CN103786883A - Controlled kite and flying method thereof - Google Patents
Controlled kite and flying method thereof Download PDFInfo
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- CN103786883A CN103786883A CN201410059654.1A CN201410059654A CN103786883A CN 103786883 A CN103786883 A CN 103786883A CN 201410059654 A CN201410059654 A CN 201410059654A CN 103786883 A CN103786883 A CN 103786883A
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Abstract
The invention relates to an unpowered manned craft, discloses a kite in which a kite pilot can ride, short for a controlled kite, and simultaneously discloses a flying method of the controlled kite. The controlled kite consists of an upper lifting surface and a lower lifting surface, wherein the lower lifting surface adopts a manner of an arc-shaped curved surface with a depressed middle part and two upwarping ends, and is distributed bisymmetrically, the wingtip parts of two ends of the upper lifting surface and the lower lifting surface are closely overlapped or connected with each other, a lifeboat, an inflatable seat, a gravity center regulating device, an inflation protection column and a driven beam driving device are arranged below the middle part of the lower lifting surface, the lower end of an upper hoisting line is connected with a traction line system through a lifting hook, the traction system has the following three modes: an iron anchor traction line device, an umbrella anchor traction line device, and an unmanned ship traction line device, and can be randomly switched to be in a traction state or a gliding state. The invention aims at creating a new sports item, and the manned kite can freely glide and distantly fly. The controlled kite has the advantages that the ground control on the kite is changed to air control, so that the ancient kite sports are more colorful.
Description
Technical field
The present invention relates to a kind of unpowered manned craft, there is the feature of obvious kite.
Background technology
People of all times a lot of are transshipped research and the exploration that people's kite flies to sky, ancient books is recorded, before more than 2500 year, kite contriver is public " tastes again for wooden kite as defeated, take advantage of to peep Sung Dynasty Village ", the Bao Weier of Baden in 1894 utilizes manned successfully first European of kite, summer in 2003, the kite fan in Weifang has comparatively intactly carried out a kite heavy burden test, the in the situation that of 3 grade half of wind-force, use the kite of long 70 meters that the load of 45 kilograms is raise to more than 20 meter, within 2010, Guangdong Chen Wang pine utilizes string data kite that the personnel of 60 kilograms of body weight are served to sky.Also do not have up to now the manned sports of kite generally to carry out, personnel rest on test session by flight of kites, and do not drive the action of kite, and kite relies on ground staff by draught line control completely; The relevant kite manned craft that Chinese patent " fixed drawing wind power flying vehicle (application number 90108736.X) " is announced, this manned craft can only, along the walking of kite draught line, can not initiatively be driven kite.
Summary of the invention
The present invention be directed to the deficiencies in the prior art, create a kind of that can initiatively drive, even long-time long-distance flight of can freely gliding, can take flight of kites person's kite, be called for short imperial kite, announce the flying method of imperial kite simultaneously.
The technical solution adopted in the present invention is: imperial kite has upper and lower two-layer lifting surface, upper strata lifting surface adopts the lifting surface of one section of continuous epirelief arc curve form, in the middle of lower lifting surface adopts, recessed two ends upwarp arc curve form, be symmetrically arranged, V-shaped wing structure, there is the larger dihedral angle, make imperial kite there is good roll stability, imperial kite adopts main gasbag and an air bag support lifting surface thereof to keep fixing outer shape, its cross-sectional plane presents Airfoil Sections shape, raising force face, lower lifting surface is in the closely overlapping or connection of the wing tip position at its two ends, four wing tips have become two wing tips, reduce induced drag, lower lifting surface middle part arranges a life boat below, to guarantee flight of kites person's safety, in the cabin of life boat for flight of kites person arranges a pneumatic seat, pneumatic seat is a set of gravity adjusting device also, a window is opened to pneumatic seat is installed in the middle part of lower lifting surface, the both sides of window and pneumatic seat, life boat connects, a gas-filled protective post is erect at life boat cabin rear portion, avoid flight of kites person to be subject to unexpected compressing, for flight of kites person's the imperial kite of safety is let fly away across the sea and flies, imperial kite also drive that beam is driven device or device is driven in accelerator wire deceleration bracing wire, flight of kites person drives device or accelerator wire deceleration bracing wire and drives the imperial kite of device control and carry out various flare maneuvers by driving beam, on carry the leading edge middle part that is connected in raising force face after the bifurcated of line upper end, on carry line lower end and be connected with draught line system by suspension hook, draught line system has following three kinds of forms: anchor pull wire arrangement, umbrella anchor pull wire arrangement, unmanned boat pull wire arrangement, imperial kite is at the flying method of anchor pull wire arrangement traction, the flying method of umbrella anchor pull wire arrangement traction, between the flying method of unmanned boat pull wire arrangement traction, switch arbitrarily, among above-mentioned three kinds of flying methods, also have two kinds of state of flights: traction state and glide state, and can between this two states, switch arbitrarily, while being switched to glide state, imperial kite freely glides, while being switched to traction state, imperial kite takes off or increases flying height.
Gravity adjusting device, air bag back cushion is placed on before the backrest of pneumatic seat, air bag pier be arranged on pneumatic seat before, air bag back cushion, air bag pier have multilayer air bag independently mutually, when these air bags are all full of air, flight of kites person's center of gravity is to reach, these air bags are whole when emptying, flight of kites person's center of gravity is moved backward, flight of kites person's center-of-gravity position depends on that air bag back cushion, air bag pier are full of the quantity of air bag, and the center-of-gravity position of flight of kites person's center-of-gravity position and imperial kite is very approaching.
Drive beam and drive device, comprise that the right side drives beam, beam and corresponding front and back end bracing wire thereof are driven in a left side, middle part bracing wire, beam is driven on the right side, the bracing wire upper end, front and back end that beam is driven on a left side is connected to the leading edge that raising force face is corresponding, trailing edge, bracing wire lower end, middle part is connected to life boat, pneumatic seat, drive beam and be bending, two ends upwarp, article two, above middle part bracing wire and life boat ship side composition triangle, be conducive to increase the pitching stability of imperial kite, pull up and down the right side to drive beam, the front end of beam is driven on a left side, can change the angle of attack of raising force face, flight of kites person drives the imperial kite of device control and carries out various sporting flyings by driving beam.
Device is driven in accelerator wire deceleration bracing wire, similar with the umbrella rope system of common parafoil, difference is that the lower end of accelerator wire deceleration bracing wire increases the bracing wire of several sections shorter, form stable triangle, make imperial kite have good pitching stability, flight of kites person carries out various sporting flyings by pulling accelerator wire deceleration bracing wire to drive the imperial kite of device control.
