CN103419907A - Flight vehicle for water sports - Google Patents

Flight vehicle for water sports Download PDF

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Publication number
CN103419907A
CN103419907A CN2012101560872A CN201210156087A CN103419907A CN 103419907 A CN103419907 A CN 103419907A CN 2012101560872 A CN2012101560872 A CN 2012101560872A CN 201210156087 A CN201210156087 A CN 201210156087A CN 103419907 A CN103419907 A CN 103419907A
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China
Prior art keywords
pipe
chassis
flange
antifriction
bearing box
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CN2012101560872A
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Chinese (zh)
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CN103419907B (en
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李钜彬
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Individual
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Individual
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Priority to CN201210156087.2A priority Critical patent/CN103419907B/en
Publication of CN103419907A publication Critical patent/CN103419907A/en
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Publication of CN103419907B publication Critical patent/CN103419907B/en
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Abstract

The invention discloses a flight vehicle for water sports. The flight vehicle comprises a foot-control jet assembly and two identical hand-control jet guns, wherein the foot-control jet assembly comprises a pair of shoes, a straight chassis and two arc bent pipes; a connection strip is fixed to the middle of the lower bottom surface of the chassis, and buoyancy barrels are fixed to four corners of the lower bottom surface of the chassis; the two bent pipes are connected to the connection strip, the initiating ends of the two bent pipes extend to form a round flared opening, a first flange is arranged outside the end portion of the round flared opening, a rolling bearing A is connected inside the first flange in a sleeved mode, the rolling bearing A is connected with one end of a water inlet pipe in a sleeved mode, the water inlet pipe is further sleeved with a rolling bearing B, and the outer wall of the water inlet pipe is fixedly sleeved with a water inlet flexible pipe; each bent pipe is divided into a head section and a tail section from the middle portion, a water division pipe is arranged on the pipe wall of each tail section, and each water division pipe is fixedly sleeved with a water division flexible pipe. When the flight vehicle is matched with a motorboat for use, a user can fly away from the water surface by several meters, and the flight vehicle is safe, exciting, interesting, easy to operate, very novel and very fun.

