CN204750595U - Control tower commander control center is moved on airport - Google Patents
Control tower commander control center is moved on airport Download PDFInfo
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- CN204750595U CN204750595U CN201520267485.0U CN201520267485U CN204750595U CN 204750595 U CN204750595 U CN 204750595U CN 201520267485 U CN201520267485 U CN 201520267485U CN 204750595 U CN204750595 U CN 204750595U
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Abstract
The utility model discloses a control tower commander control center is moved on airport, include vehicle chassis, cabin body lift platform, step on the cabin platform and the cabin body, cabin body lift platform with step on the cabin platform and fix on vehicle chassis, the cabin body sets up on the body lift platform of cabin, cabin body lift platform includes hydraulic pressure vaulting pole, two pairs of yokes, two pairs of slide rails and two couples of rotating base, the yoke includes outer arm and inner arm that intercrossing set up, the slide rail includes slide rail and lower slide rail, rotating base includes rotating base and lower rotating base, the outer arm lower extreme sets up on slide rail down, and the setting of outer arm upper end is on last rotating base, the inner arm lower extreme sets up on rotating base down, and the setting of inner arm upper end is on last slide rail, be connected with the connecting rod between the inner arm of two pairs of yokes, hydraulic pressure vaulting pole one end is fixed on vehicle chassis, and the other end is fixed on the connecting rod. In this way, the utility model discloses can realize the control of commander's dispatch temporarily function, lift platform stable in structure, the internal equipment in cabin has shock -absorbing function.
Description
Technical field
The utility model relates to approach tower command centre field, particularly relates to a kind of airport and moves controHower control center.
Background technology
It is when large-scale activity, accident that controHower control center radical function is moved on airport, plays taking off of interim command scheduling control aircraft, slides, the basic function of landing.Airport is moved controHower control center and is comprised car chassis, cabin body, and is equipped with electronic communication equipment and accessory equipment, can be widely used in the fields such as airport, air force, fire-fighting, People's Armed Police, maritime affairs, city emergency.Cabin body needs to be promoted to about 4 meters, needs to keep cabin body to stablize under lifting state; Be equipped with sophisticated electronics in the body of cabin, need to carry out shock-absorbing protecting to equipment in transportation.
Utility model content
The technical matters that the utility model mainly solves is to provide a kind of airport and moves controHower control center, the fields such as airport, air force, fire-fighting, People's Armed Police, maritime affairs, city emergency can be applicable to, interim command scheduling control function can be realized, lifting table Stability Analysis of Structures, cabin body has shock-absorbing function, can good stability be kept in transportation and lifting process, the working space that good is provided.
For solving the problems of the technologies described above, the technical scheme that the utility model adopts is: provide a kind of airport to move controHower control center, comprise: car chassis, cabin body lifting table, step on cabin platform and cabin body, described cabin body lifting table and step on cabin platform and be fixed on car chassis, described cabin body is arranged on the body lifting table of cabin; Described cabin body lifting table comprises hydraulic strut, two pairs of yokes, two pairs of slide rails and two pairs of rotating bases, and two pairs of yokes, two pairs of slide rails and two pairs of rotating bases are symmetrical arranged mutually; Described yoke comprises outer arm mutually arranged in a crossed manner and inner arm, and outer arm is connected by rotating shaft with inner arm; Described slide rail comprises slide rail and glidepath, and upper slide rail and glidepath are separately fixed on described cabin body and car chassis, upper slide rail and glidepath symmetrical; Described rotating base comprises rotating base and lower rotating base, and upper rotating base and lower rotating base are separately fixed on described cabin body and car chassis; Described outer arm lower end is arranged on glidepath, and outer arm upper end is arranged on rotating base; Described inner arm lower end is arranged on lower rotating base, and inner arm upper end is arranged on slide rail; Be connected with connecting rod between the outer arm of two pairs of yokes, described hydraulic strut one end is fixed on car chassis, and the hydraulic strut other end is fixed on connecting rod; Be fixed with hydraulic control system under described car chassis, described hydraulic control system is connected with described hydraulic strut and hydraulic control strut flexible.