Anchor pull wire arrangement, comprise anchor, spike thing, helium balloon, anchor draught line, the lower end of draught line connects anchor and is anchored in seabed by anchor, draught line upper end connects helium balloon, helium balloon has buoyancy to drive draught line upper end to swim in the air in air, draught line tail end arranges draught line tail ring, the above anchor pull wire arrangement of two covers is set on sea, anchor draught line tail ring and suspension hook can be connected together by hook connecting, also can decoupling device disconnected from each other, when anchor draught line tail ring and suspension hook are connected together by hook connecting, imperial kite takes off or increases flying height under wind-force effect, anchor draught line tail ring is when decoupling device separates with suspension hook, imperial kite departs from the traction of anchor pull wire arrangement, be switched to glide state, now imperial kite freely glides, flying height reduces gradually, when imperial kite drops to the height of regulation, flight of kites person drives device and drives imperial kite and go to find other a set of anchor pull wire arrangement by driving beam, and anchor draught line tail ring and suspension hook are linked together, now imperial kite increases flying height under the traction of anchor pull wire arrangement and the effect of wind-force, by moving in circles above, imperial kite is realized long-time long distance and is glided.
Umbrella anchor pull wire arrangement, umbrella anchor pull wire arrangement comprises umbrella anchor, umbrella anchor draught line, turn to sister block, umbrella anchor exhausting line, umbrella anchor fixed orifice, umbrella anchor reel, handle, the lower end of umbrella anchor draught line is connected in umbrella anchor, turn to sister block to hang on and carry in the suspension hook of line lower end, umbrella anchor exhausting line, the upper end of umbrella anchor draught line is fixed in the set umbrella anchor fixed orifice of umbrella anchor reel, the equal in length or approaching of the length of umbrella anchor exhausting line and umbrella anchor draught line equates, umbrella anchor exhausting line, the upper part of umbrella anchor draught line is wrapped in umbrella anchor reel, its winding direction is contrary each other, being wound around the length of part and the total length of umbrella anchor equates or approaches to equate, while clockwise rotating umbrella anchor reel, umbrella anchor draught line tightens up, umbrella anchor exhausting line loosens, now umbrella anchor opens and is anchored in sea, while rotating counterclockwise umbrella anchor reel, umbrella anchor draught line loosens, umbrella anchor exhausting line tightens up, and now umbrella anchor closes up contraction, while continuing to rotate counterclockwise umbrella anchor reel, umbrella anchor draught line, umbrella anchor exhausting line equidirectional being wrapped in umbrella anchor reel simultaneously, until umbrella anchor is recovered in life boat, turn to sister block that umbrella anchor exhausting line, umbrella anchor draught line are turned to direction, umbrella anchor reel is arranged on the fore of life boat.
Unmanned boat (unpiloted ship abbreviation unmanned boat) pull wire arrangement, driving kite with the traction of unmanned boat pull wire arrangement takes off or increases flying height, unmanned boat draught line upper end connects little dirigible, little dirigible drives draught line upper end to swim in the air, unmanned boat draught line upper end afterbody arranges a tail ring, unmanned boat draught line lower end is connected to unmanned boat, when unmanned boat draught line tail ring and suspension hook are hooked together, imperial kite drags and under produced airflow function, takes off or increase flying height at unmanned boat, when unmanned boat draught line tail ring separates with suspension hook decoupling device, imperial kite freely glides, imperial flight of kites height reduces gradually simultaneously, when imperial kite drops to the height of regulation, flight of kites person by drive fine strain of millet device drive imperial kite near and catch the upper end of unmanned boat draught line, unmanned boat draught line tail ring and suspension hook are linked together, imperial kite drags under produced airflow function and increases flying height at unmanned boat, unmanned boat adopts the simplest mode, at circular ship of sea anchoring, the ship side of unmanned boat connects horizontal hawser, the other end of horizontal hawser is connected to circular ship, and unmanned boat, take the length of horizontal hawser as radius, moves in a circle as the center of circle take circular ship, if there are many unmanned boats to navigate by water simultaneously, with connection cable, by adjacent unmanned boat connection, to guarantee safety of navigation, imperial kite also can take off on unmanned boat.
Imperial flight of kites method: imperial kite has six kinds of flying methods, state: the traction state of (one) anchor pull wire arrangement, (2) the glide state of disengaging anchor pull wire arrangement, (3) traction state of umbrella anchor pull wire arrangement, (4) the glide state of disengaging umbrella anchor pull wire arrangement, (5) traction state of unmanned boat pull wire arrangement, (6) the glide state of disengaging unmanned boat pull wire arrangement, above-mentioned six kinds of flying methods, between state, can switch mutually, its changing method step is as follows: 1. the flying method of anchor pull wire arrangement traction is switched to the method step of the flying method of umbrella anchor pull wire arrangement traction, when traction state at imperial kite in anchor pull wire arrangement and imperial kite reach higher height, flight of kites person is by the decoupling device from suspension hook of anchor draught line tail ring, anchor pull wire arrangement separates completely with suspension hook, imperial kite departs from the traction of anchor pull wire arrangement, freely glide, then flight of kites person receives the upper end hook connecting that turns to sister block in suspension hook, umbrella anchor pull wire arrangement is connected with suspension hook, clockwise rotate umbrella anchor reel and emit umbrella anchor, umbrella anchor is anchored in sea, imperial kite is switched to the traction state of umbrella anchor pull wire arrangement, increase flying height, 2. the flying method of umbrella anchor pull wire arrangement traction is switched to the method step of the flying method of unmanned boat pull wire arrangement traction, rotate counterclockwise umbrella anchor reel, recorery parachute anchor is in life boat cabin, upper end decoupling device from suspension hook of sister block will be turned to, umbrella anchor pull wire arrangement separates completely with suspension hook, now imperial kite departs from the traction of umbrella anchor pull wire arrangement, freely glide, then flight of kites person drives device and controls imperial kite near unmanned boat draught line tail ring by driving beam, catch unmanned boat draught line tail ring, and unmanned boat draught line tail ring hook connecting is received in suspension hook, now imperial kite is switched to the flying method of unmanned boat pull wire arrangement traction, imperial kite increases flying height, 3. the flying method of unmanned boat pull wire arrangement traction is switched to the method step of the flying method of anchor pull wire arrangement traction, flight of kites person is by the decoupling device from suspension hook of unmanned boat draught line tail ring, unmanned boat pull wire arrangement separates completely with suspension hook, imperial kite departs from the traction of unmanned boat pull wire arrangement, freely glide, then flight of kites person drives device and controls imperial kite near anchor draught line tail ring by driving beam, catch anchor draught line tail ring, and anchor draught line tail ring hook connecting is received in suspension hook, now imperial kite is switched to the flying method of anchor pull wire arrangement traction, imperial kite increases flying height.