Description

The aquatic sports aircraft
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, can make the low distance of user fly away from the water surface, experience aeromarine enjoyment, this be really one larger sorry and blank, remain people to go to be filled up and develop innovation.
Summary of the invention
The technical problem to be solved in the present invention, be to provide a kind of aquatic sports aircraft, while being used in conjunction with motor boat, can fly away from the height of water surface number meter, safety, stimulation, interesting, and can control flexibly heading, simple to operate, very novel joyful.
For solving the problems of the technologies described above, technical scheme of the present invention is: the overwater flight device that a kind of use of travelling is provided, it comprises foot control ejection assemblies and two identical manual spray guns, the foot control ejection assemblies comprises a pair of shoes, straight chassis and two identical circular arc bend pipes, every manual spray gun includes the J-shaped bend pipe, its straight-tube portion overcoat has the arm cover, and arm cover below is provided with and the vertical handle be connected of straight-tube portion; The a pair of shoes interval is connected in the surface on chassis, and the engaging of going to the bottom on chassis has bottom corresponding to shape with it, and the middle part of going to the bottom on chassis is fixed with connecting strap, and going to the bottom four jiaos of chassis all is fixed with buoyancy tube, and each buoyancy tube all protrudes downwards on the bottom 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 is one-body molded, and be extended with circular enlarging, be provided with the first method orchid outside the end of circular enlarging, the first flange inner sleeve is connected to the A antifriction-bearing box, one end socket of A antifriction-bearing box and coolant inlet pipe, on the coolant inlet pipe outer wall near this end also overcoat the B antifriction-bearing box is arranged, on coolant inlet pipe outer wall between A antifriction-bearing box and B antifriction-bearing box, be provided with the flange that makes the two space, B antifriction-bearing box overcoat has the connection collar, between the end face of the connection collar and the first flange, is fixedly linked; From connecting the coolant inlet pipe outer wall of the collar to 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 bend pipe is partly therefrom all two sections of head and the tail, the coupling end that these head and the tail are two sections, and outer the second flange, the three-flange that is provided with corresponding connection, wherein be socketed with the C antifriction-bearing box in the second flange respectively, and the coupling end that described bend pipe is first section, be socketed in the C antifriction-bearing box; The rear tube wall of every bend pipe approaches mouth of pipe place, is equipped with the distributive pipe vertical with tube wall, and distributive pipe is fixed with a minute water tube hose outward, and the other end fixed jacket of minute 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 pass sole with connecting strap and chassis, with connecting strap, be fixedly linked.
Aquatic sports aircraft as above, in the gap of chassis and bottom and in each buoyancy tube, all be filled with foam
Aquatic sports aircraft as above, on corresponding the second flange, three-flange, be equipped with corresponding flat position on every bend pipe, between the flat position and connecting strap of the second flange, by bolt, is connected, so that two bend pipes are fixedly connected with chassis.
Aquatic sports aircraft as above, the surface of each C antifriction-bearing box, be equipped with the oil sealing of preventing water leakage.
Above-mentioned aquatic sports aircraft, due to when being used in conjunction with motor boat, the powerful reaction thrust that can produce by two bend pipe water sprays, make the user fly away from the height of water surface number meter, while falling due to chassis and buoyancy tube with the buoyancy of foam, the user can float on the surface and can submerged, safety, stimulate, interesting, and can be by the water spraying direction of two bend pipes of conversion and manual spray gun, control flexibly heading, simple to operate, very novel joyful, as long as training a little, can skillfully grasp method of operation, be applicable to very much wideling popularize to vast aquatic sports fan.
The 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 buoyancy tube is not installed;
Fig. 2 is the split figure of foot control ejection assemblies when buoyancy tube is not installed;
The local split figure that Fig. 3 is bend pipe;
The structural relation block diagram that Fig. 4 is chassis and buoyancy tube;
The use view that Fig. 5 is described invention.
The specific embodiment
Referring to Fig. 1, Fig. 2, a kind of aquatic sports aircraft is provided, it comprises foot control ejection assemblies 1 and two identical manual spray guns 2, foot control ejection assemblies 1 comprises a pair of shoes 3, straight chassis 4 and two identical circular arc bend pipes 5, a pair of shoes 3 intervals are connected in the surface on chassis 4, the engaging of going to the bottom on chassis 4 has bottom 9 corresponding to shape with it, 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 is one-body molded, and be extended with circular enlarging 12, be provided with first method orchid 13 outside the end of circular enlarging 12, be socketed with A antifriction-bearing box 14 in the first flange 13, A antifriction-bearing box 14 is socketed with an end of coolant inlet pipe 15, on coolant inlet pipe 15 outer walls near this end also overcoat B antifriction-bearing box 16 is arranged, on coolant inlet pipe 15 outer walls between A antifriction-bearing box 14 and B antifriction-bearing box 16, be provided with the flange 17 that makes the two space, B antifriction-bearing box 16 overcoats have the collar 18 of connection, between the end face of the connection collar 18 and the first flange 13, be fixedly linked, from connecting coolant inlet pipe 15 outer walls of the collar 18 to coolant inlet pipe 15 other ends, be fixed with inlet water hose 19, inlet water hose 19 is connected with the water jet nozzle on motor boat.Due to the double rolling bearing setting of A antifriction-bearing box 14 and B antifriction-bearing box 16, during use, foot control ejection assemblies 1 or coolant inlet pipe 15 be direction free to rotate all, and can not cause inlet water hose 19 knottings, thereby can guarantee that current enter inlet water hose 19 swimmingly.Owing to being fixedly linked between the end face that connects the collar 18 and the first flange 13, can make coolant inlet pipe 15 keep being actively socketed in A antifriction-bearing box 14 and B antifriction-bearing box 16 and can not deviate from, can avoid current in coolant inlet pipe 15 to overflow from the socket gap of coolant inlet pipe 15 and bearing simultaneously.
Referring to Fig. 1-Fig. 3, every manual spray gun 2 includes J-shaped bend pipe 6, and its straight-tube portion overcoat has arm cover 7, and arm overlaps 7 belows and is provided with and the vertical handle be connected 8 of straight-tube portion; Every bend pipe 5 is partly therefrom all two sections of head and the tail, the coupling end that these head and the tail are two sections, outer the second flange 20, the three-flange 21 that is provided with corresponding connection, wherein be socketed with C antifriction-bearing box 22 in the second flange 20 respectively, the coupling end that described bend pipe 5 is first section, be socketed in C antifriction-bearing box 22; The rear tube wall of every bend pipe 5 approaches mouth of pipe place, is equipped with the distributive pipe vertical with tube wall 23, the outer minute water tube hose 24 that is fixed with of distributive pipe 23, and the other end fixed jacket of minute water tube hose 24 is in the bent tube section end of J-shaped bend pipe 6.
Referring to Fig. 1, Fig. 2, every footwear 3 all by bolt pass sole with connecting strap 25 and chassis 4, with connecting strap 10, be fixedly linked.On every bend pipe 5 on corresponding the second flange 20, three-flange 21, between the flat position 26 that is equipped with corresponding flat position 26, the second flanges 20 and connecting strap 10, by spiral shell phase-detecting company, so that two bend pipes 5 are fixedly connected with chassis 4.
