CN202593816U - Aircraft for water sports - Google Patents
Aircraft for water sports Download PDFInfo
- Publication number
- CN202593816U CN202593816U CN2012202263760U CN201220226376U CN202593816U CN 202593816 U CN202593816 U CN 202593816U CN 2012202263760 U CN2012202263760 U CN 2012202263760U CN 201220226376 U CN201220226376 U CN 201220226376U CN 202593816 U CN202593816 U CN 202593816U
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- CN
- China
- Prior art keywords
- flange
- chassis
- antifriction
- pipe
- aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H2011/006—Marine propulsion by water jets with propulsive medium supplied from sources external to propelled vessel, e.g. water from public water supply
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- Special Spraying Apparatus (AREA)
Abstract
The utility model discloses an aircraft for water sports, and the aircraft comprises a foot-control injection assembly and two identical hand-control spray guns, wherein the foot-control injection assembly comprises a pair of shoes, a flat and straight chassis and two arc elbows; a connecting bar is fixedly arranged in the middle part on the lower bottom of the chassis, and four corners on the lower bottom of the chassis are respectively and fixedly provided with a floating drum; the two elbows are connected onto the connecting bar, a starting end of the two elbows extends to be provided with a circular flared opening, a first flange is arranged outside the end part of the circular flared opening, a rolling bearing A is sleeved inside the first flange, the rolling bearing A is in socket connection with one end of a water inlet pipe, a rolling bearing B is also sleeved outside the water inlet pipe, and a water inlet hose is fixedly sleeved on the outer wall of the water inlet pipe; and each elbow is divided into a front section and a tail section from the middle part, the wall of the tail-section pipe is provided with a water distribution pipe, and a water distribution hose is fixedly sleeved outside the water distribution pipe. When the aircraft is matched with a motorboat to use, the aircraft can fly away from the water for multiple meters, so that safety, excitingness and interestingness can be realized, simplicity in operation is realized, and novelty and fun can also be realized.
Description
Technical field
The utility model relates to the aquatic sports equipment, and aircraft is used in particularly a kind of aquatic sports.
Background technology
Existing aquatic sports equipment comprises motor boat, surfboard, surfboard, windsurfing, kite plate etc., though multifarious; Have their own characteristics each, but at present on the market, also have no a kind of aquatic sports equipment; Can make the user that low distance flies away from the water surface; Experience aeromarine enjoyment, this be really one bigger sorry and blank, remain people to go to fill up and develop innovation.
The utility model content
The technical matters that the utility model will solve provides a kind of aquatic sports and uses aircraft, when being used with motor boat, can fly away from the height of water surface number meter, safety, stimulation, interesting, and can control heading flexibly, simple to operate, very novel joyful.
For solving the problems of the technologies described above; The technical scheme of the utility model is: the overwater flight device that a kind of usefulness of travelling is provided; It comprises the manual spray gun that the foot control ejection assemblies is identical with two, and the foot control ejection assemblies comprises a pair of shoes, the straight chassis circular arc bend pipe identical with two, and every manual spray gun includes the J-shaped bend pipe; Its straight-tube portion is with the arm cover outward, and arm cover below is provided with and the vertical handle that links to each other of straight-tube portion; A pair of shoes is connected in the surface on chassis at interval, and the engaging of going to the bottom on chassis has the cooresponding bottom of 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 the connecting strap, and reverse each other the stretching, extension, and the initiating terminal of the two links to each other side by side and be one-body molded; And be extended with circular enlarging, and be provided with first flange outside the end of circular enlarging, be socketed with the A antifriction-bearing box in first flange; One end socket of A antifriction-bearing box and coolant inlet pipe; Be with the B antifriction-bearing box near this end is also outer on the coolant inlet pipe outer wall, on the coolant inlet pipe outer wall between A antifriction-bearing box and the B antifriction-bearing box, be provided with the flange that makes the two space; The B antifriction-bearing box is with the adapter sleeve ring outward, is fixedly linked between the end face of the connection collar and first flange; 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 links to each other with water jet nozzle on the motor boat; Every bend pipe therefrom partly is two sections of head and the tail all, and the coupling end that these head and the tail are two sections is provided with corresponding bonded assembly second flange, the 3rd flange outward respectively, wherein is socketed with the C antifriction-bearing box in second flange, and the coupling end that said bend pipe is first section is socketed in the C antifriction-bearing box; The rear tube wall of every bend pipe is equipped with the distributive pipe vertical with tube wall near mouth of pipe place, and the distributive pipe external fixation is with the branch water tube hose, divides the bent tube section end of the other end fixed jacket of water tube hose at the J-shaped bend pipe.
Aircraft is used in aforesaid aquatic sports, every footwear all through bolt pass sole with connecting strap and chassis, be fixedly linked with connecting strap.
