CN2640919Y - Multi-seat air/land dual-purpose aerobat - Google Patents
Multi-seat air/land dual-purpose aerobat Download PDFInfo
- Publication number
- CN2640919Y CN2640919Y CN 03284805 CN03284805U CN2640919Y CN 2640919 Y CN2640919 Y CN 2640919Y CN 03284805 CN03284805 CN 03284805 CN 03284805 U CN03284805 U CN 03284805U CN 2640919 Y CN2640919 Y CN 2640919Y
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- land
- tractive
- wheel
- umbrella
- aircraft according
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Abstract
The utility model relates to a bi-function air and land aerocraft, which solves essentially the technical failures that traditional parachute powered aerocraft can not load too much people as well as keep balance and security during flight. The utility model adopts symmetric seat, and parachute wing adopts a parachute surface traction structure of double profiles and crossed traction up and down. Therefore, the utility model with good stability and easy balance adjustment in flight can carry a plurality of people.
Description
Technical field
The aircraft that the utility model relates to is a kind of by the aerial castering action of the umbrella wing with the Miniature Vehicle apparatus of sky with driving engine drive propeller realization airflight.
Background technology
Small and exquisite, the flexible operation of powered parachute flyer volume is a kind of facility that uses mainly as amusement, tourism etc. for people.Flight instruments single, that be at most the double string seat in front and back, supported at three point wheel designs but available dynamic Aircraft device is, be difficult to satisfy the user demand that many people take advantage of an aircraft simultaneously, particularly will guarantee the many people balance of machine comparatively crucial technical barrier that wherein will solve especially in-flight.
The utility model content
Take advantage of seat for making powered parachute flyer can be fit to many people, solve the aircraft that many people take advantage of seat simultaneously and should possess the technical matters of necessary security stationarity awing, the utility model provides a cover to have the technical scheme of the air and land dual purpose aircraft of multidigit seat, the major technique content of this technical scheme is: the composition of this aircraft includes body, body center of gravity place hangs the umbrella wing that is provided with, the land of stack-mounted flight dynamic devices and organism bottom is with taking turns on the body, it is total node by the one-level traction point of body side-by-side mounting center of gravity respectively that two symmetries of the umbrella wing are extended aerofoil, constitute dendritic umbrella cover tractive structure to top set step by step respectively, front and back at least two rows, the setting of the symmetrically arranged multidigit pedestal of every row is installed on the body frame of body bottom surface, the one-level tractive node of one side higher level tractive node and opposite side intersects tractive, constitutes the thriving face tractive of staggered form umbrella structure.
In order to make this aircraft except can finishing the normal flight operation, can also reach the purpose of freely travelling on land, aircraft in the technique scheme also is provided with a cover land actuating device, this land includes land engine, starts the moving diff that is in transmission connection with this with actuating device, the output shaft of diff is connected with wheel drive with the land, rear portion, makes this land constitute the land drive wheel with wheel.Handle in the place aheads of front-seat two and to be respectively equipped with emptyly with control vane and land bearing circle on the position, umbrella wing direction is adjusted drag wire and empty Throttle Opening Control backguy with driving engine and is caused and be connected on the control vane, land engine with turn to control to control with bearing circle by the land.
The aircraft that the utility model patent application is provided has adopted many seat designs, satisfied and gone into the needs of taking advantage of an aircraft simultaneously more, if support body with wheel by four lands, then more can guarantee the stationarity that move on its land, the umbrella cover guy structure that has adopted the mutual tractive of bilateral, balance to pin down on the suspended structure of special its umbrella wing, guaranteeing that the aircraft body awing to the equilibrium activity of self load, reaches the purpose of having a smooth flight, is the fabulous apparatus that is written into of many people's travellings.In addition, technique scheme has also adopted the project organization of land engine, make it not only to realize air objective, travel but also can drive on land, especially horizontal multidigit holder structure, also separation and the independent control for the steering unit of flight operation, land face mobility operation provides the condition that is provided with easily, and this makes the control of this aircraft safer and also have more alerting ability, and entertainment effect is stronger.
Description of drawings
Fig. 1 is the plan structure scheme drawing of this aircraft
Fig. 2 is that the A of Fig. 1 is to structural representation
Fig. 3, Fig. 4 are respectively the tractive structural representation of the umbrella wing
Fig. 5 is the Facad structure scheme drawing of Fig. 1.
The specific embodiment
The structure of multidigit seat powered parachute flyer of the present utility model constitutes and includes body 1, hangs the umbrella wing 3, the body 1 rear portion stack-mounted flight dynamic devices that is provided with by the umbrella wing suspension gear 2 of body, here is that the body that constitutes with the link rod frame structure is that example describes technology contents of the present utility model in detail.