Referring to Fig. 1-Fig. 4, during use, the user is inserted in both feet in footwear 3, both hands, respectively from the bent tube section place direction of two J-shaped bend pipes 6, stretch among two arm covers 7, make in two forearms to be enclosed within two arm covers 7, both hands stretch out catches respectively two handles 8, can start flight operation.The water jet nozzle ejection of powerful current from motor boat, enter two bend pipes 5 through inlet water hose 19, coolant inlet pipe 15 shuntings, then spray downwards from the tail end of two bend pipes 5, thereby produce antagonistic force upwards, can carry the weight of 150KG left and right, make the related whole aircraft of human body fly away from the height of water surface number meter, concrete flies away from highly, with the pump power of motor boat, determines, and pump power is larger, fly away from highly greatlyr, vice versa.Simultaneously, current enter two distributive pipes 23, minute water tube hose 24, 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, and the user converts the water spraying direction of manual spray gun 2, can play the effect of balance the body balance.
When needs convert the fore-and-aft direction of flight, the user shifts to forefoot by centre of body weight, trample chassis 4 with forefoot, due to chassis 4 and connecting strap 10, the second flange 20, C antifriction-bearing box 22 connects in succession, article two, the coupling end of first section of bend pipe 5, can pass through respectively the rotation of two C antifriction-bearing boxs 22, clockwise rotate, two the second flanges 20 rotate with corresponding C antifriction-bearing box 22 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, thereby three-flange 21 also the rear of related two bend pipes 5 rotate simultaneously, article two, the tail end of bend pipe 5 is offset after one's death to the user, be its water spraying direction by the vertical duction user after one's death, thereby produce antagonistic force forward, the related whole aircraft of human body is flown forward.Now, the user can, by J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards after one's death, also play the booster action that promotion is flown forward simultaneously.Otherwise, when needs fly backward, the user shifts to hind paw by centre of body weight, trample chassis 4 with hind paw, in like manner, article two, the coupling end of first section of bend pipe 5, can pass through respectively the rotation of two C antifriction-bearing boxs 22, rotate counterclockwise, two the second flanges 20 rotate with corresponding C antifriction-bearing box 22 respectively simultaneously, the three-flange 21 also rear of related two bend pipes 5 rotates simultaneously, article two, the tail end of bend pipe 5 is offset to user the place ahead, be that its water spraying direction is by vertical duction user the place ahead, thereby produce antagonistic force backward, the related whole aircraft of human body is flown backward.Now, the user can, by J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards health the place ahead, also play the booster action that promotion is flown backward simultaneously.
When needs convert the left and right directions of flight, the user shifts to the left foot palm by centre of body weight, be that health is left-leaning and trample chassis 4 with the left foot palm, article two, the tail end of bend pipe 5 is offset to the user right side, be that its water spraying direction is by vertical duction user right side, thereby produce antagonistic force left, the related whole aircraft of human body is flown left; Simultaneously, the user can be by J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards right side of body, thereby produces antagonistic force left, also plays the booster action that promotion is flown left.Otherwise, the user shifts to the right crus of diaphragm palm by centre of body weight, be the health Right deviation and trample chassis 4 with the right crus of diaphragm palm, article two, the tail end of bend pipe 5 is offset to the user left side, be that its water spraying direction is by vertical duction user left side, thereby produce antagonistic force to the right, the related whole aircraft of human body is flown to the right; Simultaneously, the user can be by J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards left side of body, thereby produces antagonistic force to the right, also plays the booster action that promotion is flown to the right.
Referring to Fig. 1, Fig. 4, Fig. 5, going to the bottom four jiaos of chassis 4 all is fixed with buoyancy tube 11, and each buoyancy tube 11 all protrudes downwards on bottom 9 surfaces, in the gap of chassis 4 and bottom 9 and in each buoyancy tube 11, all is filled with foam.When the user flies away from the water surface and then falls, due to the buoyancy of foam, the user can float on the surface and can submerged, very safe.
Referring to Fig. 3, the surface of each C antifriction-bearing box 22, be equipped with the oil sealing 27 of preventing water leakage, after can preventing that current from entering bend pipe 5, from the connection gap of two sections of bend pipe 5 head and the tail, spills, and can avoid the antagonistic force of current to be weakened.
Above-described embodiment is the preferred embodiments of the present invention, and all and the similar structure of the present invention and the equivalence of doing 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) and two identical manual spray guns (2), foot control ejection assemblies (1) comprises a pair of shoes (3), straight chassis (4) and two identical circular arc bend pipes (5), every 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 and the vertical handle be connected of straight-tube portion (8), a pair of shoes (3) interval is connected in the surface of chassis (4), the engaging of going to the bottom on chassis (4) has bottom (9) corresponding to shape with it, the middle part of going to the bottom on chassis (4) is fixed with connecting strap (10), going to the bottom four jiaos of chassis (4) all is fixed with buoyancy tube (11), and each buoyancy tube (11) all protrudes on bottom (9) surface 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 is one-body molded, and be extended with circular enlarging (12), be provided with first method orchid (13) outside the end of circular enlarging (12), be socketed with A antifriction-bearing box (14) in the first flange (13), A antifriction-bearing box (14) is socketed with an end of coolant inlet pipe (15), on coolant inlet pipe (15) outer wall near this end also overcoat B antifriction-bearing box (16) is arranged, 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) that makes the two space, B antifriction-bearing box (16) overcoat has the connection collar (18), between the end face of the connection collar (18) and the first flange (13), 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, every bend pipe (5) is partly therefrom all two sections of head and the tail, the coupling end that these head and the tail are two sections, be provided with corresponding the second flange (20), the three-flange (21) connected respectively, wherein in the second flange (20), be socketed with C antifriction-bearing box (22), the coupling end that described bend pipe (5) is first section, be socketed in C antifriction-bearing box (22), the rear tube wall of every bend pipe (5) approaches mouth of pipe place, be equipped with the distributive pipe vertical with tube wall (23), the outer minute water tube hose (24) that is fixed with of distributive pipe (23), the other end fixed jacket of minute water tube hose (24) is in the bent tube section end of J-shaped bend pipe (6).
2. according to the described aquatic sports aircraft of right 1, it is characterized in that: every footwear (3) all by bolt pass sole with connecting strap (25) and chassis (4), with connecting strap (10), be fixedly linked.
3. according to the described aquatic sports aircraft of right 1, it is characterized in that: in the gap of chassis (4) and bottom (9) and in each buoyancy tube (11), all be filled with foam.
4. according to the described aquatic sports aircraft of right 1, it is characterized in that: on upper corresponding the second flange (20) of every bend pipe (5), three-flange (21), be equipped with corresponding flat position (26), between the flat position (26) and connecting strap (10) of the second flange (20), by bolt, be connected, so that two bend pipes (5) are fixedly connected with chassis (4).
5. according to the described aquatic sports aircraft of right 1, it is characterized in that: the surface of each C antifriction-bearing box (22) is equipped with the oil sealing (27) of preventing water leakage.
CN201210156087.2A 2012-05-18 2012-05-18 Aquatic sports aircraft Expired - Fee Related CN103419907B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210156087.2A CN103419907B (en) 2012-05-18 2012-05-18 Aquatic sports aircraft

