 30 in the water.
  • FIGS. 12 and 13 a fourth embodiment of the pontoon 30 is illustrated.
  • the front side edge 33, the bottom edge 34 and the rear side edge 35 of each of the pontoons 30 are curved in cross section and are connected at both ends of the curved shape.
  • the inner and outer sides 31, 32, and the front side edge 33 and the rear side edge 35 are correspondingly formed in a straight configuration perpendicular to the bottom 23 of the hull 20, the bottom edge 34 being from bottom to top from the front side edge 33 Tilting toward the rear side edge 35 in a flat oblique shape, and the inclination angle ⁇ 2 between the bottom edge 34 and the bottom portion 23 of the hull 20 is 10 degrees to 30 degrees and greater than 10 degrees and less than 30 degrees (10° ⁇ ⁇ 2 ⁇ 30°) ).
  • each of the pontoons 30 has a V-shaped cross section, and the bottom edge 34 and the rear side edge 35 have a curved cross section to connect the inner and outer portions.
  • the propeller 36 of each of the buoys 30 has a shaft portion 361, the rear side edge 35 of the buoy 30 is provided with a mounting seat 353, and the mounting seat 353 is disposed adjacent to the rear side edge 35. At the bottom edge 34, the shaft portion 361 of the propeller 36 is brought into contact with the mounting seat 353 in parallel with the bottom portion 23 of the hull 20.
  • first, second, and third embodiments of the surface crane of the present invention have a circular arc-shaped lower half by forming the bottom of the pontoon 30 into a round cake shape or a U-shaped shape.
  • the lower half of the circular arc is pushed upward by the action of the water flow.
  • the front and the rear are used in addition to the component of the front portion of the rounded corner.
  • the inclined structure makes the water flow downstream, and the speed of the hull 20 does not change. Affecting the change of the overall upward component, the height of the hull 20 will also be less changed, and when the hull 20 is shaken to change the angle, unless the (shaking) angle is greater than the oblique angle, the component will not change.
