CN203318067U - Water and sky two-purpose vertical crossing navigating device - Google Patents
Water and sky two-purpose vertical crossing navigating device Download PDFInfo
- Publication number
- CN203318067U CN203318067U CN2012206197984U CN201220619798U CN203318067U CN 203318067 U CN203318067 U CN 203318067U CN 2012206197984 U CN2012206197984 U CN 2012206197984U CN 201220619798 U CN201220619798 U CN 201220619798U CN 203318067 U CN203318067 U CN 203318067U
- Authority
- CN
- China
- Prior art keywords
- water
- aircraft
- underwater
- cross frame
- electronic governor
- 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
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
The utility model belongs to the technical field of novel navigating device design and manufacture and provides a water and sky two-purpose vertical crossing navigating device which comprises a layered cross support, an air power device, an underwater power device, an electric speed regulator, a remote control receiver and a remote controller. The navigating device is greater than water in intensity, controls push force when entering the water, gradually lowers the speed and is slowly contacted with the water, so as to reduce damage caused by water impact; the navigating device automatically switches off power after being contacted with the water, is immersed in the water via self gravitation, and keeps an underwater navigating state after starting an underwater propeller; when exposed out of the water, the navigating device adopts dual-layer power to push out of the water. The water and sky two-purpose vertical crossing aircraft has repeated interface crossing capability and the capability to continuously navigate on multiple mediums, has advantages of no need of auxiliary equipment and repetitious use, and has higher popularization and application value.
Description
Technical field
The utility model belongs to new ideas aircraft design and manufacture technical field, relates in particular to the empty dual-purpose vertical leap aircraft of a kind of water.
Background technology
2008, U.S. national defense pioneering technology research office (DARPA) sets about researching and developing a kind of can either flight aloft, again can be at the new ideas aircraft of the water surface and submarine navigation---" diving aircraft ", be specifically designed to the special operations action of surprise attack enemy seashore, the diving aircraft be a class can be aloft, the composite of the water surface and the operation under water aircraft of entirely dwelling.
In July, 2010, according to Britain's the Daily Telegraph newspaper, " flight submarine " prepared to manufacture by the Pentagon, and it can navigate by water under water as submarine, flies in the sea of jumping out again as aircraft.Report, this plan is at present in concept phase, several outside research group has submitted design to, and Advanced Research Projects office of Department of Defense (DOD) can start the distribution of fund to the researchist in 1 year, on this message newspaper " Reference News " at home, reprinted.
This proposition that is called the new ideas aircraft of diving aircraft or flight submarine has caused great attention at once at home, has especially caused military strategy expert's concern.
Still there do not is at present the mature technology that can support the empty dual-purpose aircraft of water, the empty dual-purpose aircraft Flight Test of manque water yet.And, with the empty dual-purpose aircraft of water, compare, more existing aircraft can be crossed over medium by single, comprise that single completes interface-under water in the air and crosses over aircraft, as aerial torpedo, warship are penetrated anti-submarine guided missle, complete under water-air-interface of single is crossed over aircraft as submarine-launched ballistic missile, submarine launched cruise missile, the latent unmanned plane of penetrating.But they do not possess repeatedly interface span ability and the lasting navigation ability in a plurality of media.
Single across the relevant situation of medium aircraft type as shown in form:
| ? | Cross over interface type | Airflight speed | Integrated mode |
| Aerial torpedo | In the air-under water | Low speed | Torpedo+deceleration parachute/be not with umbrella |
| Warship is penetrated anti-submarine guided missle | In the air-under water | Subsonic | Torpedo+booster rocket or turbojet engine |
| Submarine launched missile | Under water-aerial | Subsonic/hyprsonic | Anti-warship guided missle+underwater research vehicle |
| Dive and penetrate unmanned plane | Under water-aerial | Subsonic/hyprsonic | Unmanned plane+underwater research vehicle |
But these singles are crossed over the aircraft of the empty medium of water and all can only be realized on function in the air-under water or under water-aerial span ability, all need the accessory equipments such as vehicle or retarder on operation technique, these equipment all are abandoned after crossing over, this be also restriction its can only the single leap key factor.
