CN103373474A - Novel plane runway transfer platform - Google Patents
Novel plane runway transfer platform Download PDFInfo
- Publication number
- CN103373474A CN103373474A CN2012101130696A CN201210113069A CN103373474A CN 103373474 A CN103373474 A CN 103373474A CN 2012101130696 A CN2012101130696 A CN 2012101130696A CN 201210113069 A CN201210113069 A CN 201210113069A CN 103373474 A CN103373474 A CN 103373474A
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- horizontal plate
- bearing plate
- plate
- load
- disposed
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Abstract
The invention discloses a novel plane runway transfer platform which comprises a horizontal plate, a frame and a rotary drum. The frame is located on the upper surface of the horizontal plate. The rotary drum is located on the frame. The rotary drum is provided with hooks for runway traction. A control mechanism for controlling the rotary drum to rotate is disposed on one side of the frame. A wireless communication device and a tool box are further disposed on the upper surface of the horizontal plate. A load-bearing plate the same as the horizontal plate is disposed on the lower surface of the horizontal plate. The center of the load-bearing plate and the horizontal plate are rotatably connected. A traction head is disposed on one side of the load-bearing plate. A roller mechanism is disposed on the lower surface of the load-bearing plate. The novel plane runway transfer platform has the advantages that wireless communication with the outside and wireless help requests transmission are facilitated by the wireless communication device, tools can be stored in the tool box, the load-bearing plate is rotatably connected with the horizontal plate, when the load-bearing plate stays still, the horizontal plate can rotate 360 degrees on the horizontal plane, the traction head disposed on one side of the load-bearing plate facilitate trailer traction, and convenient moving is achieved by the roller mechanism disposed on the lower surface.
Description
Technical field
The present invention relates to a kind of transfer platform, relate in particular to a kind of type aircraft road face transfer platform.
Background technology
Aircraft is taking off, landing, accidentally gun off the runway when sliding or be stranded near the runway, need to accident aircraft be transferred to perch with special wrecking equipment, in the wrecking equipment, rescue pavement transfer station commonly used, it can utilize rotating mechanism with the road face on rotating cylinder, but present transfer platform is exactly common backplane band roller, and self is heavier, more painstaking in the time of the one way or another rotation, underaction, in addition, do not have damping effect, and people need to communicate by letter with the external world at any time at rescue site, also can use a lot of related tools, present road face transfer station does not also possess the function of radio communication, and the function of taking in instrument, and it is comparatively single that function seems.
Summary of the invention
Purpose of the present invention just is that providing a kind of addresses the above problem, and flexibly again original place realization rotation has communication and takes in the type aircraft road face transfer platform of instrumental function.
To achieve these goals, the technical solution used in the present invention is such: a kind of type aircraft road face transfer platform, comprise horizontal plate, be positioned at the support body of horizontal plate upper surface, be positioned at the cylinder on the support body, described cylinder is provided with the hook of tow way face, support body one side is provided with the control mechanism of index drum rotation, the horizontal plate upper surface also is provided with a radio communication device and a tool box, the horizontal plate lower surface is provided with it identical bearing plate of a shape size, described bearing plate is connected central rotation and is connected with horizontal plate, bearing plate one side is provided with drawing head, and lower surface is provided with idler wheel mechanism.
As preferably: described idler wheel mechanism is four universal caster wheels that are positioned at the bearing plate lower surface.
As preferably: be provided with damping between bearing plate and horizontal plate.
Compared with prior art, the invention has the advantages that: the horizontal plate upper surface also is provided with a radio communication device and a tool box, can be convenient for people to carry out carry out radio communication and send wireless relief request with the external world, the convenient extraneous very first time is grasped field condition, instrument can be taken in the tool box, has well to take in function, and bearing plate is connected central rotation and is connected with horizontal plate, when bearing plate is motionless, horizontal plate can be at the horizontal surface rotating 360 degrees, and flexible, bearing plate one side is provided with drawing head, can make things convenient for trailer traction, lower surface is provided with idler wheel mechanism, conveniently moving, and idler wheel mechanism is universal caster wheel, turn to flexibly, be provided with damping between bearing plate and horizontal plate, have the effect of antidetonation shock attenuation, can reduce the vibrations of all parts on the horizontal plate, the present invention is simple in structure, and is convenient and practical.
Description of drawings
Fig. 1 is structural representation of the present invention.
Among the figure: 1, horizontal plate; 2, support body; 3, cylinder; 4, hook; 5, control mechanism; 6, bearing plate; 7, drawing head; 8, radio communication device; 9, tool box; 10, idler wheel mechanism.