  • the present invention can achieve the above-mentioned various effects through the above-mentioned surface wing ship, and has already met the patent application requirements, and has filed a patent application according to law, praying for review and early granting of patents. .
  • Buoy device 13 first buoy 131

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Bridges Or Land Bridges (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
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Abstract

水面机翼船，其包括一船体（20）、设于该船体（20）相对两侧的偶数机翼（40）以及设于该船体（20）底部两侧的偶数浮筒（30），各该浮筒（30）成形为中空扁平形态，并于后侧缘设有一螺旋桨（36），通过船体（20）底部（23）的浮筒（30）结构，使来自船体（20）两侧的波浪主要打击在各该浮筒的连接部上，从而降低来自船体（20）两侧的波浪打击在浮筒（30）上所造成的反作用力，达到提高船体行驶稳定度和增加乘坐安全及舒适性的目的。

Description

水面机翼船 技术领域
本发明有关于一种水面机翼船，特别是指通过其浮筒结构而得以更平稳在水面上飞行的水面机翼船。
背景技术
按，水翼船(英语：Hydrofoil)是一种高速船，其船身底部有支架以安装水翼。当船的速度逐渐增加，水翼可提供浮力将船身抬离水面，形成所谓的水翼飞航或水翼航行，从而大幅减少水的阻力且增加航行速度。
如图1、图2所示，显示本案发明人先前提出的一种水面机翼船10，其包括一船体11，该船体11两侧设有数量对应的机翼12，各该机翼12后缘设有螺旋桨121，该船体11底部设有一浮筒装置13，该浮筒装置13具有多个长条形的第一浮筒131，各该第一浮筒131两端部设有螺旋桨135，并通过一沿该第一浮筒131延伸的片状连接部132与该船体11底部连接，该浮筒装置13于船体11两侧邻近底部处另设有二个第二浮筒133，各该第二浮筒133通过二弯曲状连结部134与该船体11连接，藉此，如图2所示，当已知水面机翼船10静止停舶在水面上时，该第一浮筒131完全没入水面下，而该第二浮筒133则与水面接触地浮于水面上，以使船体11浮于水面之上，且当已知水面机翼船10在水面上飞行时，使该第一浮筒131的连接部132与该第二浮筒133完全离开水面，而在空中作一稳定地飞行。
然而，已知水面机翼船10的浮筒装置13的浮筒皆为沿着船体11延伸的长条形结构，不论水面机翼船10在静止或行驶状态下，只要浪由船体11两侧打来，将大面积地打击在第一浮筒131或第二浮筒133上，容易造成船体11晃动偏移；尤其，相较于呈长条圆筒状而能够略使波浪分流的浮筒而言，在水面机翼船10快速行驶时，两侧打来的浪不仅打在第一浮筒131上，更将与该第一浮筒131的 片状连接部132打击接触，形成更明显撼动船体11的作用力。
是以，要控制水面机翼船10一直保持在水平状态的困难极高，而只能借着连接部132连接船体11，再配合机翼12达到保持在水平状态。然而，当机翼12接触到不稳定的气流时，将造成第一浮筒131随着水面机翼船10整体作向上或向下的移动，使第一浮筒131的周侧由平均受力改变为单一方向的面接触，在高速水流冲击后产生了不可预期的路径变化，尤其水的反作用力大于空气甚多，因此当速度愈快或改变角度愈大时，其产生的冲击将愈明显，终将使整个水面机翼船10快速地往上或往下冲越，导致航行不稳定的状态。
藉此，已知水面机翼船10在于如何提高行驶稳定度以增加乘坐安全及舒适性的课题上，仍有其进一步改善的空间。
发明内容
本发明的目的在于提供一种水面机翼船，其包括一船体、设于该船体相对两侧的偶数机翼以及设于该船体底部两侧的偶数浮筒，各该浮筒成形为中空扁平形态，并于后侧缘设有一螺旋桨，藉此，通过船体底部的浮筒结构设计，使来自船体两侧的波浪主要打击在各该浮筒的连接部上，从而降低来自船体两侧的波浪打击在浮筒上所造成的反作用力，达到提高船体行驶稳定度和增加乘坐安全及舒适性的目的。
缘是，为达上述目的，本发明所提供一种水面机翼船，包括：一船体，具有相对的一前端及一后端，该前、后端之间具有一底部连接；偶数个浮筒，成对地设于该船体底部，各该浮筒成形为中空扁平形态，具有对应该船体两侧的一内侧面及一外侧面，该内、外侧面之间具有一前侧缘、一底缘及一后侧缘连接，且各该浮筒后侧缘上设有一螺旋浆，以在水中作用产生推进力；以及偶数个机翼，成对地设于该船体相对两侧，各该机翼设有至少一螺旋桨，以在空气中作用产生推进力。
较佳的，本发明水面机翼船中，各该浮筒通过其前侧缘、底缘及后侧缘连接该内、外侧面，而界定一组设于该船体底部的连接部， 以及一自该连接扩张成形为圆饼形态的浮力部，该浮筒的圆饼形态浮力部具有一中心，该连接部沿该中心朝向船体底部延伸，且该连接部可直立地朝向该船体底部，或者朝向该船体后端倾斜设置以进一步降低该浮筒所产生的前进阻力。其中，该浮筒的螺旋桨具有一轴部，该浮筒后侧缘设有一安装座，且该安装座设在该后侧缘和一垂直于该船体底部的切线的相切处，以使该螺旋桨轴部平行于该船体底部地与该安装座组接，提供船体较佳的驱动动力效能。