The utility model content
The utility model provides a kind of water empty dual-purpose vertical leap aircraft, being intended to solve more existing aircraft is merely able to carry out single and passes through medium, and on operation technique, all need vehicle or retarder as accessory equipment, do not possess repeatedly the problem of interface span ability and the lasting navigation ability in a plurality of media.
The purpose of this utility model is to provide a kind of water empty dual-purpose vertical leap aircraft, and this aircraft comprises: layering cross frame, air generation plants, underwater power pack, electronic governor, receiver of remote-control sytem, remote controller.
The upper strata of described layering cross frame is equipped with described air generation plants, the lower floor of described layering cross frame is equipped with described underwater power pack, described air generation plants and underwater power pack are connected with described receiver of remote-control sytem by described electronic governor, described receiver of remote-control sytem is arranged on the upper end of described layering cross frame, and described receiver of remote-control sytem and described remote controller carry out wireless telecommunications.
Further, described electronic governor also is connected with battery pack, and described battery pack is arranged on the lower end of described layering cross frame.
Further, described air generation plants comprises: upper strata crosswise support, air screw; The upper strata of layering cross frame is equipped with described upper strata crosswise support, on the crosswise support of described upper strata, four air screws is installed, and described air screw is connected with electronic governor.
Further, each air screw is equipped with an electronic governor.
Further, described underwater power pack comprises: lower floor's crosswise support, underwater propeller; The upper strata of layering cross frame is equipped with described lower floor crosswise support, on described lower floor crosswise support, four underwater propellers is installed, and described underwater propeller is connected with electronic governor.
Further, each underwater propeller is equipped with an electronic governor.
The empty dual-purpose vertical leap aircraft of the water that the utility model provides, by the layering cross frame, air generation plants, underwater power pack, electronic governor, receiver of remote-control sytem and remote controller form, aircraft design density is greater than water, progressively reduce the rotating speed of air generation plants while entering water, the shock infringement of minimizing to aircraft, close air generation plants after touching water, rely on the aircraft self gravitation not have upstream face, restart underwater propeller and enter the submerge state, during the aircraft water outlet, adopt two-layer power relay to advance water outlet, possess repeatedly interface span ability and the lasting navigation ability in a plurality of media, have and do not need accessory equipment and reusable advantage, having stronger propagation and employment is worth.
The accompanying drawing explanation
Fig. 1 is the structural representation of the empty dual-purpose vertical leap aircraft of the water that provides of the utility model embodiment;
Fig. 2 is the structural representation of the air generation plants that provides of the utility model embodiment;
Fig. 3 is the structural representation of the underwater power pack that provides of the utility model embodiment;
Fig. 4 is the principle schematic that two-layer power relay that the utility model embodiment provides advances the aircraft water outlet;
Fig. 5 is the principle of work structured flowchart of the empty dual-purpose vertical leap aircraft of the water that provides of the utility model embodiment.
In figure: 1, layering cross frame; 2, air generation plants; 21, upper strata crosswise support; 22, air screw; 3, underwater power pack; 31, lower floor's crosswise support; 32, underwater propeller; 4, electronic governor; 5, receiver of remote-control sytem; 6, remote controller; 7, battery pack; 8, twist-lock device.
The specific embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the utility model is described in further detail.Should be appreciated that specific embodiment described herein is only in order to explain the utility model, and be not used in the restriction utility model.
Fig. 1 and Fig. 5 show the structure of the empty dual-purpose vertical leap aircraft of water that the utility model embodiment provides.For convenience of explanation, only show the part relevant to the utility model.
This aircraft comprises: layering cross frame 1, air generation plants 2, underwater power pack 3, electronic governor 4, receiver of remote-control sytem 5, remote controller 6;
The upper strata of layering cross frame 1 is equipped with air generation plants 2, the lower floor of layering cross frame 1 is equipped with underwater power pack 3, air generation plants 2 and underwater power pack 3 are connected with receiver of remote-control sytem 5 by electronic governor 4, receiver of remote-control sytem 5 is arranged on the upper end of layering cross frame 1, and receiver of remote-control sytem 5 carries out wireless telecommunications with remote controller 6.