The specific embodiment
The invention will be further described below in conjunction with accompanying drawing.
Embodiment 1: referring to Fig. 1, a kind of type aircraft road face transfer platform, comprise horizontal plate 1, be positioned at the support body 2 of horizontal plate 1 upper surface, be positioned at the cylinder 3 on the support body 2, described cylinder 3 is provided with the hook 4 of tow way face, support body 2 one sides are provided with the control mechanism 5 of index drum 3 rotations, horizontal plate 1 upper surface also is provided with a radio communication device 8 and a tool box 9, horizontal plate 1 lower surface is provided with it identical bearing plate 6 of a shape size, the central rotation that described bearing plate 6 is connected with horizontal plate connects, bearing plate 6 one sides are provided with drawing head 7, lower surface is provided with idler wheel mechanism 10, described idler wheel mechanism 10 is for being positioned at four universal caster wheels of bearing plate 6 lower surfaces, and 1 of bearing plate 6 and horizontal plate are provided with damping.
Horizontal plate 1 upper surface also is provided with a radio communication device 8 and a tool box 9, can be convenient for people to carry out carry out radio communication and send wireless relief request with the external world, the convenient extraneous very first time is grasped field condition, instrument can be taken in tool box 9, have and well take in function, the central rotation that bearing plate 6 is connected with horizontal plate connects, when bearing plate 6 is motionless, horizontal plate 1 can be at the horizontal surface rotating 360 degrees, and flexible, bearing plate 6 one sides are provided with drawing head 7, can make things convenient for trailer traction, lower surface is provided with idler wheel mechanism 10, conveniently moving, and idler wheel mechanism 10 is universal caster wheel, turn to flexibly, 1 of bearing plate 6 and horizontal plate are provided with damping, have the effect of antidetonation shock attenuation, can reduce the vibrations of all parts on the horizontal plate 1.
Claims (3)
1. type aircraft road face transfer platform, comprise horizontal plate, be positioned at the horizontal plate upper surface support body, be positioned at the cylinder on the support body, described cylinder is provided with the hook of tow way face, support body one side is provided with the control mechanism of index drum rotation, it is characterized in that: the horizontal plate upper surface also is provided with a radio communication device and a tool box, the horizontal plate lower surface is provided with it identical bearing plate of a shape size, described bearing plate is connected central rotation and is connected with horizontal plate, bearing plate one side is provided with drawing head, and lower surface is provided with idler wheel mechanism.
2. type aircraft according to claim 1 road face transfer platform, it is characterized in that: described idler wheel mechanism is four universal caster wheels that are positioned at the bearing plate lower surface.
3. type aircraft according to claim 1 road face transfer platform is characterized in that: be provided with damping between bearing plate and horizontal plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101130696A CN103373474A (en) | 2012-04-18 | 2012-04-18 | Novel plane runway transfer platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101130696A CN103373474A (en) | 2012-04-18 | 2012-04-18 | Novel plane runway transfer platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103373474A true CN103373474A (en) | 2013-10-30 |
Family
ID=49459430
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012101130696A Pending CN103373474A (en) | 2012-04-18 | 2012-04-18 | Novel plane runway transfer platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103373474A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003240518A (en) * | 2002-02-13 | 2003-08-27 | Kawasaki Heavy Ind Ltd | Method, system and apparatus for inspection of earth surface state |
| CN201597757U (en) * | 2009-12-07 | 2010-10-06 | 徐孝勤 | Transfer platform for emergency rescue road surface of airplane |
| CN102239087A (en) * | 2008-11-25 | 2011-11-09 | 以色列宇航工业有限公司 | Towbarless airplane tug |
| CN202686774U (en) * | 2012-04-18 | 2013-01-23 | 成都思茂科技有限公司 | Novel airplane runway pavement transfer platform |
-
2012
- 2012-04-18 CN CN2012101130696A patent/CN103373474A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003240518A (en) * | 2002-02-13 | 2003-08-27 | Kawasaki Heavy Ind Ltd | Method, system and apparatus for inspection of earth surface state |
| CN102239087A (en) * | 2008-11-25 | 2011-11-09 | 以色列宇航工业有限公司 | Towbarless airplane tug |
| CN201597757U (en) * | 2009-12-07 | 2010-10-06 | 徐孝勤 | Transfer platform for emergency rescue road surface of airplane |
| CN202686774U (en) * | 2012-04-18 | 2013-01-23 | 成都思茂科技有限公司 | Novel airplane runway pavement transfer platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20131030 |