较佳的，本发明水面机翼船中，该浮筒另可使其前、后侧缘成形为平直形态，且浮筒底缘成形由前向后朝向船体底部倾斜的平斜形态，通过调整该底缘与船体底部之间倾斜角度，达到调整降低浮筒在水中前进的阻力大小。进一步地，该浮筒的前侧缘截面可成形为V形，以利用其尖状前端使使水分流至浮筒两侧，达到再降低水中阻力的目的。
较佳的，本发明水面机翼船中，各该机翼可呈片状体或呈轮状体，且该机翼可通过旋转调整该组接部以控制偏转角度，令该船体底部距离水面预定高度进行飞行。
有关于本发明为达成上述目的，所采用的技术、手段及其他功效，兹举较佳可行实施例并配合图式详细说明如后。
附图说明书
图1是已知水面机翼船的立体结构示意图。
图2是已知水面机翼船在水面上静止时的前视结构示意图。
图3是本发明水面机翼船的立体结构示意图。
图4是本发明水面机翼船的侧视结构示意图。
图5是本发明水面机翼船在水面上静止时的前视结构示意图。
图6是本发明水面机翼船浮筒结构第一实施例的剖视示意图。
图7是本发明水面机翼船机翼另一实施例的立体结构示意图。
图8是本发明水面机翼船机翼另一实施例的侧视结构示意图。
图9是本发明水面机翼船机翼另一实施例在水面上静止时的前视结构示意图。
图10本发明水面机翼船浮筒结构第二实施例的剖视示意图。
图11本发明水面机翼船浮筒结构第三实施例的剖视示意图。
图12本发明水面机翼船浮筒结构第四实施例的剖视示意图。
图13本发明水面机翼船浮筒结构第五实施例的剖视示意图。
图14本发明水面机翼船浮筒结构第六实施例的立体外观示意图。
图15本发明水面机翼船浮筒结构第六实施例的剖视示意图。
具体实施方式
请配合参阅图3至图15所示，说明本发明水面机翼船的具体实施方式。
如图3至图9所示，本发明水面机翼船包括一船体20、设于该船体20底部23两侧的偶数浮筒30以及设于该船体20相对两侧的偶数机翼40，其中：
该船体20具有相对的一前端21及一后端22，该前、后端21、22之间具有一底部23连接；于本实施例中，该船体20可为预定形状，内部设有容纳乘坐或运输空间的形态，且该船体20底部23可在静止状态下与水面上的波浪少许接触，并于飞行时通过控制而距离一预定高度地完全离开水面。
该偶数个浮筒30是成对地设于该船体20底部21，本实施例设有四个浮筒30，各该浮筒30设有一螺旋桨36，但该浮筒30及该螺旋桨36的数量并不限于此，可视具体需求而增加或减少；其中，如图4至图6所示，各该浮筒30成形为中空扁平形态，且以其扁平周缘对应船体20前、后端21、22的方向设于船体20底部23，以在提供船体20所需浮力的同时，具有降低船体20前进阻力的功效，各该浮筒30具有对应该船体20两侧的一内侧面31及一外侧面32，该内、外侧面31、32之间具有一前侧缘33、一底缘34及一后侧缘35连接，且各该浮筒30后侧缘35上设有一螺旋浆36，以在水中作用产生推进力。
于本实施例中，各该浮筒30的前侧缘33、底缘34及后侧缘35 系截面呈弧形，并以弧形两端连接该内、外侧面31、32，该前侧缘33及该后侧缘35对应成形为一平直段331、351及一圆弧段332、352，该底缘34成形为圆弧形态并以圆弧两端与该二前、后侧缘33、35的圆弧段332、352连接，令该二平直段331、351与该内、外侧面31、32共同界定一连接部301组设于该船体20底部23，且该二圆弧段332、352、该底缘34与该内、外侧面31、32共同界定一圆饼形态的浮力部302，该螺旋浆36设于该后侧缘35的圆弧段352上；如图5所示，该浮筒30在静止状态时，其连接部301近乎全部位于水面下，当飞行时，该浮力部302位于水面下而该连接部301位于水面上。
此外，本发明浮筒30的螺旋桨36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35圆弧段352和一垂直于该船体20底部23的切线的相切处，令该螺旋桨36轴部361平行于该船体20底部23地与该安装座353组接。
又，如图4所示，该浮筒30的圆饼形态浮力部302具有一中心P，该连接部301沿该中心P朝向船体20底部23延伸，且该连接部301朝向该船体20后端22倾斜设置，定义该连接部301与该船体20底部23之间具有一夹角θ1，该夹角θ1介于40度至90度且小于90度大于40度(90°＜θ1＜40°)。
偶数个机翼40成对地设于该船体20相对两侧，各该机翼40设有至少一螺旋桨41，本发明实施例中，该水面机翼船是设有四个机翼40，各该机翼40设有二螺旋桨41，以在空气中作用产生推进力，但该机翼40及该螺旋桨41的数量并不限于此，可视具体需求而增加或减少；其中如图3至图5所示，各该机翼40可呈片状体而具有一朝向该船体20后端22的侧缘401该螺旋桨41设于该侧缘401上，又如图7至图9所示，各该机翼40亦可成形为轮状体而具有一轮圈部402及一连接该轮圈部402及该船体20的组接部403，该螺旋桨41设于该轮圈部402内，藉此，本发明水面机翼船的机翼40可通过旋转调整而控制偏转角度，使该船体20底部23距离水面预定高度进行飞行。
以上所述即为本发明实施例主要构件及其组态说明，至于本发明优选实施例的操作方式及其功效，请配合以图4配合参阅图5，做以下说明。