In the utility model embodiment, the concrete function of each several part is as follows:
1) main structure body that layering cross frame 1 is aircraft, hierarchical layout's design is to realize that relay advances the framework basis of water outlet;
2) air generation plants 2 is air screw, for pulling force aloft is provided;
3) underwater power pack 3 is the water screw propeller, for thrust is provided under water;
4) electronic governor 4 is for controlling the horsepower output of screw propeller motor, and then controls the push/pull of rotating speed and generation;
5) energy parts that battery pack is aircraft, for engine installation provides electric power;
6) the gyroscopic equilibrium instrument is for controlling the flight attitude of aircraft;
7) remote controller equipment is controlled action and the attitudes such as flight, submerge and leap of aircraft for teacher of the controlling.
In the utility model embodiment, electronic governor 4 also is connected with battery pack 7, and battery pack 7 is arranged on the lower end of layering cross frame 1.
As shown in Figure 2, in the utility model embodiment, air generation plants 2 comprises: upper strata crosswise support 21, air screw 22; The upper strata of layering cross frame 1 is equipped with upper strata crosswise support 21, and four air screws 22 are installed on upper strata crosswise support 21, and air screw 22 is connected with electronic governor 4.
In the utility model embodiment, each air screw 22 is equipped with an electronic governor 4.
As shown in Figure 3, in the utility model embodiment, underwater power pack 3 comprises: lower floor's crosswise support 31, underwater propeller 32; The upper strata of layering cross frame 1 is equipped with lower floor's crosswise support 31, and four underwater propellers 32 are installed on lower floor's crosswise support 31, and underwater propeller 32 is connected with electronic governor 4.
In the utility model embodiment, each underwater propeller 32 is equipped with an electronic governor 4.
In the utility model embodiment, this aircraft design density is greater than water, progressively reduces the rotating speed of air generation plants 2 while entering water, close air generation plants 2 after touching water, rely on self gravitation not have upstream face, restart underwater power pack 3, aircraft enters the submerge state.
As shown in Figure 4, in the utility model embodiment, before aircraft is prepared water outlet, improve horsepower output, accelerate to rise; When aircraft approaches the water surface, air generation plants 2 quits work, and promotes aircraft by underwater power pack 3 and rises; After air generation plants 2 leaves the water surface, with the underwater power pack 3 steady steaming device that works together; Underwater power pack 3 quits work when approaching the water surface, and the power of aircraft flight is provided separately by air generation plants 2; After aircraft is pulled out the water surface, remote controller 6 is adjusted the rotating speed of air generation plants 2 by electronic governor 4, and aircraft flies before tilting.
In the utility model embodiment, in air generation plants 2 and underwater power pack 3, the screw propeller design of the position that is separated by is retrograde rotation, prevents twist moment.
Below in conjunction with drawings and the specific embodiments, application principle of the present utility model is further described.
As shown in Figures 1 and 5, layering cross frame 1 upper strata is provided with upper strata crosswise support 21, and lower floor is designed with lower floor's crosswise support 31; Crosswise support 21 ends, upper strata are provided with air screw 22, on each support of upper strata crosswise support 21, are provided with electronic governor 4; Lower floor's crosswise support 31 ends are provided with underwater propeller 32, in the middle of each support of lower floor's crosswise support 31, are provided with electronic governor 4; Layering cross frame 1 upper end is provided with receiver of remote-control sytem 5, and lower end is provided with battery pack 7.
The empty dual-purpose vertical leap aircraft of a kind of water in this example, mainly by air screw 22, electronic governor 4, receiver of remote-control sytem 5, layering cross frame 1, battery pack 7, underwater propeller 32, upper strata crosswise support 21, lower floor's crosswise support 31 forms, the layering cross frame is the two-layer upper strata crosswise support 21 that is provided with Shang Xia 1, lower floor's crosswise support 31, at upper strata crosswise support 21, the end of lower floor's crosswise support 31 is installed respectively 4 air screws 22 and underwater propeller 32, be provided with electronic governor 4 in the middle of each support, electronic governor 4 by control linkage air screw 22 and underwater propeller 32 is adjusted propeller speed, control navigation direction and the speed of aircraft.
The empty dual-purpose vertical leap aircraft of a kind of water in this example, aircraft design density is greater than water, progressively reduce the rotating speed of air screw 22 while entering water, and then infringement is clashed in the minimizing that underspeeds, close air generation plants 2 after touching water, rely on self gravitation not have upstream face, then start underwater propeller 32 and enter the submerge state.
During water outlet, the two-layer power relay of employing advances water outlet, and main process is: before preparing water outlet, improve horsepower output, accelerate to rise; The air screw 22 that is positioned at upper strata while approaching the water surface quits work, and by the underwater propeller 32 that is positioned at lower floor, is promoted to rise; After air screw 22 leaves the water surface, with the underwater propeller 32 steady steaming device that works together; Lower floor's underwater propeller 32 quits work when approaching the water surface, by upper strata air screw 22, provides separately pulling force; After aircraft is pulled out to the water surface, by electronic governor 4, adjust the rotating speed that outgoing current changes air screw 22, make to fly before the aircraft inclination.
The empty dual-purpose vertical leap aircraft of a kind of water that the utility model provides, design architecture is divided into two-layer up and down, air generation plants 2 and underwater power pack 3 are set respectively, adopt under water and stablize lasting thrust with the relay mode of aerial power for media span provides, every layer of dynamic design is four screw propellers, the position screw propeller design of being separated by is retrograde rotation, prevent the aircraft spin, this aircraft is the low speed landing water surface steadily, relatively aerial torpedo relies on the disposable apparatus such as deceleration parachute and buffer cap, and having does not need accessory equipment and reusable advantage; Under water-air is crossed over the stage, rely on innovative design can independently realize crossing over, relatively latenter unmanned plane and the submarine launched missiles etc. penetrated can only pass through the empty medium of water by single, and the shortcoming that can't rely on self power to repeat to cross over the empty medium of water, filled up the design of the empty dual-purpose aircraft of water and developed blank.
The empty dual-purpose vertical leap aircraft of the water that the utility model embodiment provides, by layering cross frame 1, air generation plants 2, underwater power pack 3, electronic governor 4, receiver of remote-control sytem 5 and remote controller 6 form, aircraft design density is greater than water, progressively reduce the rotating speed of air generation plants 2 while entering water, the shock infringement of minimizing to aircraft, close air generation plants 2 after touching water, rely on the aircraft self gravitation not have upstream face, restart underwater propeller 32 and enter the submerge state, during the aircraft water outlet, adopt two-layer power relay to advance water outlet, possess repeatedly interface span ability and the lasting navigation ability in a plurality of media, have and do not need accessory equipment and reusable advantage, having stronger propagation and employment is worth.
These are only preferred embodiment of the present utility model, not in order to limit the utility model, all any modifications of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., within all should being included in protection domain of the present utility model.
Claims (6)
1. the empty dual-purpose vertical leap aircraft of water, is characterized in that, this aircraft comprises: layering cross frame, air generation plants, underwater power pack, electronic governor, lithium cell group, gyroscopic equilibrium instrument, receiver of remote-control sytem, remote controller;
The upper strata of described layering cross frame is equipped with described air generation plants, the lower floor of described layering cross frame is equipped with described underwater power pack, described air generation plants and underwater power pack are connected with described receiver of remote-control sytem by described electronic governor, described balanced gyroscope is connected with air screw, described receiver of remote-control sytem is arranged on the upper end of described layering cross frame, and described receiver of remote-control sytem and described remote controller carry out wireless telecommunications.
2. aircraft as claimed in claim 1, is characterized in that, described electronic governor also is connected with battery pack, and described battery pack is arranged on the lower end of described layering cross frame.
3. aircraft as claimed in claim 1, is characterized in that, described air generation plants further comprises: upper strata crosswise support, air screw; The upper strata of layering cross frame is equipped with described upper strata crosswise support, on the crosswise support of described upper strata, four air screws is installed, and described air screw is connected with electronic governor.
4. aircraft as claimed in claim 3, is characterized in that, each screw propeller is equipped with an electronic governor, can adjust rotating speed and then change force controlled navigation direction.
5. aircraft as claimed in claim 1, is characterized in that, described underwater power pack further comprises: lower floor's crosswise support, underwater propeller; The upper strata of layering cross frame is equipped with described lower floor crosswise support, on described lower floor crosswise support, four underwater propellers is installed, and described underwater propeller is connected with electronic governor.
6. aircraft as claimed in claim 5, is characterized in that, each underwater propeller is equipped with an electronic governor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012206197984U CN203318067U (en) | 2012-11-16 | 2012-11-16 | Water and sky two-purpose vertical crossing navigating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012206197984U CN203318067U (en) | 2012-11-16 | 2012-11-16 | Water and sky two-purpose vertical crossing navigating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203318067U true CN203318067U (en) | 2013-12-04 |
Family
ID=49657452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012206197984U Expired - Fee Related CN203318067U (en) | 2012-11-16 | 2012-11-16 | Water and sky two-purpose vertical crossing navigating device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203318067U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102963230A (en) * | 2012-11-16 | 2013-03-13 | 空军工程大学 | Water-air vertical crossing vehicle |
| CN106809397A (en) * | 2015-11-30 | 2017-06-09 | 黄鹏搏 | A kind of accelerator does the ROV of drive device |
-
2012
- 2012-11-16 CN CN2012206197984U patent/CN203318067U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102963230A (en) * | 2012-11-16 | 2013-03-13 | 空军工程大学 | Water-air vertical crossing vehicle |
| CN102963230B (en) * | 2012-11-16 | 2015-04-01 | 空军工程大学 | Water-air vertical crossing vehicle |
| CN106809397A (en) * | 2015-11-30 | 2017-06-09 | 黄鹏搏 | A kind of accelerator does the ROV of drive device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102963230B (en) | Water-air vertical crossing vehicle | |
| CN104290907B (en) | Novel hybrid vertical/short take off and landing unmanned vehicle | |
| CN102717887B (en) | A kind of inflatable wing and can the near space dirigible of tilted propeller of adopting | |
| CN104843181A (en) | Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system | |
| CN108688803A (en) | It is a kind of can VTOL aircraft | |
| CN104139845B (en) | Unmanned aerostat system | |
| CN200988577Y (en) | Double airframe triphibian aircraft | |
| CN204527630U (en) | A kind of oil electric mixed dynamic fixed-wing VUAV system | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN106628099A (en) | Tethered and autonomous flight dual-purpose solar aerostat | |
| CN106956555A (en) | The empty dual-purpose variant of water based on the conformal semi-ring wing crosses over ROV | |
| CN102991663A (en) | System for mooring stratospheric telecommunication platform with rotor wing | |
| CN203318067U (en) | Water and sky two-purpose vertical crossing navigating device | |
| CN206141833U (en) | Unmanned aerial vehicle system | |
| CN107554351A (en) | To the aerogenerator device people of high electric air commercial aircraft wireless power | |
| CN106628251A (en) | Combined spacecraft and orbiter launching and recycling method | |
| Meyer et al. | Design considerations for a low altitude long endurance solar powered unmanned aerial vehicle | |
| CN107792360A (en) | Water air double-used aircraft | |
| Posada | Advances, challenges and future of all-electric aircraft | |
| CN206336422U (en) | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship | |
| CN204507268U (en) | Helios power system | |
| CN204264457U (en) | A kind of hybrid power unmanned plane | |
| CN202987513U (en) | Oil-electricity hybrid power unmanned remote sensing airplane | |
| RU2506204C1 (en) | Method of locating high-altitude platform and high-altitude platform | |
| CN101992699A (en) | Solar unmanned spaceship |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: Air Force Engineering University of PLA Document name: Notification of Termination of Patent Right |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131204 Termination date: 20151116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |