CN202863765U - Water aircraft - Google Patents
Water aircraft Download PDFInfo
- Publication number
- CN202863765U CN202863765U CN 201220410634 CN201220410634U CN202863765U CN 202863765 U CN202863765 U CN 202863765U CN 201220410634 CN201220410634 CN 201220410634 CN 201220410634 U CN201220410634 U CN 201220410634U CN 202863765 U CN202863765 U CN 202863765U
- Authority
- CN
- China
- Prior art keywords
- water
- aircraft
- seat
- knapsack
- buoyancy chamber
- 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 - Fee Related
Links
Images
Landscapes
- Emergency Lowering Means (AREA)
- Portable Outdoor Equipment (AREA)
Abstract
The utility model discloses a water aircraft. The water aircraft is characterized by comprising a buoyancy chamber, a knapsack device, a seat, a water knockout vessel and an operating handle, wherein a power system and a water pump system are arranged inside the buoyancy chamber; the seat, the water knockout vessel and the operating handle are arranged on the knapsack device; and the knapsack device is connected with the buoyancy chamber through a hose. Compared with the prior art, the water aircraft has the advantages that the effect of upward and forward parallel movement is achieved by counter-acting force generated by downward and backward high-pressure jet water bodies of two nozzles of balancing devices at the left and right edges; and the noise generated by a jet aircraft to the environment is overcome, so that the water aircraft is environment-friendly; and an injury on a human body which is caused by high heat generated by the jet aircraft is avoided. Therefore, the water aircraft is safe.
Description
Technical field
The utility model relates to manned craft, is specifically related to a kind of overwater flight device.
Background technology
Since ancient times, human just by self effort and developing, the flight tools such as manufacturing kite and fire balloon are pursued great flight dream, these simple manual blanks that aircraft has just been achieved in making of making.
In the centuries backward, countless flight pioneers constantly makes great efforts to attempt flight, U.S. Lai Te brother drives and for the first time dynamicly, manned, lasting, stable and exercisable on the human history overweights successfully going up to the air first, flying of air aircraft in December, 1903, indicates that the dream of human the conquest of air begins to come true.
People did not stop step to the research of aircraft, and in the after this time of decades, aircraft has moved towards the battlefield from the laboratory, just made it be able to develop rapidly because of afield application; And then be applied to civil aviaton afterwards, its effect is developed.
In the development aeronautical technology, human in order to satisfy the needs of Science Explorations, increasing makes aircraft research enter the brand-new epoch to the research of space technology.
Human when constantly realizing the flying apsaras dream, also constantly seeking new flying apsaras pattern.Along with people to healthy pursuit, to the ardent hope of stimulus to the sense organ and spiritual happiness degree, original aircraft since cost high, particularly in the flight course, human limb's degree of participation is low, can't realize the train on that improves the health at all.
The utility model content
The utility model is in order to solve above-mentioned deficiency, a kind of overwater flight device to be provided.
Above-mentioned purpose of the present utility model realizes by following technical scheme: a kind of overwater flight device, it is characterized in that: comprise buoyancy module, knapsack device, seat, water-segregator and joystick, described buoyancy module internally-powered system and water pump system, described seat, water-segregator and joystick are installed on the knapsack device, and described knapsack device is connected with buoyancy module by flexible pipe.
Described knapsack device is provided with safety belt.
Described seat is provided with seat adjustment device.
The utility model advantage compared with prior art is: the utility model with two nozzles of left and right both sides balancing device downwards, the antagonistic force that produces of high-pressure injection water body backward, realize upwards, the effect of parallel forward, it has overcome the noise that jet-propelled aircraft produces environment, therefore more environmental protection; Avoided that jet-propelled aircraft produces that high heat may cause to the human injury, therefore safer.
Description of drawings
Fig. 1 is structural representation of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is described in further detail:
As shown in Figure 1, a kind of overwater flight device, it is characterized in that: comprise buoyancy module 1, knapsack device 2, seat 3, water-segregator 4 and joystick 5, described buoyancy module 1 internally-powered system 11 and water pump system 12, described seat 3, water-segregator 4 and joystick 5 are installed on the knapsack device 2, and described knapsack device 2 is connected with buoyancy module 1 by flexible pipe 6.
Described knapsack device 2 is provided with safety belt 7; Described seat 3 is provided with seat adjustment device 8.