如图5所示，当本发明水面机翼船处于静止状态时，其船体20通过浮筒30浮力，而使底部23与水面波浪少许接触，呈现浮力部302完全位于水面下而连接部301只有与船体20连接处位于水面上或邻近水面。同时，自船体20两侧延伸的机翼40大致处于水平状态。在驱动浮筒30和机翼40的螺旋桨36、41后，船体20即可通过螺旋桨36、41与水、空气作用产生推进力而前进行驶。此时，船体20可以通过旋转调整机翼40的偏转角度，据以产生迫使船体20朝高度方向推升的力量，加上船体20底部23与水流表面目成的动态气流，使船体20底部23上抬而完全离开水面，在空中稳定地飞行。
藉此，本发明通过前述浮筒30的结构设置，使浮筒30和船体20之间仅具有连接部32连接，当本发明水面机翼船在飞行过程中，遇波浪从船体20侧边袭来时，波浪只会和该浮筒30连接部301打击接触，大幅降低波浪和浮筒30的接触面积，从而降低来自船体20两侧的波浪打击在浮筒30上所造成的反作用力，使船体20行驶时能更为稳定，达到增加乘坐安全及舒适性。
本发明水面机翼船的浮筒30形态并不限于图3至图11所示形态，亦可以为图10至图15所示的第二至六实施例形态。
如图10所示，说明该浮筒30的第二实施态样，该浮筒30的圆饼形态浮力部302具有一中心P，令该连接部301沿该中心P垂直地朝向船体20底部23延伸，使各该浮筒30直立地组设在船体20底部23，即连接部301与该船体20底部23夹角θ1为90度或接瑢90度的形态。
如图11所示，说明该浮筒30的第三实施态样，各该浮筒30的前侧缘33、底缘34及后侧缘35系截面呈弧形，并以弧形两端连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，通过使该底缘34成形为圆弧形态， 降低浮筒30在水中前行的阻力。
如图12、13所示，说明该浮筒30的第四实施态样，各该浮筒30的前侧缘33、底缘34及后侧缘35系截面呈弧形，并以弧形两端连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，该底缘34由下而上地从该前侧缘33朝向该后侧缘35倾斜呈平斜形态，且该底缘34与该船体20底部23之间的倾斜角度θ2为10度至30度且大于10度小于30度(10°＜θ2＜30°)。
如图14、15所示，说明该浮筒30的第六实施态样，各该浮筒30前侧缘33截面呈V形且底缘34及后侧缘35截面呈弧形以连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，该底缘34由下而上地从该前侧缘33朝向该后侧缘35倾斜呈平斜形态，该底缘34与该船体20底部23之间的倾斜角度θ2为10度至30度且大于10度小于30度(10°＜θ2＜30°)。
该第2至6实施例中，各该浮筒30的螺旋浆36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35邻近该底缘34处，令该螺旋浆36轴部361平行该船体20底部23地与该安装座353组接。
值得说明的是，本发明水面机翼船的第一、第二、第三实施例，透过将浮筒30底部成形为圆饼形态或U形形态而共同具有圆弧形下半部，当船体20开始前进而速度渐渐加快时，此时圆弧形的下半部受到水流的作用分力而向上推挤，在速度愈快或受力体积愈大或向上分力截面积愈大时，使整个水面机翼船往上提的力量就愈大，即船体20推向上的高度愈高时，透过该圆弧形结构达到分流作用，使船体20摇晃而使受力角度不同时，整体的受力仍旧是相同的，不会因整体受力的突然改变而使船体呈现不平稳的状态。
此外本发明水面机翼船的第四、第五、第六实施例，透过将浮筒30底部成形为倾斜底缘，除了前方圆角少部分的分力外，利用该由前下向后上倾斜的结构使水流顺流，则船体20的速度改变即不会 影响整体向上分力的改变，船体20的高度亦将少有改变，且当船体20受力摇晃而使角度改变时，除非(摇晃)角度大于斜向角度，否则分力也将不会改变，达到使船体20稳定航行的目的。
综上所述，本发明透过上述水面机翼船，确实可达到上述诸项功效，诚已符合专利申请要件，爰依法提出专利申请，祈请惠予审查并早日赐准专利，实感德便。
【符号说明】
(已知)
水面机翼船10          船体11
机翼12                螺旋桨121
浮筒装置13            第一浮筒131
连接部132             第二浮筒133
连结部134             螺旋桨135
(本发明)
船体20                前端21
后端22                底部23
浮筒30                内侧面31
外侧面32              前侧缘33
平直段331             圆弧段332
底缘34                后侧缘35
平直段351             圆弧段352
安装座353             螺旋浆36
轴部361
机翼40                侧缘401
轮圈部402             组接部403
螺旋桨41
夹角θ1            中心P
倾斜角度θ2

Claims (14)

  1. 一种水面机翼船，包括：
    一船体20，具有相对的一前端21及一后端22，该前、后端21、22之间具有一底部23连接；
