CN2617682Y - Two-purpose aircraft with land drive - Google Patents
Two-purpose aircraft with land drive Download PDFInfo
- Publication number
- CN2617682Y CN2617682Y CN 03212907 CN03212907U CN2617682Y CN 2617682 Y CN2617682 Y CN 2617682Y CN 03212907 CN03212907 CN 03212907 CN 03212907 U CN03212907 U CN 03212907U CN 2617682 Y CN2617682 Y CN 2617682Y
- Authority
- CN
- China
- Prior art keywords
- wheel
- fuselage
- land
- aircraft
- driving
- 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
- Toys (AREA)
Abstract
The utility model relates to an aircraft which takes umbrella, which is an aviation aircraft with umbrella wing as lifting power for flying and a propelling device as flying power. The technical proposal provides an aircraft with land driving device for use in air and on land, aiming at overcoming the shortcomings the aircraft in prior cannot drive freely on land. The utility model is matched with the original aircraft structure for assembly, and has the advantages of better performance with more flexible and convenient operation as an ideal apparatus for traveling and other purpose.
Description
Technical field
To the utility model relates to the propeller be Powerpush Unit, be the aviation aircraft technology of aerial lifting power part with the umbrella wing.
Background technology
In this technical field, the name of product of this aircraft so-called " Aircraft ", it is a kind of safe and reliable, flexible operation, based on the middle-size and small-size aviation aircraft of amusement, the purposes of travelling, it is to drive propeller as its flying power by the flight driving engine, finishes by the umbrella wing and takes off, circles in the air and operations such as landing.But existing Aircraft on land can only be vehicle towed by other owing to self do not have the surface driving engine installation, or the manpower push-and-pull moves, and very inconvenience is moved on its ground, and its use is also very inconvenient.
Summary of the invention
For making the Aircraft aircraft have both the dual-use function of flight and land locomotion, the utility model provides the empty land of a kind of energy dual-purpose aircraft, the air and land dual purpose aircraft of the technical program mainly includes the umbrella wing, fuselage, is assemblied in flying power thrust unit, bottom wheel on the fuselage, its major technique characteristics are also to be provided with the land of driving wheel running on the fuselage with driving motion device, this land with drive motion device include driving engine, with engine-drive bonded assembly diff, the driving of diff output shaft and wheel is connected.
In above-mentioned overall technical architecture, forebody, middle part are the installation position of gauge panel and operator's saddle, invade and harass in driving, making machine inner controller and personnel avoid wind and rain, have a fleetline fuselage protective cover by what operator's saddle to front fuselage was provided with spiral-lock, the top of this protective cover is provided with can the Wang Chuangai that dry in the air hinged unlatching, that mainly made by the bright material of full impregnated.Being provided with of this protective cover can also be driven motion device keeps front and back weight on fuselage balance with the land usefulness of fuselage afterbody setting.
In above-mentioned overall technical architecture, bring some harmful effect to the land with the installation of driving motion device for eliminating because of fuselage self space is limited, diff both sides output shaft drives with wheel through universal joint shaft and is connected; The land is provided with engaging and disengaging gear with driving between motion device and the wheel wheel shaft, and this engaging and disengaging gear is the slip clutch that is arranged on the shaft part of universal joint shaft.
Technical solutions of the utility model drive the land of wheel active transport with driving motion device by what be provided with self engine installation, make aircraft initiatively drive down walking freely by wheel, realized that land face ultromotivity moves the purpose of travelling, this device can be realized the identical assembling with airframe structure, the performance of its this type of aircraft product is more superior, using more flexible, convenience, is the desirable apparatus of tourism and other purposes.
Description of drawings
Describe present technique in detail below in conjunction with concrete structure.
Fig. 1 is the plan structure scheme drawing of this air and land dual purpose aircraft
Fig. 2 is the main TV structure figure of Fig. 1
Fig. 3 is that the A of Fig. 1 is to constructional drawing
Fig. 4 is the connection structure scheme drawing of land with drive transmission.
The specific embodiment
The structure of air and land dual purpose aircraft of the present utility model is formed, and includes fuselage, and flying power thrust unit and wheel are installed on the fuselage, also is provided with the umbrella wing hitch that is used to hang the umbrella wing.Present embodiment is to analyze the explanation the technical program with the airframe structure that the rod-type framework constitutes as concrete example.
In the fuselage 4, the front portion is provided with operator's saddle 44 and controller dial plate 45 and control member; Fuselage 4 operator's saddle rear portions are provided with the flying power thrust unit, are driven propeller 3 and are realized flight operation by the lifting of the umbrella wing by flight driving engine 1, and its fuel tank 6 operated by rotary motion are in the operator's saddle bottom; The place ahead and the rear side of fuselage 4 bottoms are provided with wheel 20, and the center of gravity place of fuselage 4 is provided with the hitch 13 that is used to hang the assembling umbrella wing.The land that also is provided with 20 runnings of driving wheel on the fuselage 4 is with driving motion device, it includes the driving engine 2 that is fixedly installed in fuselage 4, the takeoff output beam warp drive disk assembly 16 of driving engine 2 is connected with diff 8, and diff 8 both sides output shafts and wheel 20 wheel shafts drive and are in transmission connection.Its described drive disk assembly 16 can be messenger chain or drive belt etc.In the present embodiment, has a fleetline fuselage protective cover 40 by what operator's saddle 44 to front fuselage was provided with spiral-lock, the top of this protective cover 40 is provided with and can covers 41 by hinged unlatching De lookout window, the prestige window lid 41 that dries in the air is provided with by transparent material and makes De lookout window 42 ， lookout window lid 41 by support link 43 unlatching supports.Umbrella wing hitch is the manipulation position that is caused instrument control panel by the guiding fixed pulley of drag wire and fuselage, by the stay thimble 11 control umbrella wings.Because the land increases the weight of complete machine with the setting of driving motion device, for this reason, can suitably increase the umbrella blade area, or improve the power-handling capability of flight driving engine 1.
But for the complete land operating function of driving motion device, be provided with reverse drive controller 17 between driving engine 2 and the diff 8, its reversing control stalk 7 is by the joystick control of gauge panel position.In the present embodiment, because fuselage self space is limited the land is produced harmful effect with the installation of driving motion device for avoiding as far as possible, the output shaft of diff 8 both sides is in transmission connection through the wheel shaft of universal joint shaft 19 with wheel 20; And drive the mechanical resistance of motion device for the Shi Luyong that reduces to take off, wheel 20 and land are provided with the engaging and disengaging gear that can be separated with its drive element with driving between the motion device, as shown in the figure, its engaging and disengaging gear is the slip clutch 12 that is provided with on the universal joint shaft 19, and this engaging and disengaging gear can also be: located by locating dowel pin 21 between wheel 20 wheel shafts and wheel hub.
Claims (7)
1, a kind of air and land dual purpose aircraft, include the umbrella wing, fuselage (4), be assemblied in flying power thrust unit, bottom wheel on the fuselage, it is characterized in that also being provided with on the fuselage land of driving wheel (20) running with driving motion device, this land with drive motion device include driving engine (2), with engine-drive bonded assembly diff (8), the driving of diff output shaft and wheel is connected.
2, aircraft according to claim 1, it is characterized in that fuselage has a fleetline fuselage protective cover (40) by what waist to front end was provided with spiral-lock, the top of this protective cover (40) be provided with can hinged unlatching, mainly make De lookout window lid (41) by the bright material of full impregnated.
3, aircraft according to claim 1 is characterized in that the output shaft of diff (8) both sides is connected with wheel (20) driving through universal joint shaft (19).
4, aircraft according to claim 1 is characterized in that the land is provided with engaging and disengaging gear with driving between motion device and wheel (20) wheel shaft.
5,, it is characterized in that its engaging and disengaging gear is that the shaft part of universal joint shaft (19) is provided with slip clutch (12) according to claim 3 or 4 described aircraft.
6, aircraft according to claim 4 is characterized in that its engaging and disengaging gear is by locating dowel pin (18) positioning and fixing between wheel (20) wheel shaft and wheel hub.
7, aircraft according to claim 1, it is characterized in that the umbrella wing hangs setting by the umbrella wing hitch at body nodal point place, its hitch is that the manipulation position that the guiding fixed pulley by drag wire and fuselage causes instrument control panel constitutes, and is provided with umbrella wing control stay thimble (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03212907 CN2617682Y (en) | 2003-04-30 | 2003-04-30 | Two-purpose aircraft with land drive |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03212907 CN2617682Y (en) | 2003-04-30 | 2003-04-30 | Two-purpose aircraft with land drive |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2617682Y true CN2617682Y (en) | 2004-05-26 |
Family
ID=34242063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03212907 Expired - Fee Related CN2617682Y (en) | 2003-04-30 | 2003-04-30 | Two-purpose aircraft with land drive |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2617682Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102835381A (en) * | 2011-06-23 | 2012-12-26 | 邓捷 | Plant protection power umbrella |
| US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
-
2003
- 2003-04-30 CN CN 03212907 patent/CN2617682Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9259984B2 (en) | 2008-07-28 | 2016-02-16 | Fleck Future Concepts Gmbh | Combined air, water and road vehicle |
| CN102835381A (en) * | 2011-06-23 | 2012-12-26 | 邓捷 | Plant protection power umbrella |
| CN102835381B (en) * | 2011-06-23 | 2015-03-11 | 北京圣明瑞农业科技有限公司 | Plant protection power umbrella |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6382556B1 (en) | VTOL airplane with only one tiltable prop-rotor | |
| CN106043689B (en) | Backpack Fixed Wing AirVehicle takes off vertically auxiliary system | |
| US20070246601A1 (en) | Manned/unmanned V.T.O.L. flight vehicle | |
| CN206273678U (en) | The unmanned plane that a kind of variable empennage is controlled with folded wing | |
| US20060113426A1 (en) | Vtol vehicles | |
| CN101885295A (en) | Land and air double-used aircraft | |
| CN111003166A (en) | Tandem electric double-rotor helicopter and control system thereof | |
| CN109896003A (en) | A kind of VTOL is verted three rotor wing unmanned aerial vehicles | |
| CN206734620U (en) | The round-the-clock long endurance fixed-wing unmanned plane of VTOL | |
| CN104260873B (en) | A kind of delta-wing aircraft | |
| CN109353176B (en) | Tricycle is experienced in flight | |
| RU2688506C1 (en) | Transformable unmanned aerial vehicle | |
| CN2617682Y (en) | Two-purpose aircraft with land drive | |
| CN207607646U (en) | A kind of vertical take-off and landing unmanned aerial vehicle | |
| CN201419025Y (en) | Model helicopter | |
| CN208377060U (en) | A kind of umbrella wing glide vehicle of nobody full autonomous control | |
| CN1118385C (en) | Flapping-wing flying water automobile | |
| CN107284658B (en) | Composite vertical/short-distance take-off and landing aircraft | |
| CN201989946U (en) | Small-size double-wheel foldable wing airplane | |
| CN110963029A (en) | Method for forming large-wing bird-lift aircraft dragged by power of tilting rotor wing | |
| CN110217391A (en) | A kind of oil electric mixed dynamic VTOL sweepforward fixed-wing unmanned plane | |
| CN109250091A (en) | A kind of flap aircraft | |
| US8944366B2 (en) | Rotorcraft empennage mounting system | |
| CN205930083U (en) | Electronic hovercar of chassis detachable | |
| CN209600800U (en) | A kind of VTOL is verted three rotor wing unmanned aerial vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |