CN103419907B - Aquatic sports aircraft - Google Patents
Aquatic sports aircraft Download PDFInfo
- Publication number
- CN103419907B CN103419907B CN201210156087.2A CN201210156087A CN103419907B CN 103419907 B CN103419907 B CN 103419907B CN 201210156087 A CN201210156087 A CN 201210156087A CN 103419907 B CN103419907 B CN 103419907B
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- antifriction
- chassis
- bearing box
- pipe
- flange
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Abstract
The invention discloses a kind of aquatic sports aircraft, it comprises the foot control ejection assemblies manual spray gun identical with two, and foot control ejection assemblies comprises a pair of shoes, straight chassis and two circular arc bend pipes; The middle part of going to the bottom on chassis is fixed with connecting strap, and the corner of going to the bottom on chassis is all fixed with buoyancy tube; Article two, bend pipe is connected on connecting strap, the initiating terminal of the two is extended with circular enlarging, first method orchid is provided with outside the end of circular enlarging, first flange inner sleeve is connected to A antifriction-bearing box, one end of A antifriction-bearing box and coolant inlet pipe is socketed, coolant inlet pipe is gone back overcoat and have B antifriction-bearing box, coolant inlet pipe outer wall is fixed with inlet water hose; Every bar bend pipe all therefrom part is head and the tail two sections, and its rear tube wall is equipped with distributive pipe, and distributive pipe fixed sleeves has a point water tube hose.Said structure and motor boat with the use of time, the height of water surface number meter can be flown away from, safety, stimulate, interesting, simple to operate, very novel joyful.
Description
Technical field
The present invention relates to Boating-used equipment, particularly a kind of aquatic sports aircraft.
Background technology
Existing Boating-used equipment, comprise motor boat, surfboard, surfboard, windsurfing, kite plate etc., although multifarious, have their own characteristics each, but at present on the market, also without any a kind of Boating-used equipment, the low distance of user can be made to fly away from the water surface, experience aeromarine enjoyment, this be really one larger sorry and blank, needing people goes to carry out filling up and developing innovation.
Summary of the invention
The technical problem to be solved in the present invention, is to provide a kind of aquatic sports aircraft, with motor boat with the use of time, the height of water surface number meter can be flown away from, safety, stimulate, interesting, and heading can be controlled flexibly, simple to operate, very novel joyful.
For solving the problems of the technologies described above, technical scheme of the present invention is: provide a kind of overwater flight device of travelling, it comprises the foot control ejection assemblies manual spray gun identical with two, foot control ejection assemblies comprises a pair of shoes, the straight chassis circular arc bend pipe identical with two, every only manual spray gun includes J-shaped bend pipe, its straight-tube portion overcoat has arm cover, and arm cover below is provided with the handle that be connected vertical with straight-tube portion; A pair of shoes interval is connected to the surface on chassis, the bottom engaging and have shape with it corresponding of going to the bottom on chassis, and the middle part of going to the bottom on chassis is fixed with connecting strap, and the corner of going to the bottom on chassis is all fixed with buoyancy tube, and each buoyancy tube protrudes all downwards at bottom on the surface; Article two, bend pipe is connected on connecting strap, and mutually oppositely stretch, the initiating terminal of the two is connected side by side and one-body molded, and be extended with circular enlarging, first method orchid is provided with outside the end of circular enlarging, first flange inner sleeve is connected to A antifriction-bearing box, one end of A antifriction-bearing box and coolant inlet pipe is socketed, on coolant inlet pipe outer wall, near this end, also overcoat has B antifriction-bearing box, on coolant inlet pipe outer wall between A antifriction-bearing box and B antifriction-bearing box, be provided with the flange making the two spaced, B antifriction-bearing box overcoat has the connection collar, connects between the collar and the end face of the first flange and is fixedly linked; From the connection collar to the coolant inlet pipe outer wall of the coolant inlet pipe other end, be fixed with inlet water hose, inlet water hose is connected with the water jet nozzle on motor boat; Every bar bend pipe all therefrom part is the coupling end of head and the tail two sections, these head and the tail two sections, and outer the second flange, the three-flange being provided with correspondence and connecting, is wherein socketed with C antifriction-bearing box in the second flange, the coupling end that described bend pipe is first section, is socketed in C antifriction-bearing box respectively; The rear tube wall of every bar bend pipe, close to mouth of pipe place, is equipped with the distributive pipe vertical with tube wall, and distributive pipe fixed sleeves has a point water tube hose, and the other end fixed jacket of point water tube hose is in the bent tube section end of J-shaped bend pipe.
Aquatic sports aircraft as above, every footwear all by bolt through sole with connecting strap and chassis, be fixedly linked with connecting strap.
Aquatic sports aircraft as above, in the gap of chassis and bottom and in each buoyancy tube, is all filled with foam
Aquatic sports aircraft as above, on the second flange corresponding on every article of bend pipe, three-flange, is equipped with corresponding flat position, between the flat position of the second flange and connecting strap, is connected, is fixedly connected with to make two bend pipes with chassis by bolt.
Aquatic sports aircraft as above, the surface of each C antifriction-bearing box, is equipped with the oil sealing of preventing water leakage.
Above-mentioned aquatic sports aircraft, due to motor boat with the use of time, by the powerful reaction thrust that two bend pipe water sprays produce, user is made to fly away from the height of water surface number meter, when falling due to chassis and buoyancy tube the buoyancy with foam, user can float on the surface and can not submerged, safety, stimulate, interesting, and by converting the water spraying direction of two bend pipes and manual spray gun, flexible control heading, simple to operate, very novel joyful, as long as train a little, skillfully can grasp method of operation, be applicable to very much wideling popularize to vast aquatic sports fan.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the present invention is further detailed explanation.
Fig. 1 is the block diagram of described invention when not installing buoyancy tube;
Fig. 2 is the split figure of foot control ejection assemblies when not installing buoyancy tube;
Fig. 3 is the local split figure of bend pipe;
Fig. 4 is the structural relation block diagram of chassis and buoyancy tube;
Fig. 5 is the using state schematic diagram of described invention.
Detailed description of the invention
See Fig. 1, Fig. 2, a kind of aquatic sports aircraft is provided, it comprises the foot control ejection assemblies 1 manual spray gun 2 identical with two, foot control ejection assemblies 1 comprises a pair of shoes 3, the circular arc bend pipe 5 that straight chassis 4 is identical with two, a pair of shoes 3 interval is connected to the surface on chassis 4, the bottom 9 engaging and have shape with it corresponding of going to the bottom on chassis 4, the middle part of going to the bottom on chassis 4 is fixed with connecting strap 10, article two, bend pipe 5 is connected on connecting strap 10, and mutually oppositely stretch, the initiating terminal of the two is connected side by side and one-body molded, and be extended with circular enlarging 12, first method orchid 13 is provided with outside the end of circular enlarging 12, A antifriction-bearing box 14 is socketed with in first flange 13, A antifriction-bearing box 14 is socketed with one end of coolant inlet pipe 15, on coolant inlet pipe 15 outer wall, near this end, also overcoat has B antifriction-bearing box 16, on coolant inlet pipe 15 outer wall between A antifriction-bearing box 14 and B antifriction-bearing box 16, be provided with the flange 17 making the two spaced, B antifriction-bearing box 16 overcoat has the connection collar 18, connect between the collar 18 and the end face of the first flange 13 and be fixedly linked, from connecting coolant inlet pipe 15 outer wall of the collar 18 to coolant inlet pipe 15 other end, be fixed with inlet water hose 19, inlet water hose 19 is connected with the water jet nozzle on motor boat.Because the double rolling bearing of A antifriction-bearing box 14 and B antifriction-bearing box 16 is arranged, during use, foot control ejection assemblies 1 or coolant inlet pipe 15 direction all free to rotate, and inlet water hose 19 can not be caused to tie a knot, thus enter inlet water hose 19 while smooth in water flow can be ensured.Be fixedly linked owing to connecting between the collar 18 and the end face of the first flange 13, coolant inlet pipe 15 can be made to keep being actively socketed in A antifriction-bearing box 14 and B antifriction-bearing box 16 and can not deviating from, the current in coolant inlet pipe 15 can be avoided simultaneously to overflow from coolant inlet pipe 15 and the socket gap of bearing.
See Fig. 1-Fig. 3, often only manual spray gun 2 includes J-shaped bend pipe 6, and its straight-tube portion overcoat has arm to overlap 7, is provided with the handle 8 that be connected vertical with straight-tube portion below arm cover 7; Every bar bend pipe 5 all therefrom part is head and the tail two sections, the coupling end of these head and the tail two sections, outer the second flange 20, the three-flange 21 being provided with corresponding connection, is wherein socketed with C antifriction-bearing box 22 in the second flange 20 respectively, the coupling end of first section of described bend pipe 5, is socketed in C antifriction-bearing box 22; The rear tube wall of every bar bend pipe 5, close to mouth of pipe place, is equipped with the distributive pipe 23 vertical with tube wall, and distributive pipe 23 fixed sleeves has point water tube hose 24, and the other end fixed jacket of point water tube hose 24 is in the bent tube section end of J-shaped bend pipe 6.
See Fig. 1, Fig. 2, every footwear 3 all by bolt through sole with connecting strap 25 and chassis 4, be fixedly linked with connecting strap 10.On the second flange 20 corresponding on every article of bend pipe 5, three-flange 21, between the flat position 26 being equipped with corresponding flat position 26, second flange 20 and connecting strap 10, connected by spiral shell phase-detecting, be fixedly connected with chassis 4 to make two bend pipes 5.
See Fig. 1-Fig. 4, during use, both feet are inserted in footwear 3 by user, both hands, respectively from the direction, bent tube section place of two J-shaped bend pipes 6, stretch among two arm covers 7, make to be enclosed within two forearms in two arm covers 7, both hands stretch out catches two handles 8 respectively, can start flight operation.Powerful current are from the water jet nozzle ejection motor boat, two bend pipes 5 are entered through inlet water hose 19, coolant inlet pipe 15 shunting, then spray downwards from the tail end of two bend pipes 5, thus produce antagonistic force upwards, the weight of about 150KG can be carried, the related whole aircraft of human body is made to fly away from the height of water surface number meter, concrete flies away from height, and fixed with the pump power of motor boat, pump power is larger, fly away from highly larger, vice versa.Meanwhile, current enter two distributive pipes 23, point water tube hose 24, and then enter the J-shaped bend pipe 6 of two manual spray guns 2, and spray from the mouth of pipe of its straight-tube portion, user converts the water spraying direction of manual spray gun 2, can play the effect regulating total balance of the body.
When needing the fore-and-aft direction of conversion flight, centre of body weight is shifted to forefoot by user, namely chassis 4 is trampled with forefoot, due to chassis 4 and connecting strap 10, second flange 20, C antifriction-bearing box 22 connects in succession, article two, the coupling end of first section of bend pipe 5, can respectively by the rotation of two C antifriction-bearing boxs 22, rotate clockwise, two the second flanges 20 rotate with the C antifriction-bearing box 22 of correspondence respectively simultaneously, again due to two three-flanges 21 respectively with two the second flanges 20, article two, the rear of bend pipe 5 is connected, thus the rear of three-flange 21 also related two articles of bend pipes 5 rotates simultaneously, article two, namely the tail end of bend pipe 5 offsets after one's death to user, namely its water spraying direction by vertical duction user after one's death, thus the antagonistic force produced forward, make the related whole aircraft forward flight of human body.Now, user by J-shaped bend pipe 6 water injector of two manual spray guns 2 towards after one's death, can also play the booster action promoting flight forward simultaneously.Otherwise, when needs fly backward, centre of body weight is shifted to hind paw by user, namely chassis 4 is trampled with hind paw, in like manner, article two, the coupling end of first section of bend pipe 5, can respectively by the rotation of two C antifriction-bearing boxs 22, rotate counterclockwise, two the second flanges 20 rotate with the C antifriction-bearing box 22 of correspondence respectively simultaneously, the rear of three-flange 21 also related two articles of bend pipes 5 rotates simultaneously, article two, namely the tail end of bend pipe 5 offsets to user front, namely its water spraying direction is by vertical duction user front, thus the antagonistic force produced backward, the related whole aircraft of human body is flown backward.Now, user by J-shaped bend pipe 6 water injector of two manual spray guns 2 towards health front, can also play the booster action that promotion is flown backward simultaneously.
When needing the left and right directions of conversion flight, centre of body weight is shifted to the left foot palm by user, namely health is left-leaning and trample chassis 4 with the left foot palm, article two, namely the tail end of bend pipe 5 offsets on the right side of user, namely its water spraying direction is by the right side of vertical duction user, thus the antagonistic force produced left, the related whole aircraft of human body is flown left; Meanwhile, user by J-shaped bend pipe 6 water injector of two manual spray guns 2 towards right side of body, thus can produce antagonistic force left, also plays the booster action that promotion is flown left.Otherwise, centre of body weight is shifted to the right crus of diaphragm palm by user, namely health Right deviation and with right crus of diaphragm the palm trample chassis 4, article two, namely the tail end of bend pipe 5 offsets on the left of user, namely its water spraying direction is by the left of vertical duction user, thus the antagonistic force produced to the right, the related whole aircraft of human body is flown to the right; Meanwhile, user by J-shaped bend pipe 6 water injector of two manual spray guns 2 towards left side of body, thus can produce antagonistic force to the right, also plays the booster action that promotion is flown to the right.
See Fig. 1, Fig. 4, Fig. 5, the corner of going to the bottom on chassis 4 is all fixed with buoyancy tube 11, and each buoyancy tube 11 protrudes at bottom 9 on the surface all downwards, in the gap of chassis 4 and bottom 9 and in each buoyancy tube 11, is all filled with foam.User flies away from the water surface when then falling, and due to the buoyancy of foam, user can float on the surface and can not submerged, very safe.
See Fig. 3, the surface of each C antifriction-bearing box 22, is equipped with the oil sealing 27 of preventing water leakage, after can preventing current from entering bend pipe 5, spills, the antagonistic force of current can be avoided to be weakened from the connection gap of bend pipe 5 head and the tail two sections.
Above-described embodiment is the preferred embodiments of the present invention, and all structures similar with the present invention and the equivalence done change, and all should belong to protection category of the present invention.
Claims (5)
1. an aquatic sports aircraft, it is characterized in that: it comprises foot control ejection assemblies (1) the manual spray gun (2) identical with two, foot control ejection assemblies (1) comprises a pair of shoes (3), straight chassis (4) the circular arc bend pipe (5) identical with two, every only manual spray gun (2) includes J-shaped bend pipe (6), its straight-tube portion overcoat has arm cover (7), and arm cover (7) below is provided with the handle (8) that be connected vertical with straight-tube portion, a pair of shoes (3) interval is connected to the surface of chassis (4), the bottom (9) engaging and have shape with it corresponding of going to the bottom on chassis (4), the middle part of going to the bottom on chassis (4) is fixed with connecting strap (10), the corner of going to the bottom on chassis (4) is all fixed with buoyancy tube (11), and each buoyancy tube (11) protrudes at bottom (9) on the surface all downwards, article two, bend pipe (5) is connected on connecting strap (10), and mutually oppositely stretch, the initiating terminal of the two is connected side by side and one-body molded, and be extended with circular enlarging (12), first method orchid (13) is provided with outside the end of circular enlarging (12), A antifriction-bearing box (14) is socketed with in first flange (13), A antifriction-bearing box (14) is socketed with one end of coolant inlet pipe (15), on coolant inlet pipe (15) outer wall, near this end, also overcoat has B antifriction-bearing box (16), on coolant inlet pipe (15) outer wall between A antifriction-bearing box (14) and B antifriction-bearing box (16), be provided with the flange (17) making the two spaced, B antifriction-bearing box (16) overcoat has the connection collar (18), connect between the collar (18) and the end face of the first flange (13) and be fixedly linked, from the connection collar (18) to coolant inlet pipe (15) outer wall of coolant inlet pipe (15) other end, be fixed with inlet water hose (19), inlet water hose (19) is connected with the water jet nozzle on motor boat, every bar bend pipe (5) all therefrom part is head and the tail two sections, the coupling end of these head and the tail two sections, outer the second flange (20), the three-flange (21) being provided with corresponding connection respectively, wherein be socketed with C antifriction-bearing box (22) in the second flange (20), the coupling end of first section of described bend pipe (5), is socketed in C antifriction-bearing box (22), the rear tube wall of every bar bend pipe (5) is close to mouth of pipe place, be equipped with the distributive pipe (23) vertical with tube wall, distributive pipe (23) fixed sleeves has a point water tube hose (24), and the other end fixed jacket of point water tube hose (24) is in the bent tube section end of J-shaped bend pipe (6).
2. aquatic sports aircraft according to claim 1, it is characterized in that: every footwear (3) all by bolt through sole with connecting strap (25) and chassis (4), be fixedly linked with connecting strap (10).
3. aquatic sports aircraft according to claim 1, is characterized in that: in the gap of chassis (4) and bottom (9) and in each buoyancy tube (11), be all filled with foam.
4. aquatic sports aircraft according to claim 1, it is characterized in that: on upper corresponding the second flange (20) of every article bend pipe (5), three-flange (21), be equipped with corresponding flat position (26), between the flat position (26) of the second flange (20) and connecting strap (10), be connected by bolt, be fixedly connected with chassis (4) to make two bend pipes (5).
5. aquatic sports aircraft according to claim 1, is characterized in that: the surface of each C antifriction-bearing box (22), is equipped with the oil sealing (27) of preventing water leakage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210156087.2A CN103419907B (en) | 2012-05-18 | 2012-05-18 | Aquatic sports aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210156087.2A CN103419907B (en) | 2012-05-18 | 2012-05-18 | Aquatic sports aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103419907A CN103419907A (en) | 2013-12-04 |
| CN103419907B true CN103419907B (en) | 2015-12-16 |
Family
ID=49645401
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210156087.2A Expired - Fee Related CN103419907B (en) | 2012-05-18 | 2012-05-18 | Aquatic sports aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103419907B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109737820A (en) * | 2019-03-04 | 2019-05-10 | 叶兴龙 | A kind of water flying fireworks display device |
| CN111419565A (en) * | 2020-04-22 | 2020-07-17 | 王凡 | Auxiliary walking wheelchair for surgery |
| CN115077860A (en) * | 2022-06-01 | 2022-09-20 | 山东电力工程咨询院有限公司 | Submarine optical cable damage detection device and detection method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7614355B2 (en) * | 2006-07-12 | 2009-11-10 | Eugene Zeyger | Personal flying water jet apparatus |
| CN101857074A (en) * | 2009-04-09 | 2010-10-13 | 尚德敏 | Over-water running method and over-water running shoes |
| CN202593816U (en) * | 2012-05-18 | 2012-12-12 | 李钜彬 | Aircraft for water sports |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3818905B2 (en) * | 2001-12-10 | 2006-09-06 | 本田技研工業株式会社 | Ship exhaust and drainage structure |
| US7182295B2 (en) * | 2002-11-12 | 2007-02-27 | Scott D. Redmond | Personal flight vehicle and system |
| US7258301B2 (en) * | 2004-03-26 | 2007-08-21 | Raymond Li | Personal propulsion device |
-
2012
- 2012-05-18 CN CN201210156087.2A patent/CN103419907B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7614355B2 (en) * | 2006-07-12 | 2009-11-10 | Eugene Zeyger | Personal flying water jet apparatus |
| CN101857074A (en) * | 2009-04-09 | 2010-10-13 | 尚德敏 | Over-water running method and over-water running shoes |
| CN202593816U (en) * | 2012-05-18 | 2012-12-12 | 李钜彬 | Aircraft for water sports |
Non-Patent Citations (1)
| Title |
|---|
| 加拿大华裔梦幻发明：喷水背包让你飞;王寅珊;《新华每日电讯》;20090217;全文 * |
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| Publication number | Publication date |
|---|---|
| CN103419907A (en) | 2013-12-04 |
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Granted publication date: 20151216 Termination date: 20170518 |
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| CF01 | Termination of patent right due to non-payment of annual fee |