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Application Number Priority Date Filing Date Title
CN201210156087.2A CN103419907B (en) 2012-05-18 2012-05-18 Aquatic sports aircraft

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CN103419907A true CN103419907A (en) 2013-12-04
CN103419907B CN103419907B (en) 2015-12-16

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109737820A (en) * 2019-03-04 2019-05-10 叶兴龙 A kind of overwater flight fireworks setting-off device
CN111419565A (en) * 2020-04-22 2020-07-17 王凡 Auxiliary walking wheelchair for surgery

Citations (6)

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Publication number Priority date Publication date Assignee Title
JP2003176719A (en) * 2001-12-10 2003-06-27 Honda Motor Co Ltd Exhaust and drain structure for vessel
WO2004043783A1 (en) * 2002-11-12 2004-05-27 Scott Redmond Personal flight vehicle
WO2005091713A2 (en) * 2004-03-26 2005-10-06 Raymond Li Personal propulsion device
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003176719A (en) * 2001-12-10 2003-06-27 Honda Motor Co Ltd Exhaust and drain structure for vessel
WO2004043783A1 (en) * 2002-11-12 2004-05-27 Scott Redmond Personal flight vehicle
WO2005091713A2 (en) * 2004-03-26 2005-10-06 Raymond Li Personal propulsion device
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)

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Title
王寅珊: "加拿大华裔梦幻发明:喷水背包让你飞", 《新华每日电讯》, 17 February 2009 (2009-02-17) *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109737820A (en) * 2019-03-04 2019-05-10 叶兴龙 A kind of overwater flight fireworks setting-off device
CN111419565A (en) * 2020-04-22 2020-07-17 王凡 Auxiliary walking wheelchair for surgery

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