Be arranged with four lands before and after the bottom of organism frame with taking turns 4, wherein two lands at its rear portion are driven by land engine with wheel 40, and in order to reduce this aircraft resistance to motion under steam, its two lands, rear portion are with being covered with stream line pattern protective cover 41 on the wheel 40.Also have a cover land actuating device on this aircraft, this land includes land engine 6, starts the moving diff 7 that is in transmission connection with this with actuating device, and the output shaft of diff drives with wheel 40 with the land, rear portion and is connected, and makes this land constitute the land drive wheel with wheel.The propeller pushing mechanism 5 that the sky that flight dynamic devices is provided with for the organism frame rear portion drives with driving engine, two rows, every row are symmetrical arranged four pedestals 17 of two before and after being fixed with on two parallel body frame beams 18 of body 1 bottom surface, the control in front-seat two the place aheads is handled and has been respectively equipped with on the position with control vane 14 and a land with bearing circle 15, and the direction control drag wire of the umbrella wing and sky are connected with the Throttle Opening Control backguy of driving engine and cause on the control vane 14.Body by back row's seat extremely before is provided with stream line pattern body protective cover 8, and this protective cover 8 is provided with transparent material Zhi Cheng lookout window 60.
It is total tractive node by the one-level traction point of the suspension center of gravity of body 1 both sides respectively that two symmetries of the umbrella wing 3 are extended aerofoils, constitute dendritic umbrella cover tractive structure to top set step by step respectively, in the present embodiment, two flank faces are respectively equipped with three grades of pulling rope tractive nodes, each tractive node A of a side higher level
31, A
32All with the one-level tractive node B of opposite side
0The intersection tractive, the higher level of opposite side and tractive node B
31, B
32All with the one-level tractive node A of opposite side
0The intersection tractive, thus constitute the thriving face tractive of staggered form umbrella structure.
Because the seat increases, the increase of load carrying ability, the suitably umbrella cover of the framed structure of enhancing body and the umbrella wing.
Claims (6)
1, a kind of many air and land dual purpose aircrafts, it includes land that body (1), body center of gravity place hang stack-mounted flight dynamic devices (5) on the umbrella wing (3) that is provided with, the body and organism bottom with wheel (4), it is total node by the one-level traction point of body side-by-side mounting center of gravity respectively that two symmetries of the umbrella wing (3) are extended aerofoil, constitute dendritic umbrella cover tractive structure to top set step by step respectively, at least two rows, the setting of the symmetrically arranged multidigit pedestal of every row are installed on the body frame of body bottom surface before and after it is characterized in that.The one-level tractive node of one side higher level tractive node and opposite side intersects tractive, constitutes the thriving face tractive of staggered form umbrella structure.
2, aircraft according to claim 1 is characterized in that the front and back, bottom of organism frame are arranged with four lands with taking turns (4).
3, aircraft according to claim 2 is characterized in that two lands, rear portion are with being covered with stream line pattern protective cover (41) on the wheel (40).
4, aircraft according to claim 1, it is characterized in that also being provided with in the aircraft cover land actuating device, this land includes land engine (6), starts the moving diff (7) that is in transmission connection with this with actuating device, the output shaft of diff drives with wheel (40) with the land, rear portion and is connected, and makes this land constitute the land drive wheel with wheel.
5, aircraft according to claim 1, it is characterized in that on the manipulation position in front-seat two the place aheads, being respectively equipped with empty with control vane (14) and land with universal dish (15), umbrella wing direction control drag wire and sky cause with the Throttle Opening Control backguy of driving engine and are connected on the control vane (14).
6, aircraft according to claim 1, the body that it is characterized in that back row's seat is to before being provided with stream line pattern body protective cover (6), and this protective cover (6) is provided with transparent material and makes De lookout window (60).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03284805 CN2640919Y (en) | 2003-08-19 | 2003-08-19 | Multi-seat air/land dual-purpose aerobat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03284805 CN2640919Y (en) | 2003-08-19 | 2003-08-19 | Multi-seat air/land dual-purpose aerobat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2640919Y true CN2640919Y (en) | 2004-09-15 |
Family
ID=34303919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03284805 Expired - Fee Related CN2640919Y (en) | 2003-08-19 | 2003-08-19 | Multi-seat air/land dual-purpose aerobat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2640919Y (en) |
Cited By (2)
| 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 |
| CN112550658A (en) * | 2020-12-08 | 2021-03-26 | 芜湖中科飞机制造有限公司 | High-performance and high-strength series-seat type composite material machine body structure |
-
2003
- 2003-08-19 CN CN 03284805 patent/CN2640919Y/en not_active Expired - Fee Related
Cited By (2)
| 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 |
| CN112550658A (en) * | 2020-12-08 | 2021-03-26 | 芜湖中科飞机制造有限公司 | High-performance and high-strength series-seat type composite material machine body structure |
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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 |