The object of the invention is: start a kind of new sports item, make ancient kite motion increase new content, improve kite sports level; The manned Long-term Free of realizing of kite glides and long-distance flight.
Order advantage of the present invention: the control of kite is transferred in the air by ground, imperial kite is at the flying method of anchor pull wire arrangement traction, the flying method of umbrella anchor pull wire arrangement traction, between the flying method of unmanned boat pull wire arrangement traction, switch arbitrarily, wherein in each flying method, also comprise the two kinds of state of flights that can switch: glide state and traction state, being switched to the imperial kite of glide state freely glides, be switched to the imperial kite of traction state and increase flying height, the even long-distance flight of can Long-term Free gliding of imperial kite, make ancient kite motion more rich and varied.
Accompanying drawing explanation
Accompanying drawing 1 is imperial kite overall plan schematic diagram;
Accompanying drawing 2 is imperial kite structural representation, in figure, the direction shown in arrow F is the front end of imperial kite, direction shown in arrow K is the right side of imperial kite, and the figure in figure in long and two-short dash line circle is partial enlarged drawing, and the figure in rectangular broken line frame is draught line system schematic;
Accompanying drawing 3 is for gravity adjusting device and drive beam and drive device schematic diagram, and the figure in figure in long and two-short dash line circle is partial enlarged drawing, and the direction shown in arrow F is the front end of imperial kite, and the direction shown in arrow K is the right side of imperial kite;
Accompanying drawing 4 is driven device schematic diagram for accelerator wire deceleration bracing wire, and in figure, the direction shown in arrow F is the front end of imperial kite, and the direction shown in arrow K is the right side of imperial kite;
Accompanying drawing 5 is the cutaway view of accompanying drawing 4 along A-A direction;
Accompanying drawing 6 is anchor pull wire arrangement schematic diagram, and the figure in long and two-short dash line circle is partial enlarged drawing;
Accompanying drawing 7 is umbrella anchor pull wire arrangement schematic diagram, and the figure in long and two-short dash line circle is partial enlarged drawing;
Accompanying drawing 8 is umbrella anchor in reclaiming view, and the figure in long and two-short dash line circle is partial enlarged drawing;
Accompanying drawing 9 is unmanned boat pull wire arrangement schematic diagram, and the figure in long and two-short dash line circle is partial enlarged drawing;
In accompanying drawing, 100-raising force face, 101-upper main gasbag and an air bag thereof, 102-lower lifting surface, 104-lower main gasbag and an air bag thereof, the bracing wire of 105-bottom right, the bracing wire of 106-lower-left, 107-life boat, 108-gas-filled protective post, 109-above carry line, 110-under carry line, 111-draught line system, 200-pneumatic seat, 301-air bag back cushion, 302-air bag pier, beam is driven on 400-right side, beam is driven on 401-left side, the bracing wire of 402-right rear end, the bracing wire of 403-right front ends, 404-left back end bracing wire, 405-left front end bracing wire, 406-right bracing wire, 407-left bracing wire, 500-right accelerator wire, 501-right deceleration bracing wire, 502-left accelerator wire, 503-left deceleration bracing wire, 504-left back upper line, 505-left horizontal line, 506-left back oblique line, 507-left rear line, 508-LAO line, 509-left front line, 510-right back upper line, 511-right horizontal line, 512-right back oblique line, 513-right rear line, 514-right front oblique line, 515-right front line, 600-suspension hook, 700-anchor, 701-spike thing, 702-helium balloon, 703-anchor draught line, 704-anchor draught line tail ring, 800-umbrella anchor, 801-umbrella anchor draught line, 802-turn to sister block, 804-umbrella anchor exhausting line, 805-umbrella anchor fixed orifice, 806-umbrella anchor reel, 807-handle, 808-arc arrow, 900-unmanned boat, 901-circular ship, 902-horizontal hawser, 903-connection cable, 904-circular trace, 905-unmanned boat draught line, 906-little dirigible, 907-unmanned boat draught line tail ring.
The specific embodiment
Embodiment 1, as shown in accompanying drawing 1～accompanying drawing 9, imperial kite comprises: raising force face 100, upper main gasbag and an air bag 101 thereof, lower lifting surface 102, lower main gasbag and an air bag 104 thereof, bottom right bracing wire 105, lower-left bracing wire 106, life boat 107, gas-filled protective post 108, on carry line 109, under carry line 110, pneumatic seat 200, gravity adjusting device (comprises air bag back cushion 301, air bag pier 302), drive beam and drive device and (comprise that the right side drives beam 400, beam 401 is driven on a left side, right rear end bracing wire 402, right front ends bracing wire 403, left back end bracing wire 404, left front end bracing wire 405, right bracing wire 406, left bracing wire 407) or accelerator wire deceleration bracing wire drive device and (comprise right accelerator wire 500, right deceleration bracing wire 501, left accelerator wire 502, left deceleration bracing wire 503, left back upper line 504, left horizontal line 505, left back oblique line 506, left rear line 507, LAO line 508, left front line 509, right back upper line 510, right horizontal line 511, right back oblique line 512, right rear line 513, right front oblique line 514, right front line 515), suspension hook 600, draught line system 111, draught line system 111 has following three kinds of forms: anchor pull wire arrangement (comprises anchor 700, spike thing 701, helium balloon 702, anchor draught line 703, anchor draught line tail ring 704), umbrella anchor pull wire arrangement (comprises umbrella anchor 800, umbrella anchor draught line 801, turn to sister block 802, umbrella anchor exhausting line 804, umbrella anchor fixed orifice 805, umbrella anchor reel 806, handle 807, umbrella anchor draught line 801), unmanned boat pull wire arrangement (comprises unmanned boat 900, circular ship 901, horizontal hawser 902, connection cable 903, unmanned boat draught line 905, little dirigible 906, unmanned boat draught line tail ring 907).