    偶数个浮筒30，成对地设于该船体20底部23，各该浮筒30成形为中空扁平形态，具有对应该船体20两侧的一内侧面31及一外侧面32，该内、外侧面31、32之间具有一前侧缘33、一底缘34及一后侧缘35连接，且各该浮筒30后侧缘35上设有一螺旋浆36，以在水中作用产生推进力；偶数个机翼40，成对地设于该船体20相对两侧，各该机翼40设有至少一螺旋桨41，以在空气中作用产生推进力。
  2. 如权利要求1所述的水面机翼船，其特征在于，各该浮筒30的前侧缘33、底缘34及后侧缘35截面呈弧形以连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为一平直段331、351及一圆弧段332、352，该底缘34成形为圆弧形态，令该二个平直段331、351与该内、外侧面31、32共同界定一连接部301组设于该船体20底部23，且该二个圆弧段332、352、该底缘34与该内、外侧面31、32共同界定一圆饼形态的浮力部302，该螺旋浆36设于该后侧缘35的圆弧段352上。
  3. 如权利要求2所述的水面机翼船，其特征在于，该浮筒30的圆饼形态浮力部302具有一中心P，该连接部301沿该中心P朝向船体20底部23延伸，且该连接部301朝向该船体20后端22倾斜设置，定义该连接部301与该船体20底部23之间具有一夹角θ1，该夹角θ1介于90度至40度(90°＜θ＜40°)。
  4. 如权利要求2所述的水面机翼船，其特征在于，该浮筒30的圆饼形态浮力部302具有一中心P，令该连接部301沿该中心P 垂直地朝向船体20底部23延伸。
  5. 如权利要求2所述的水面机翼船，其特征在于，该浮筒30的螺旋桨36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35圆弧段352和一垂直于该船体20底部23的切线的相切处，令该螺旋桨36轴部361平行于该船体20底部23地与该安装座353组接。
  6. 如权利要求1所述的水面机翼船，其特征在于，各该浮筒30的前侧缘33、底缘34及后侧缘35截面呈弧形以连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，该底缘34成形为圆弧形态。
  7. 如权利要求1所述的水面机翼船，其特征在于，各该浮筒30的前侧缘33、底缘34及后侧缘35截面呈弧形以连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，该底缘34由下而上地从该前侧缘33朝向该后侧缘35倾斜呈平斜形态，且该底缘34与该船体20底部23之间的倾斜角度θ2为10度至30度。
  8. 如权利要求1所述的水面机翼船，其特征在于，各该浮筒30的前侧缘33截面呈V形且底缘34及后侧缘35截面呈弧形以连接该内、外侧面31、32，且该前侧缘33及该后侧缘35对应成形为垂直于船体20底部23的平直形态，该底缘34由下而上地从该前侧缘33朝向该后侧缘35倾斜呈平斜形态，该底缘34与该船体20底部23之间的倾斜角度为10度至30度。
  9. 如权利要求6所述的水面机翼船，其特征在于，各该浮筒30的螺旋浆36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35邻近该底缘34处，令该螺旋浆36 轴部361平行该船体20底部23地与该安装座353组接。
  10. 如权利要求7所述的水面机翼船，其特征在于，各该浮筒30的螺旋浆36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35邻近该底缘34处，令该螺旋浆36轴部361平行该船体20底部23地与该安装座353组接。
  11. 如权利要求8所述的水面机翼船，其特征在于，各该浮筒30的螺旋浆36具有一轴部361，该浮筒30后侧缘35设有一安装座353，且该安装座353设在该后侧缘35邻近该底缘34处，令该螺旋浆36轴部361平行该船体20底部23地与该安装座353组接。
  12. 如权利要求1所述的水面机翼船，其特征在于，各该机翼40呈片状体而具有一朝向该船体20后端22的侧缘401，该螺旋桨41设于该侧缘401上，且该机翼40旋转调整而控制偏转角度，令该船体20底部23距离水面预定高度进行飞行。
  13. 如权利要求1所述的水面机翼船，其特征在于，各该机翼40成形为轮状体而具有一轮圈部402及一连接该轮圈部402及该船体20的组接部403，该螺旋桨41设于该轮圈部402内，且该机翼40通过旋转调整该组接部403以控制偏转角度，令该船体20底部23距离水面预定高度进行飞行。
  14. 如权利要求1所述的水面机翼船，其特征在于，该船体20底部23设有四该浮筒30，该四浮筒30成对地分设于该船体20底部23邻近前端21及后端22处，且该船体20两侧设有四该机翼40，该四机翼40成对地分设于该船体20两侧邻近前端21及后端22处。
PCT/CN2015/092292 2014-10-24 2015-10-20 水面机翼船 Ceased WO2016062238A1 (zh)

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