The above only is embodiment of the present utility model; be not so limit claim of the present utility model; every equivalent structure or equivalent flow process conversion that utilizes the utility model specification sheets and accompanying drawing content to do; or directly or indirectly be used in other relevant technical fields, all in like manner be included in the scope of patent protection of the present utility model.
Claims (3)
1. overwater flight device, it is characterized in that: comprise buoyancy module, knapsack device, seat, water-segregator and joystick, described buoyancy module internally-powered system and water pump system, described seat, water-segregator and joystick are installed on the knapsack device, and described knapsack device is connected with buoyancy module by flexible pipe.
2. a kind of overwater flight device according to claim 1, it is characterized in that: described knapsack device is provided with safety belt.
3. a kind of overwater flight device according to claim 1, it is characterized in that: described seat is provided with seat adjustment device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220410634 CN202863765U (en) | 2012-08-12 | 2012-08-12 | Water aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220410634 CN202863765U (en) | 2012-08-12 | 2012-08-12 | Water aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202863765U true CN202863765U (en) | 2013-04-10 |
Family
ID=48030507
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220410634 Expired - Fee Related CN202863765U (en) | 2012-08-12 | 2012-08-12 | Water aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202863765U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743113A (en) * | 2015-03-13 | 2015-07-01 | 河南摩西机械制造有限公司 | Hydrodynamic unmanned machine |
| CN107982933A (en) * | 2017-12-19 | 2018-05-04 | 刘淑敏 | A kind of manned plane simulation aerocraft system of amusement on water |
| WO2021051816A1 (en) * | 2019-09-20 | 2021-03-25 | 山东理工大学 | Movable operating platform for paddy field |
-
2012
- 2012-08-12 CN CN 201220410634 patent/CN202863765U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743113A (en) * | 2015-03-13 | 2015-07-01 | 河南摩西机械制造有限公司 | Hydrodynamic unmanned machine |
| CN107982933A (en) * | 2017-12-19 | 2018-05-04 | 刘淑敏 | A kind of manned plane simulation aerocraft system of amusement on water |
| CN107982933B (en) * | 2017-12-19 | 2019-10-25 | 上海昕鼎网络科技有限公司 | A kind of manned plane simulation aerocraft system of amusement on water |
| WO2021051816A1 (en) * | 2019-09-20 | 2021-03-25 | 山东理工大学 | Movable operating platform for paddy field |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Siddall et al. | Fast aquatic escape with a jet thruster | |
| EP2548802A3 (en) | Aircraft versatile power system | |
| CN202863765U (en) | Water aircraft | |
| WO2012125052A3 (en) | Airborne platform | |
| Siddall et al. | A water jet thruster for an aquatic micro air vehicle | |
| CN104340292A (en) | Wheel-leg dual-purpose shape shifting robot | |
| CN104432658A (en) | Flying suit | |
| CN203844993U (en) | Dual-purpose electric power thruster for underwater diving of single person | |
| CN203958610U (en) | Twin-inlet Hypersonic waveriders aircraft device | |
| CN106741905B (en) | A kind of dedicated Vertical Lift manned vehicle model in boat paradise | |
| CN104679933A (en) | Airplane fatigue load designing method | |
| CN202863773U (en) | Control device of overwater air vehicle | |
| CN202491923U (en) | Jet-propelled parachute | |
| CN202863766U (en) | Knapsack device of water aircraft | |
| Hudson et al. | Bio-inspired jumping maneuver for launching flapping wing micro air vehicles | |
| CN203666970U (en) | Driving connecting structure for aileron of unmanned aerial vehicle | |
| CN204056275U (en) | A kind of foot-operated overwater flight device | |
| CN103112580A (en) | Balloon flying machine | |
| CN202863764U (en) | Buoyancy chamber of water aircraft | |
| CN106516149A (en) | Electromagnetic aircraft launch system and method | |
| CN204066564U (en) | There is the aircraft carrier model of submarine function | |
| CN202863769U (en) | Composite structure of overwater air vehicle seat and pedal device | |
| 동희김 et al. | Dynamic modeling and motion analysis of unmanned underwater gliders with mass shifter unit and buoyancy engine | |
| CN206345022U (en) | Aircraft electromagnetic ejection system | |
| CN202470899U (en) | Military portable rapid deception device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130410 Termination date: 20130812 |