Imperial kite arranges upper and lower two-layer lifting surface, the two ends of raising force face 100 are overlapping with the two ends of lower lifting surface 102 or be connected respectively, four wing tips have become two wing tips, reduce induced drag, raising force face 100 arranges main gasbag and an air bag 101 thereof, in the middle of lower lifting surface 102 adopts, recessed two ends upwarp arc curve form, be symmetrically arranged, V-shaped wing structure, there is the larger dihedral angle, make imperial kite there is good roll stability, lower lifting surface 102 arranges lower main gasbag and an air bag 104 thereof, the upper and lower lifting surface of imperial kite adopts air sac supporting structure to keep fixing outer shape, its cross-sectional plane presents Airfoil Sections shape, lower lifting surface 102, below lower main gasbag and an air bag 104 thereof, a life boat 107 is set, to guarantee flight of kites person's safety, the cabin middle part of life boat 107 arranges a pneumatic seat 200 for flight of kites person, pneumatic seat 200 is a set of by air bag back cushion 301, the gravity adjusting device that air bag pier 302 forms, bracing wire 105 right-hand members in bottom right are connected in the leading edge right side of lower lifting surface 102, bracing wire 105 left ends in bottom right are connected with the fore right side of life boat 107, the left end of lower-left bracing wire 106 is connected in the leading edge left side of lower lifting surface 102, the right-hand member of lower-left bracing wire 106 is connected with the fore of life boat left side, the effect of these two bracing wires is that the lower lifting surface 102 of restriction is undue bending under wind-force effect, a window is opened to pneumatic seat 200 is installed in the middle part of lower lifting surface 102, and be connected with pneumatic seat 200, a gas-filled protective post 108 is erect at life boat 107 cabin rear portions, avoids flight of kites person to be subject to unexpected compressing, and the cross section of gas-filled protective post 108 is stream line pattern to alleviate air resistance, on carry the leading edge middle part that is connected in raising force face 100 after line 109 upper end bifurcateds, on carry line 109 lower ends and be connected in the upper end of suspension hook 600, under carry line 110 front ends and be connected in the upper end of suspension hook 600, under carry line 110 rear ends and be connected in the middle part of lower lifting surface front end or controlled by flight of kites person, suspension hook 600 is by anchor draught line tail ring 704 or turn to sister block 802 or unmanned boat draught line tail ring 907 is connected with draught line system 111, and draught line system 111 has following three kinds of forms: anchor pull wire arrangement, umbrella anchor pull wire arrangement, unmanned boat pull wire arrangement.
Gravity adjusting device comprises: air bag back cushion 301, air bag pier 302, referring to accompanying drawing 3, air bag back cushion 301 is placed on before the backrest of pneumatic seat 200, air bag pier 302 be arranged on pneumatic seat 200 before, air bag back cushion 301, air bag pier 302 has multilayer air bag independently mutually, when these air bags are all full of air, center of gravity when flight of kites person is sitting in pneumatic seat 200 is to reach, these air bags are whole when emptying, flight of kites person's center of gravity is moved backward, flight of kites person's center-of-gravity position depends on air bag back cushion 301, air bag pier 302 is full of the quantity of air bag, the center-of-gravity position of flight of kites person's center-of-gravity position and imperial kite is very approaching.
Drive beam and drive device, referring to accompanying drawing 3, comprising: beam 400 is driven on the right side, beam 401, right rear end bracing wire 402, right front ends bracing wire 403, left back end bracing wire 404, left front end bracing wire 405, right bracing wire 406, left bracing wire 407 are driven in a left side, the rear end that beam 400 is driven on the right side is connected with the trailing edge right side of raising force face 100 by right rear end bracing wire 402, the lower end of right front ends bracing wire 403 is connected to the right side and drives the M point of 1/4th distances of its total length of front end indentation of beam 400, the upper end of right front ends bracing wire 403 is connected with the leading edge right side of raising force face 100, the middle part of beam 400 is driven by right bracing wire 406 and pneumatic seat 200 in the right side, life boat 107 right sides connect, pneumatic seat 200 is fixed in life boat 107 cabins, the rear end that beam 401 is driven on a left side is connected with the trailing edge left side of raising force face 100 by left back end bracing wire 404, the lower end of left front end bracing wire 405 is connected to a left side and drives the N point of 1/4th distances of its total length of front end indentation of beam 401, the upper end of left front end bracing wire 405 is connected with the leading edge left side of raising force face 100, the middle part of beam 401 is driven by left bracing wire 407 and pneumatic seat 200 in a left side, life boat 107 left sides connect, beam 400 is driven on the right side, a left side is driven beam 401 and is bending, make imperial kite there is good pitching stability, flight of kites person drives the front end of beam 401 and drives imperial kite and do various sporting flyings by pulling the right side to drive beam 400, a left side, when flight of kites person upwards pulls the right side to drive the front end of beam 400, the right side trailing edge of raising force face 100 declines, right side leading edge rises, right side resistance increment, imperial kite turning flight to the right, when flight of kites person upwards pulls a left side to drive the front end of beam 401, the left side trailing edge of raising force face 100 declines, and left side leading edge rises, left side resistance increment, imperial kite turning flight to the left.
Anchor pull wire arrangement, comprise anchor 700, spike thing 701, helium balloon 702, anchor draught line 703, as shown in Figure 6, the lower end of anchor draught line 703 is connected in anchor 700 and is anchored at seabed, anchor draught line 703 upper ends connect helium balloon 702 at about 5% place from afterbody, helium balloon has buoyancy to drive anchor draught line upper end to swim in the air in air, anchor draught line 703 tail ends arrange anchor draught line tail ring 704, the anchor draught line afterbody spike thing 701 of tying up, so that increasing target is convenient to observe, the above anchor pull wire arrangement of two covers is set on sea, anchor draught line tail ring 704 and suspension hook 600 can be connected together by hook connecting, also can decoupling device disconnected from each other, when anchor draught line tail ring 704 and suspension hook 600 hook connectings are connected together, imperial kite takes off or increases flying height under wind-force effect, anchor draught line tail ring 704 is when 600 decoupling devices separate with suspension hook, imperial kite departs from the traction of anchor pull wire arrangement, be switched to glide state, now imperial kite freely glides, flying height reduces gradually simultaneously, when imperial flight of kites height is reduced to the height of regulation, flight of kites person drives imperial kite and goes to find another set of anchor pull wire arrangement, near and catch anchor draught line 703, anchor draught line tail ring 704 and suspension hook 600 hook connectings are connected together, now imperial kite increases flying height under the traction of anchor pull wire arrangement and the effect of wind-force, by moving in circles above, imperial kite is realized Long-term Free and is glided.
Anchor pull wire arrangement, unmanned boat pull wire arrangement are arranged in sea simultaneously, and umbrella anchor pull wire arrangement is standing in the life boat of imperial kite, so that imperial kite is switched to different flying methods, state.
Embodiment 2, as shown in accompanying drawing 4, accompanying drawing 5, accelerator wire deceleration bracing wire is driven device and is comprised: left back upper line 118, left horizontal line 119, left back oblique line 120, left rear line 121, LAO line 122, left front line 123, left accelerator wire 124, left deceleration bracing wire 125, right back upper line 126, right horizontal line 127, right back oblique line 128, right rear line 129, right front oblique line 130, right front line 131, right accelerator wire 132, right deceleration bracing wire 133, the upper end of left back upper line 118 is connected in the trailing edge left side of raising force face 100, its lower end and left horizontal line 119, left back oblique line 120, left rear line 121 is connected in 1 B, the upper end of left accelerator wire 124 is connected in the leading edge left side of raising force face 100, its lower end and left horizontal line 119, left front line 123, LAO line 122 is connected in 1 C, left rear line 121, the lower end of left front line 123 is connected in lower-left lifting surface and props up 1 D of air bag middle front part, the lower end of LAO line 122 is connected in lower-left lifting surface and props up air bag postmedian, the lower end of LAO line 122 is connected in lower-left lifting surface and props up air bag front end, left horizontal line 119, left rear line 121, left front line 123 forms stable triangle, make imperial kite there is good pitching stability, the upper end of right back upper line 126 is connected in the trailing edge right side of raising force face 100, its lower end and right horizontal line 127, right back oblique line 128, right rear line 129 is connected in 1 E, the upper end of right accelerator wire 132 is connected in the leading edge right side of raising force face 100, its lower end and right horizontal line 127, right back oblique line 128, right rear line 129 is connected in 1 E, the upper end of right accelerator wire 132 is connected in the leading edge right side of raising force face 100, its lower end and right horizontal line 127, right front line 131, right front oblique line 130 is connected in 1 H, right rear line 129, the lower end of left front line 131 is connected in bottom right lifting surface and props up air bag middle front part G point, connection bottom right, the lower end lifting surface of right back oblique line 128 props up air bag postmedian, the lower end of right front oblique line 130 is connected in bottom right lifting surface and props up air bag front end, right horizontal line 127, right rear line 129, right front line 131 forms stable triangle, make imperial kite there is good pitching stability.
Embodiment 3, as shown in accompanying drawing 7 Fig. 8, umbrella anchor pull wire arrangement, comprise umbrella anchor 800, umbrella anchor draught line 801, turn to sister block 802, umbrella anchor exhausting line 804, umbrella anchor fixed orifice 805, umbrella anchor reel 806, handle 807, the lower end of umbrella anchor draught line 801 is connected in umbrella anchor 800, and be anchored in sea by umbrella anchor 800, turn to sister block 802 to hang on and carry in the suspension hook 600 of line 109 lower ends, on carry line 109, the tractive force of umbrella anchor draught line 801 is transferred to raising force face 100 leading edge middle parts by suspension hook 600, umbrella anchor exhausting line 804, the upper end of umbrella anchor draught line 801 is fixed in the set umbrella anchor fixed orifice 805 of umbrella anchor reel 806, the equal in length or approaching of the length of umbrella anchor exhausting line 804 and umbrella anchor draught line 801 equates, umbrella anchor exhausting line 804, the upper part of umbrella anchor draught line 801 is wrapped in umbrella anchor reel 806, its winding direction is contrary each other, being wound around the length of part and the total length of umbrella anchor equates or approaches to equate, when cw (direction shown in arc arrow 808) Rotatable umbrella anchor reel 806, umbrella anchor draught line 801 tightens up, umbrella anchor exhausting line 804 loosens, umbrella anchor 800 opens, when conter clockwise (reversing sense shown in arc arrow 808) Rotatable umbrella anchor reel 806, umbrella anchor draught line 801 loosens, umbrella anchor exhausting line 804 tightens up, umbrella anchor 800 shrinks and closes up, turn to sister block 802 by umbrella anchor exhausting line 804, umbrella anchor draught line 801 is turned direction, umbrella anchor reel 806 is arranged on the fore of life boat 107, the recovery speed of umbrella anchor 800 is greater than the gliding speed of imperial kite, umbrella anchor reel 806 can adopt driven by power, recorery parachute anchor method and emit umbrella anchor method referring to embodiment 5.
Embodiment 4, as shown in Figure 9, unmanned boat pull wire arrangement, comprise unmanned boat 900, circular ship 901, horizontal hawser 902, connection cable 903, unmanned boat draught line 905, little dirigible 906, unmanned boat draught line tail ring 907, driving kite with the traction of unmanned boat pull wire arrangement takes off or increases flying height, unmanned boat draught line 905 upper ends connect little dirigible 906 at about 5% place of afterbody, little dirigible 906 drives unmanned boat draught line 905 upper ends, unmanned boat draught line tail ring 907 swims in the air, on carry line 109 lower end connecting shackles 600, when unmanned boat draught line tail ring 907 is connected together with suspension hook 600 hook connectings, imperial kite drags and under produced airflow function, takes off or increase flying height at unmanned boat, when unmanned boat draught line tail ring 907 separates with suspension hook 600 decoupling devices, imperial kite freely glides, now imperial flight of kites height reduces gradually, when imperial kite drops to the height of regulation, flight of kites person by drive beam drive device drive imperial kite near and catch the upper end of unmanned boat draught line 905, unmanned boat draught line tail ring 907 and suspension hook 600 hook connectings are connected together, imperial kite drags under produced airflow function and increases flying height at unmanned boat, unmanned boat 600 adopts the simplest mode, at circular ship 901 of sea anchoring, the ship side of unmanned boat 900 arranges horizontal hawser 902, the other end of horizontal hawser 902 is connected to circular ship 901, unmanned boat 900 is take the length of horizontal hawser 902 as radius, move in a circle as the center of circle take circular ship 901, form circular flight path 904, if there are many unmanned boats 900 to navigate by water simultaneously, adjacent unmanned boat 900 is connected with connection cable 903, to guarantee safety of navigation, imperial kite also can take off on unmanned boat.
Embodiment 5, the flying method of imperial kite, imperial kite has six kinds of flying methods, state: the traction state of (one) anchor pull wire arrangement; (2) the glide state of disengaging anchor pull wire arrangement; (3) traction state of umbrella anchor pull wire arrangement; (4) the glide state of disengaging umbrella anchor pull wire arrangement; (5) traction state of unmanned boat pull wire arrangement; (6) the glide state of disengaging unmanned boat pull wire arrangement; Between above-mentioned six kinds of flying methods, state, can switch mutually, its changing method step is as follows,
First stage, the flying method of anchor pull wire arrangement traction is switched to the method step of the flying method of umbrella anchor pull wire arrangement traction,
First step, imperial kite is in the time that the flying method of anchor pull wire arrangement traction takes off and reach higher flying height, flight of kites person is by the decoupling device from suspension hook 600 of anchor draught line tail ring 704, anchor pull wire arrangement separates completely with suspension hook 600, imperial kite departs from the traction of anchor pull wire arrangement, freely glide
Second step, flight of kites person receives the upper end hook connecting that turns to sister block 802 in suspension hook 600, and umbrella anchor pull wire arrangement is connected with suspension hook 600,
Third step, clockwise rotates umbrella anchor reel 806 and emits umbrella anchor 800, and the anchoring 800 of umbrella anchor is in sea, and imperial kite is switched to the traction state of umbrella anchor pull wire arrangement, increases flying height;
Subordinate phase, the flying method of umbrella anchor pull wire arrangement traction is switched to the method step of the flying method of unmanned boat pull wire arrangement traction,
The 4th step, rotates counterclockwise umbrella anchor reel 806 recorery parachute anchors 800 in life boat cabin, will turn to upper end decoupling device from suspension hook 600 of sister block 802, umbrella anchor pull wire arrangement separates completely with suspension hook 600, now imperial kite departs from the traction of umbrella anchor pull wire arrangement, freely glides
The 5th step, flight of kites person drives device and controls imperial kite near unmanned boat draught line 905 upper ends by driving beam, catches unmanned boat draught line tail ring 907,
The 6th step, receives unmanned boat draught line tail ring 907 hook connectings in suspension hook 600, and unmanned boat draught line tail ring 907 is connected with suspension hook 600, and now imperial kite is switched to the flying method of unmanned boat pull wire arrangement traction, and imperial kite increases flying height,
Phase III, unmanned boat pull wire arrangement flying method is switched to the method step of anchor pull wire arrangement flying method,
The 7th step, flight of kites person is by the decoupling device from suspension hook 600 of unmanned boat draught line tail ring 907, and unmanned boat pull wire arrangement separates completely with suspension hook 600, and imperial kite departs from the traction of unmanned boat pull wire arrangement, freely glides,
The 8th step, flight of kites person drives device and controls the upper end of imperial kite near anchor draught line 703 by driving beam, catches anchor draught line tail ring 704,
The 9th step, receives suspension hook 600 by anchor draught line tail ring 704 hook connectings, and anchor draught line tail ring 704 is connected with suspension hook 600, and now imperial kite is switched to the flying method of anchor pull wire arrangement traction, and imperial kite increases flying height.
Recorery parachute anchor method: referring to accompanying drawing 6, accompanying drawing 7, when traction state at imperial kite in umbrella anchor pull wire arrangement and imperial kite reach higher height, conter clockwise (reversing sense shown in arc arrow 808) Rotatable umbrella anchor reel 806, umbrella anchor draught line 801 loosens, umbrella anchor exhausting line 804 tightens up, now umbrella anchor 800 shrinks and closes up, after the part that umbrella anchor draught line 801 upper end virgin states are wound around is all loosened, umbrella anchor draught line 801, umbrella anchor exhausting line 804 simultaneously conter clockwise (reversing sense shown in arc arrow 808) direction is wrapped on umbrella anchor reel 806, umbrella anchor draught line 801, 804 rollings of umbrella anchor exhausting line are in umbrella anchor reel 806, thereby umbrella anchor 800 is recovered in the cabin of life boat 107, the recovery speed of umbrella anchor 800 is greater than the gliding speed of imperial kite, now imperial kite is switched to glide state, imperial kite freely glides, its flying height declines gradually simultaneously.
Emit umbrella anchor method: referring to accompanying drawing 6, accompanying drawing 7, imperial kite is in free glide state, when imperial kite is reduced to specified altitude, cw (direction shown in arc arrow 808) direction Rotatable umbrella anchor reel 806, umbrella anchor draught line 801, umbrella anchor exhausting line 804, umbrella anchor 800 is emitted, when umbrella anchor draught line 801 is all emitted, suitable cw (direction shown in arc arrow 808) direction Rotatable umbrella anchor reel 806 again, suitably tighten up umbrella anchor draught line 801, loosen umbrella anchor exhausting line 804 completely, now umbrella anchor 800 opens and is anchored in sea, locking anchor reel 806 prevents its reversion, now imperial kite is switched to umbrella anchor pull wire arrangement traction state, imperial kite increases flying height.
Claims (9)
1. imperial kite, comprise kite, draught line, described imperial kite is characterized in that: imperial kite comprises raising force face (100), lower lifting surface (102), bottom right bracing wire (105), lower-left bracing wire (106), gas-filled protective post (108), gravity adjusting device, drive beam and drive device, suspension hook (600), draught line system (111), imperial kite arranges upper and lower two-layer lifting surface, the two ends of raising force face (100) are overlapping with the two ends of lower lifting surface (102) or be connected respectively, lower lifting surface (102) is recessed in the middle of adopting, two ends upwarp, arc curve form is symmetrically arranged, V-shaped wing structure, there is the larger dihedral angle, a life boat (107) is set below lower lifting surface (102), the cabin middle part of life boat (107) arranges a pneumatic seat (200) for flight of kites person, gas seat (200) arranges a set of gravity adjusting device, bottom right bracing wire (105) right-hand member is connected in the right side of lower main gasbag and an air bag (104) thereof, bottom right bracing wire (105) left end is connected with the fore right side of life boat (107), the left end of lower-left bracing wire (106) is connected in the left side of lower main gasbag and an air bag (104) thereof, the right-hand member of lower-left bracing wire (106) is connected with the fore of life boat left side, a window is opened to pneumatic seat (200) is installed in the middle part of lower lifting surface (102), and be connected with pneumatic seat (200), a gas-filled protective post (108) is erect at life boat (107) cabin rear portion, on carry line (109) lower end and be connected in suspension hook (600) upper end, under carry line (110) front end and be connected in suspension hook (600) upper end, under carry line (110) rear end and be connected in the middle part of lower lifting surface (102) or controlled by flight of kites person, suspension hook (600) is by anchor draught line tail ring (704) or turn to sister block (802) or unmanned boat draught line tail ring (907) is connected with draught line system (111), draught line system (111) has following three kinds of forms: anchor pull wire arrangement, umbrella anchor pull wire arrangement, unmanned boat pull wire arrangement.