Aircraft is used in aforesaid aquatic sports, in the gap of chassis and bottom and in each buoyancy tube, all is filled with foam
Aircraft is used in aforesaid aquatic sports, on corresponding second flange, the 3rd flange, is equipped with cooresponding flat position on every bend pipe, between the flat position and connecting strap of second flange, links to each other through bolt, so that two bend pipes are captiveed joint with the chassis.
Aircraft is used in aforesaid aquatic sports, and the surface of each C antifriction-bearing box is equipped with the anti-oil sealing that leaks.
Aircraft is used in above-mentioned aquatic sports, because when being used with motor boat, can be through the powerful reaction thrust of two bend pipe water sprays generation; Make the user fly away from the height of water surface number meter, when falling because chassis and buoyancy tube with the buoyancy of foam, the user can float on the surface and can submerged; Safety, stimulation, interesting, and can control heading flexibly through the water spraying direction of two bend pipes of conversion and manual spray gun; Simple to operate, very novel joyful, as long as training a little; On top of method of operation is fit to widely popularize to vast aquatic sports fan very much.
Description of drawings
Below in conjunction with the accompanying drawing and the specific embodiment the utility model is done further detailed explanation.
Block diagram when Fig. 1 does not install buoyancy tube for said utility model;
Split figure when Fig. 2 does not install buoyancy tube for the foot control ejection assemblies;
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 running condition scheme drawing of said utility model.
The specific embodiment
Referring to Fig. 1, Fig. 2, provide a kind of aquatic sports to use aircraft, it comprises the manual spray gun 2 that foot control ejection assemblies 1 is identical with two; Foot control ejection assemblies 1 comprises a pair of shoes 3, the straight chassis 4 circular arc bend pipe 5 identical with two, and a pair of shoes 3 is connected in the surface on chassis 4 at interval, and the engaging of going to the bottom on chassis 4 has the cooresponding bottom 9 of shape with it; The middle part of going to the bottom on chassis 4 is fixed with 10, two bend pipes 5 of connecting strap and is connected on the connecting strap 10, and reverse each other the stretching, extension; The initiating terminal of the two links to each other side by side and is one-body molded; And be extended with circular enlarging 12, be provided with outside the end of circular enlarging 12 in first flange, 13, the first flanges 13 and be socketed with A antifriction-bearing box 14; One end socket of A antifriction-bearing box 14 and coolant inlet pipe 15; Be with B antifriction-bearing box 16 near this end is also outer on coolant inlet pipe 15 outer walls, on coolant inlet pipe 15 outer walls between A antifriction-bearing box 14 and the B antifriction-bearing box 16, be provided with the flange 17 that makes the two space; The B antifriction-bearing box 16 outer adapter sleeve rings 18 that are with are fixedly linked between the end face of the connection collar 18 and first flange 13; 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 links to each other with water jet nozzle on the motor boat.Since 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 direction all free to rotate, and can not cause inlet water hose 19 knottings, thus can guarantee that current get into inlet water hose 19 swimmingly.Owing to be fixedly linked between the end face of the connection collar 18 and first flange 13; Coolant inlet pipe 15 is kept being actively socketed in A antifriction-bearing box 14 and the B antifriction-bearing box 16 and can not deviate from, can avoid the current in the coolant inlet pipe 15 from the socket slit of coolant inlet pipe 15 and bearing, to overflow simultaneously.
Referring to Fig. 1-Fig. 3, every manual spray gun 2 includes J-shaped bend pipe 6, and its straight-tube portion is with arm cover 7 outward, and arm overlaps 7 belows and is provided with and the vertical handle that links to each other 8 of straight-tube portion; Every bend pipe 5 all therefrom partly is two sections of head and the tail; Two sections coupling end of these head and the tail, outer respectively corresponding bonded assembly second flange 20, the 3rd flange 21 of being provided with wherein is socketed with C antifriction-bearing box 22 in second flange 20; The coupling end that said bend pipe is 5 first sections is socketed in the C antifriction-bearing box 22; The rear tube wall of every bend pipe 5 is equipped with the distributive pipe vertical with tube wall 23 near mouth of pipe place, and distributive pipe 23 external fixation are with branch water tube hose 24, divides the bent tube section end of the other end fixed jacket of water tube hose 24 at J-shaped bend pipe 6.
Referring to Fig. 1, Fig. 2, every footwear 3 all through bolt pass sole with connecting strap 25 and chassis 4, be fixedly linked with connecting strap 10.On every bend pipe 5 on corresponding second flange 20, the 3rd flange 21, continuous between the flat position 26 that is equipped with cooresponding flat position 26, the second flanges 20 and the connecting strap 10 through bolt, so that two bend pipes 5 are captiveed joint with chassis 4.
Referring to Fig. 1-Fig. 4, during use, the user is inserted in both feet in the footwear 3; Both hands from the bent tube section place direction of two J-shaped bend pipes 6, stretch among two arm covers 7 respectively, make to be enclosed within two forearms in two arm covers 7; Both hands stretch out catches two handles 8 respectively, can begin flight operation.Powerful current spray from the water jet nozzle on the motor boat, flow into two bend pipes 5 in 15 minutes through inlet water hose 19, coolant inlet pipe, and the tail end from two bend pipes 5 sprays downwards then; Thereby produce antagonistic force upwards, can carry the weight about 150KG, make the related whole aircraft of human body fly away from the height of water surface number meter; Concrete flies away from highly, decides with the pump power of motor boat, and pump power is big more; Fly away from greatly highly more, vice versa.Simultaneously, current get into two distributive pipes 23, divide water tube hose 24, get into the J-shaped bend pipe 6 of two manual spray guns 2 then, and spray from the mouth of pipe of its straight-tube portion, and the water spraying direction of the manual spray gun 2 of user's conversion can play the effect of regulating total balance of the body.
When needing the fore-and-aft direction of conversion flight, the user shifts to forefoot with centre of body weight, promptly tramples chassis 4 with forefoot; Because chassis 4 and connecting strap 10, second flange 20, C antifriction-bearing box 22 are connected in succession, the coupling end that two bend pipes are 5 first sections can pass through the rotation of two C antifriction-bearing boxs 22 respectively; Clockwise rotate; Simultaneously two second flanges 20 rotate with cooresponding C antifriction-bearing box 22 respectively, because two the 3rd flanges 21 link to each other with the rear of two second flanges 20, two bend pipes 5 respectively, thereby the rear of also related two bend pipes 5 of the 3rd flange 21 rotates simultaneously again; Article two, the tail end of bend pipe 5 promptly squints to the user after one's death; 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.At this moment, the user simultaneously can also play the booster action that promotion is flown forward with J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards after one's death.Otherwise when needs flew backward, the user shifted to hind paw with centre of body weight; Promptly trample chassis 4 with hind paw, in like manner, the coupling end that two bend pipes are 5 first sections; Can rotate counterclockwise respectively through the rotation of two C antifriction-bearing boxs 22, two second flanges 20 rotate with cooresponding C antifriction-bearing box 22 respectively simultaneously; The rear of also related two bend pipes 5 of the 3rd flange 21 rotates simultaneously, and the tail end of two bend pipes 5 promptly squints to user the place ahead, and promptly 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.At this moment, the user simultaneously can also play the booster action that promotion is flown backward with J-shaped bend pipe 6 water injectors of two manual spray guns 2 towards health the place ahead.
When needing the left and right directions of conversion flight; The user shifts to the left foot palm with centre of body weight; Be that health is left-leaning and promptly squint to the user right side with the tail end that the left foot palm is trampled 4, two bend pipes 5 in chassis, promptly 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 with 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; With the person centre of body weight is shifted to the right crus of diaphragm palm; Be the health Right deviation and promptly squint that promptly its water spraying direction is by on the left of the vertical duction user to the user left side with the tail end that the right crus of diaphragm palm is trampled 4, two bend pipes 5 in chassis; Thereby produce antagonistic force to the right, the related whole aircraft of human body is flown to the right; Simultaneously, the user can be with 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 flew away from the water surface and falls then, because the buoyancy of foam, the user can float on the surface and can submerged, and was as safe as a house.
Referring to Fig. 3, the surface of each C antifriction-bearing box 22 is equipped with the anti-oil sealing 27 that leaks, can prevent that current from getting into bend pipe 5 after, from the connection slit of two sections of bend pipe 5 head and the tail, spill, can avoid the antagonistic force of current to be weakened.
The foregoing description is the preferred embodiment of the utility model, and all and the similar structure of the utility model and the equivalence of being done change, and all should belong to the protection category of the utility model.
Claims (5)
1. aircraft is used in an aquatic sports; It is characterized in that: it comprises the manual spray gun (2) that foot control ejection assemblies (1) is 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 manual spray gun (2) includes J-shaped bend pipe (6), and its straight-tube portion is with arm cover (7) outward, and arm cover (7) below is provided with and the vertical handle that links to each other of straight-tube portion (8); A pair of shoes (3) is connected in the surface of chassis (4) at interval; The engaging of going to the bottom on chassis (4) has the cooresponding bottom of shape (9) 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 the connecting strap (10); And reverse each other the stretching, extension, the initiating terminal of the two links to each other side by side and is one-body molded, and is extended with circular enlarging (12); Be provided with first flange (13) outside the end of circular enlarging (12); Be socketed with A antifriction-bearing box (14) in first flange (13), an end socket of A antifriction-bearing box (14) and coolant inlet pipe (15) also is with B antifriction-bearing box (16) outward near this end on coolant inlet pipe (15) outer wall; On coolant inlet pipe (15) outer wall between A antifriction-bearing box (14) and the B antifriction-bearing box (16); Be provided with the flange (17) that makes the two space, the outer adapter sleeve ring (18) that is with of B antifriction-bearing box (16) is fixedly linked between the end face of the connection collar (18) and first flange (13); 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) links to each other with water jet nozzle on the motor boat; Every bend pipe (5) all therefrom partly is two sections of head and the tail; The coupling end that these head and the tail are two sections; Outer respectively corresponding bonded assembly second flange (20), the 3rd flange (21) of being provided with; Wherein be socketed with C antifriction-bearing box (22) in second flange (20), the coupling end that said bend pipe (5) is first section is socketed in the C antifriction-bearing box (22); The rear tube wall of every bend pipe (5) is equipped with the distributive pipe vertical with tube wall (23) near mouth of pipe place, and distributive pipe (23) external fixation is with branch water tube hose (24), divides the bent tube section end of the other end fixed jacket of water tube hose (24) at J-shaped bend pipe (6).
2. aircraft is used in 1 described aquatic sports according to right, it is characterized in that: every footwear (3) all through bolt pass sole with connecting strap (25) and chassis (4), be fixedly linked with connecting strap (10).
3. aircraft is used in 1 described aquatic sports according to right, 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. aircraft is used in 1 described aquatic sports according to right; It is characterized in that: every bend pipe (5) is gone up on corresponding second flange (20), the 3rd flange (21); Be equipped with cooresponding flat position (26); Between the flat position (26) and connecting strap (10) of second flange (20), link to each other through bolt, so that two bend pipes (5) are captiveed joint with chassis (4).
5. aircraft is used in 1 described aquatic sports according to right, it is characterized in that: the surface of each C antifriction-bearing box (22) is equipped with the anti-oil sealing (27) that leaks.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012202263760U CN202593816U (en) | 2012-05-18 | 2012-05-18 | Aircraft for water sports |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012202263760U CN202593816U (en) | 2012-05-18 | 2012-05-18 | Aircraft for water sports |
Publications (1)
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CN202593816U true CN202593816U (en) | 2012-12-12 |
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CN2012202263760U Expired - Lifetime CN202593816U (en) | 2012-05-18 | 2012-05-18 | Aircraft for water sports |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103231784A (en) * | 2013-04-06 | 2013-08-07 | 周良勇 | Airship capable of hovering and travelling above water surface |
CN103419907A (en) * | 2012-05-18 | 2013-12-04 | 李钜彬 | Flight vehicle for water sports |
CN103661832A (en) * | 2013-10-12 | 2014-03-26 | 浙江定川机电制造有限公司 | Pedal type water flying device |
CN104097754A (en) * | 2013-04-06 | 2014-10-15 | 周良勇 | Airship |
KR101467980B1 (en) * | 2013-09-27 | 2014-12-02 | 주식회사 유엔아이 | the fly board with leisure for with high stability |
CN106573165A (en) * | 2014-03-05 | 2017-04-19 | 扎帕塔控股公司 | Device and system for propelling a passenger |
CN113247255A (en) * | 2021-06-02 | 2021-08-13 | 浙江工业大学 | Low-altitude run-up boot type aircraft |
-
2012
- 2012-05-18 CN CN2012202263760U patent/CN202593816U/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103419907A (en) * | 2012-05-18 | 2013-12-04 | 李钜彬 | Flight vehicle for water sports |
CN103419907B (en) * | 2012-05-18 | 2015-12-16 | 李钜彬 | Aquatic sports aircraft |
CN103231784A (en) * | 2013-04-06 | 2013-08-07 | 周良勇 | Airship capable of hovering and travelling above water surface |
CN104097754A (en) * | 2013-04-06 | 2014-10-15 | 周良勇 | Airship |
KR101467980B1 (en) * | 2013-09-27 | 2014-12-02 | 주식회사 유엔아이 | the fly board with leisure for with high stability |
CN103661832A (en) * | 2013-10-12 | 2014-03-26 | 浙江定川机电制造有限公司 | Pedal type water flying device |
CN106573165A (en) * | 2014-03-05 | 2017-04-19 | 扎帕塔控股公司 | Device and system for propelling a passenger |
CN113247255A (en) * | 2021-06-02 | 2021-08-13 | 浙江工业大学 | Low-altitude run-up boot type aircraft |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20121212 Effective date of abandoning: 20151216 |
|
C25 | Abandonment of patent right or utility model to avoid double patenting |