2. imperial kite according to claim 1 is characterized in that: gravity adjusting device comprises: multi-layer airbag back cushion (301), multi-layer airbag pier (302), multi-layer airbag back cushion (301) is placed on the backrest of pneumatic seat (200), multi-layer airbag pier (302) be arranged on pneumatic seat (200) before, multi-layer airbag back cushion (301), multi-layer airbag pier (302) has multilayer air bag independently mutually, when these air bags are all full of air, center of gravity when flight of kites person is sitting in pneumatic seat (200) is to reach, these air bags are whole when emptying, flight of kites person's center of gravity is moved backward, flight of kites person's center-of-gravity position depends on multi-layer airbag back cushion (301), multi-layer airbag pier (302) is full of the quantity of air bag.
3. imperial kite according to claim 1 is characterized in that: drive beam and drive device, comprising: beam (400) is driven on the right side, beam (401), right rear end bracing wire (402), right front ends bracing wire (403), left back end bracing wire (404), left front end bracing wire (405), right bracing wire (406), left bracing wire (407) are driven in a left side, the rear end that beam (400) is driven on the right side is connected with the trailing edge right side of raising force face (100) by right rear end bracing wire (402), the lower end of right front ends bracing wire (403) is connected to the right side and drives the front end of beam (400), the upper end of right front ends bracing wire (403) is connected with the leading edge right side of raising force face (100), the middle part of beam (400) is driven by right bracing wire (406) and pneumatic seat (200) in the right side, life boat (107) right side connects, pneumatic seat (200) is fixed in life boat (107) cabin, the rear end that beam (401) is driven on a left side is connected with the trailing edge left side of raising force face (100) by left back end bracing wire (404), the lower end of left front end bracing wire (405) is connected to a left side and drives the front end of beam (401), the upper end of left front end bracing wire (405) is connected with the leading edge left side of raising force face (100), the middle part of beam (401) is driven by left bracing wire (407) and pneumatic seat (200) in a left side, life boat (107) left side connects, beam (400) is driven on the right side, a left side is driven beam (401) and is bending.
4. imperial kite according to claim 1 is characterized in that: anchor pull wire arrangement, comprise anchor (700), anchor draught line (703), the lower end of anchor draught line (703) is connected in anchor (700) and is anchored at seabed, anchor draught line (703) tail end arranges anchor draught line tail ring (704), and the above anchor pull wire arrangement of two covers is set on sea.
5. imperial kite according to claim 1 is characterized in that: described umbrella anchor pull wire arrangement, comprise and turn to sister block (802), turn to sister block (802) to hang on and carry in the suspension hook (600) of line (109) lower end, on carry line (109), the tractive force of umbrella anchor draught line (801) is transferred to raising force face (100) leading edge middle part by suspension hook (600), umbrella anchor exhausting line (804), the upper end of umbrella anchor draught line (801) is fixed in the set umbrella anchor fixed orifice (805) of umbrella anchor reel (806), the equal in length or approaching of the length of umbrella anchor exhausting line (804) and umbrella anchor draught line (801) equates, umbrella anchor exhausting line (804), the upper part of umbrella anchor draught line (801) is wrapped in umbrella anchor reel (806), its winding direction is contrary each other, the length being wound around and the total length of umbrella anchor equate or approach to equate, while clockwise rotating umbrella anchor reel (806), umbrella anchor draught line (801) tightens up, umbrella anchor exhausting line (804) loosens, while rotating counterclockwise umbrella anchor reel, umbrella anchor draught line loosens, umbrella anchor exhausting line tightens up, umbrella anchor closes up flexible, while continuing to rotate counterclockwise umbrella anchor reel, umbrella anchor draught line, umbrella anchor exhausting line equidirectional being wrapped in umbrella anchor reel simultaneously, until umbrella anchor is recovered in life boat, turn to sister block (802) that umbrella anchor exhausting line (804), umbrella anchor draught line (801) are turned to direction.
6. imperial kite according to claim 1 is characterized in that: described unmanned boat pull wire arrangement, comprise unmanned boat (900), circular ship (901), horizontal hawser (902), connection cable (903), unmanned boat draught line (905), unmanned boat draught line tail ring (907), when the unmanned boat draught line tail ring (907) that unmanned boat draught line (905) upper end arranges is connected together with suspension hook (600) hook connecting, imperial kite drags and under produced airflow function, takes off or increase flying height at unmanned boat, when unmanned boat draught line tail ring (907) separates with suspension hook (600) decoupling device, imperial kite freely glides, at a circular ship of sea anchoring (901), the ship side of unmanned boat (900) arranges horizontal hawser (902) and is connected to circular ship (901), unmanned boat (900) is take the length of horizontal hawser (902) as radius, move in a circle as the center of circle take circular ship (901), if there are many unmanned boats (900) to navigate by water simultaneously, adjacent unmanned boat (900) is connected with connection cable (903), imperial kite also can take off on unmanned boat.
7. imperial flight of kites method is characterized in that: the flying method of described imperial kite has six kinds of flying methods, state: the traction state of (one) anchor pull wire arrangement; (2) the glide state of disengaging anchor pull wire arrangement; (3) traction state of umbrella anchor pull wire arrangement; (4) the glide state of disengaging umbrella anchor pull wire arrangement; (5) traction state of unmanned boat pull wire arrangement; (6) the glide state of disengaging unmanned boat pull wire arrangement; Between above-mentioned six kinds of flying methods, state, can switch mutually, its changing method step is as follows,
First stage, the flying method of anchor pull wire arrangement traction is switched to the method step of the flying method of umbrella anchor pull wire arrangement traction, imperial kite in the time that the flying method of anchor pull wire arrangement traction takes off and reach higher flying height,
First step, flight of kites person is by anchor draught line tail ring (704) decoupling device from suspension hook (600), and anchor pull wire arrangement separates completely with suspension hook (600), and imperial kite departs from the traction of anchor pull wire arrangement, freely glides,
Second step, flight of kites person receives the upper end hook connecting that turns to sister block (802) in suspension hook (600), and umbrella anchor pull wire arrangement is connected with suspension hook (600),
Third step, clockwise rotates umbrella anchor reel (806) and emits umbrella anchor (800), and umbrella anchor anchoring (800) is in sea, and imperial kite is switched to the traction state of umbrella anchor pull wire arrangement, increases flying height;
Subordinate phase, the flying method of umbrella anchor pull wire arrangement traction is switched to the method step of the flying method of unmanned boat pull wire arrangement traction,
The 4th step, rotate counterclockwise umbrella anchor reel (806) recorery parachute anchor (800) in life boat cabin, to turn to upper end decoupling device from suspension hook (600) of sister block (802), umbrella anchor pull wire arrangement separates completely with suspension hook (600), now imperial kite departs from the traction of umbrella anchor pull wire arrangement, freely glide
The 5th step, flight of kites person drives device and controls imperial kite near unmanned boat draught line (906) upper end by driving beam, catches unmanned boat draught line tail ring (907),
The 6th step, unmanned boat draught line tail ring (907) hook connecting is received in suspension hook (600), unmanned boat draught line tail ring (907) is connected with suspension hook (600), the now flying method of imperial kite in the traction of unmanned boat pull wire arrangement, imperial kite increases flying height
Phase III, unmanned boat pull wire arrangement flying method is switched to the method step of anchor pull wire arrangement flying method,
The 7th step, flight of kites person is by unmanned boat draught line tail ring (907) decoupling device from suspension hook (600), and unmanned boat pull wire arrangement separates completely with suspension hook (600), and imperial kite departs from the traction of unmanned boat pull wire arrangement, freely glide
The 8th step, flight of kites person drives device and controls the upper end of imperial kite near anchor draught line (703) by driving beam, catches anchor draught line tail ring (704),
The 9th step, anchor draught line tail ring (704) hook connecting is received to suspension hook (600), anchor draught line tail ring (704) is connected with suspension hook (600), the now flying method of imperial kite in the traction of anchor pull wire arrangement, imperial kite increases flying height.
8. imperial flight of kites method according to claim 7 is characterized in that: recorery parachute anchor method, when traction state at imperial kite in umbrella anchor pull wire arrangement and imperial kite reach higher height, conter clockwise (reversing sense shown in arc arrow 808) Rotatable umbrella anchor reel (806), umbrella anchor draught line (801) loosens, umbrella anchor exhausting line (804) tightens up, now umbrella anchor (800) shrinks and closes up, when the part that umbrella anchor draught line (801) upper end virgin state is wound around is all loosened, umbrella anchor draught line (801), umbrella anchor exhausting line (804) simultaneously conter clockwise (reversing sense shown in arc arrow 808) direction is wrapped on umbrella anchor reel (806), umbrella anchor draught line (801), umbrella anchor exhausting line (804) rolling is in umbrella anchor reel (806), umbrella anchor (800) is recovered in the cabin of life boat (107), the recovery speed of umbrella anchor (800) is greater than the gliding speed of imperial kite.
9. imperial flight of kites method according to claim 7 is characterized in that: emit umbrella anchor method, imperial kite is in free glide state, when imperial kite is reduced to specified altitude, flight of kites person's cw (direction shown in arc arrow 808) direction Rotatable umbrella anchor reel (806), umbrella anchor draught line (801), umbrella anchor exhausting line (804), umbrella anchor (800) is emitted, when umbrella anchor draught line (801) is all emitted, suitable cw (direction shown in arc arrow 808) direction Rotatable umbrella anchor reel (806) again, suitably tighten up umbrella anchor draught line (801), loosen umbrella anchor exhausting line (804) completely, now umbrella anchor (800) opens and is anchored in sea, locking anchor reel (806) prevents its reversion, now imperial kite is switched to umbrella anchor pull wire arrangement traction state, imperial kite increases flying height.
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018058736A1 (en) * | 2016-09-27 | 2018-04-05 | 国家深海基地管理中心 | Method and device for detecting marine magnetism |
| CN111247067A (en) * | 2018-09-13 | 2020-06-05 | 株式会社松田康利事务所 | Equipment for flying and water skiing |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3024951A1 (en) * | 1980-07-02 | 1982-01-28 | Albrecht G. Prof. Dr. 4600 Dortmund Fischer | Lightweight wing for manned glider - has tubular front edge and adjustable profile fabric cover over struts |
| CH681880A5 (en) * | 1990-03-05 | 1993-06-15 | Jean Philippe Jaton | Hang-glider with inflated wing leading edge - has wing maintaining constant shape in flight permanently secured to rigid structure and stiffened behind leading edge |
| WO1998017530A1 (en) * | 1996-10-21 | 1998-04-30 | Andrew Raymond Campbell | Pilotable flying craft |
| FR2856651A1 (en) * | 2003-06-30 | 2004-12-31 | Patrick Jean Walter Hubert | Aquatic vehicle for water sports, has autonomous drift connected to vessel by line, where vessel has nose having inclination with respect to drift plane and adjustable along axis |
| CN101511671A (en) * | 2006-08-15 | 2009-08-19 | 天帆有限两合公司 | Apparatus for transmission and recovery of aerodynamic profile element, and aerodynamic profile element |
| EP2221090A1 (en) * | 2009-02-18 | 2010-08-25 | Sup'Air | Shock absorption device for a paraglider harness |
| US8490915B2 (en) * | 2010-07-20 | 2013-07-23 | Christopher Paul FARBOLIN | Ram air Rigid Structure Glider |
-
2014
- 2014-02-23 CN CN201410059654.1A patent/CN103786883A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3024951A1 (en) * | 1980-07-02 | 1982-01-28 | Albrecht G. Prof. Dr. 4600 Dortmund Fischer | Lightweight wing for manned glider - has tubular front edge and adjustable profile fabric cover over struts |
| CH681880A5 (en) * | 1990-03-05 | 1993-06-15 | Jean Philippe Jaton | Hang-glider with inflated wing leading edge - has wing maintaining constant shape in flight permanently secured to rigid structure and stiffened behind leading edge |
| WO1998017530A1 (en) * | 1996-10-21 | 1998-04-30 | Andrew Raymond Campbell | Pilotable flying craft |
| FR2856651A1 (en) * | 2003-06-30 | 2004-12-31 | Patrick Jean Walter Hubert | Aquatic vehicle for water sports, has autonomous drift connected to vessel by line, where vessel has nose having inclination with respect to drift plane and adjustable along axis |
| CN101511671A (en) * | 2006-08-15 | 2009-08-19 | 天帆有限两合公司 | Apparatus for transmission and recovery of aerodynamic profile element, and aerodynamic profile element |
| EP2221090A1 (en) * | 2009-02-18 | 2010-08-25 | Sup'Air | Shock absorption device for a paraglider harness |
| US8490915B2 (en) * | 2010-07-20 | 2013-07-23 | Christopher Paul FARBOLIN | Ram air Rigid Structure Glider |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018058736A1 (en) * | 2016-09-27 | 2018-04-05 | 国家深海基地管理中心 | Method and device for detecting marine magnetism |
| US10295699B2 (en) | 2016-09-27 | 2019-05-21 | National Deep Sea Center | Marine magnetism detection method and device |
| CN111247067A (en) * | 2018-09-13 | 2020-06-05 | 株式会社松田康利事务所 | Equipment for flying and water skiing |
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