Preferably, described cabin body lifting table is provided with travel switch, limiting stopper and latch gear; Described travel switch and limiting stopper are all arranged on the side near inner arm lower end on glidepath, and described travel switch is connected with the hydraulic control system of described hydraulic strut; Described latch gear comprises gathering lock pin and launches lock pin, draws lock pin in and is arranged between outer arm and inner arm, launches lock pin and is arranged between outer arm and glidepath.
Preferably, be provided with rack, seat, bench board, tower control seat, control tower clearance seat, ups power, air-conditioning and water closet in the body of described cabin, body top, cabin is provided with illuminating lamp, and body all sides in cabin are provided with window blind; VHF voice communication system, meteorological system, radar system and ancillary system is equipped with in the body of described cabin; The external side roof part in described cabin is provided with pick up camera, radar, antenna, alarm obstruction lamp, search lamp and elevation mast; Be provided with bumper between described cabin body and rack, bumper is arranged on corner and body wall place, cabin bottom rack.
Preferably, body top, described cabin is provided with mounting strap, and described mounting strap cross-sectional plane is I shape, and mounting strap side is distributed with electric wiring and fixes hole clipping, has some discharge port bottom mounting strap.
Preferably, bottom the body of described cabin and fixed by twistlock between upper slide rail.
Preferably, body top, described cabin is positioned at body corner, cabin place and is provided with rope mechanism.
Preferably, body four sides in described cabin is provided with glass port, and described glass port entirety is obliquely installed obliquely, and inwardly arranges bottom glass port; Turnoverly on the cabin body of described glass port lower end be set with door-plate, the cabin body of glass port upper end is provided with buckle; Fixed by snap on the body of cabin when described door-plate upwards overturns, and door-plate covers described glass port.
Preferably, be fixed with hydraulic support leg under described car chassis, hydraulic support leg can to external expansion, and hydraulic support leg is connected with described hydraulic control system.
Preferably, described in step on cabin platform be fixed hydraulic bay-lift, fixed hydraulic bay-lift is provided with overload fender guard, hydraulic line bursts protective valve and emergent lowering means; Described fixed hydraulic bay-lift is fixed with guardrail and aerial ladder.
Preferably, described bumper is Rubber shock-absorbing pad.
The beneficial effects of the utility model are: the utility model can be applicable to the fields such as airport, air force, fire-fighting, People's Armed Police, maritime affairs, city emergency, and can realize interim command scheduling control function, lifting table Stability Analysis of Structures, cabin body has shock-absorbing function.
Accompanying drawing explanation
Fig. 1 is the main TV structure schematic diagram that controHower control center travelling position is moved on the utility model airport;
Fig. 2 is the main TV structure schematic diagram that controHower control center deployed condition is moved on shown airport;
Fig. 3 is that the side-looking structural representation removing in controHower control center deployed condition and step on cabin platform is moved on shown airport;
Fig. 4 is the cabin body semi-sictional view structural representation that controHower control center is moved on shown airport;
Fig. 5 is the structural representation that the cabin body lifting table deployed condition of controHower control center is moved on shown airport;
In accompanying drawing, the mark of each parts is as follows: 1, car chassis; 2, cabin body lifting table; 3, cabin platform is stepped on; 4, cabin body; 5, mounting strap; 6, hydraulic support leg; 7, glass port; 8, door-plate; 21, outer arm; 22, inner arm; 23, hydraulic strut; 24, upper slide rail; 25, glidepath; 26, upper rotating base; 27, lower rotating base.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Refer to Fig. 1 to Fig. 5, the utility model embodiment comprises:
ControHower control center is moved on a kind of airport, comprising: car chassis 1, cabin body lifting table 2, step on cabin platform 3 and cabin body 4, described cabin body lifting table 2 and step on cabin platform 3 and to be fixed on car chassis 1, and described cabin body 4 is arranged on cabin body lifting table 2; Described cabin platform 3 of stepping on is for fixed hydraulic bay-lift, and fixed hydraulic bay-lift is provided with overload fender guard, hydraulic line bursts protective valve and emergent lowering means; Described fixed hydraulic bay-lift is fixed with guardrail and aerial ladder; Described cabin body lifting table 2 comprises hydraulic strut 23, two pairs of yokes, two pairs of slide rails and two pairs of rotating bases, and two pairs of yokes, two pairs of slide rails and two pairs of rotating bases are symmetrical arranged mutually; Described yoke comprises outer arm 21 mutually arranged in a crossed manner and inner arm 22, and outer arm 21 is connected by rotating shaft with inner arm 22; Described slide rail comprises slide rail 24 and glidepath 25, and upper slide rail 24 and glidepath 25 are separately fixed on described cabin body 4 and car chassis 4, and upper slide rail 24 and glidepath 25 symmetrically, are fixed by twistlock bottom described cabin body 4 and between upper slide rail 24; Described rotating base comprises rotating base 26 and lower rotating base 27, and upper rotating base 26 and lower rotating base 27 are separately fixed on described cabin body 4 and car chassis 1; Described outer arm 21 lower end is arranged on glidepath 25, and outer arm 21 upper end is arranged on rotating base 26; Described inner arm 22 lower end to be arranged on lower rotating base 27, and inner arm 22 upper end is arranged on slide rail 24; Be connected with connecting rod between the outer arm 21 of two pairs of yokes, described hydraulic strut 23 one end is fixed on car chassis 1, and hydraulic strut 23 other end is fixed on connecting rod; Described car chassis is fixed with hydraulic control system 1 time, described hydraulic control system is connected with described hydraulic strut and hydraulic control strut flexible, described car chassis is fixed with hydraulic support leg 61 time, and hydraulic support leg 6 can to external expansion, and hydraulic support leg 6 is connected with described hydraulic control system.Described cabin body lifting table 2 is provided with travel switch, limiting stopper and latch gear; Described travel switch and limiting stopper are all arranged on the side near inner arm 22 lower end on glidepath, and described travel switch is connected with the hydraulic control system of described hydraulic strut; Described latch gear comprises gathering lock pin and launches lock pin, draws lock pin in and is arranged between outer arm and inner arm, launches lock pin and is arranged between outer arm and glidepath.
Be provided with rack, seat, bench board, tower control seat, control tower clearance seat, ups power, air-conditioning and water closet in described cabin body 4, body top, cabin is provided with illuminating lamp, and body four sides in cabin are provided with window blind; VHF voice communication system, meteorological system, radar system and ancillary system is equipped with in described cabin body 4; Described cabin body 4 outside top is provided with pick up camera, radar, antenna, alarm obstruction lamp, search lamp and elevation mast; Be provided with Rubber shock-absorbing pad between described cabin body 4 and rack, Rubber shock-absorbing pad is arranged on corner place and body wall place, cabin bottom rack, and Rubber shock-absorbing pad can instrument on available protecting rack; Body 4 top, described cabin is provided with mounting strap 5, described mounting strap 5 cross-sectional plane is I shape, mounting strap 5 side is distributed with electric wiring and fixes hole clipping, some discharge port are had bottom mounting strap 5, pick up camera, radar, antenna, Warning light, search lamp and elevation mast are fixed on mounting strap 5, electric wiring is fixed hole clipping and is facilitated cabling, and discharge port is beneficial to cabin body top draining; Body 4 top, described cabin is positioned at body corner, cabin place and is provided with rope mechanism, when cabin body rises, rope pull-out is fixed with ground, can strengthen the stability of cabin body; Body four sides, described cabin is provided with glass port 7, and described glass port 7 entirety is obliquely installed obliquely, and inwardly arranges bottom glass port 7, and glass port 7 can not produce reflective to overhead, affect aviator's sight line; Turnoverly on the cabin body of described glass port 7 lower end be set with door-plate 8, the cabin body of glass port 7 upper end is provided with buckle; Fixed by snap on cabin body 4 when described door-plate 8 upwards overturns, and door-plate 8 covers described glass port 7, when travelling position, door-plate 8 can play bridging effect.
When travelling position, door-plate preventing glass window, yoke shrinks, and draws lock pin in and is fixed between outer arm and inner arm, making cabin body stable fixing, preventing cabin body from beating when jolting; When needs rise cabin body carries out schedule job, hydraulic control system launches hydraulic support leg, hydraulic support leg coarse adjustment is put down, accurate adjustment is put down again, unclamp gathering lock, hydraulic strut props up cabin body lifting table, when cabin body is raised to specified altitude assignment, touch travel switch on the downside of outer arm, hydraulic strut stops extending, and launches lock pin and outer arm and glidepath is fixed, complete cabin body and promote operation, limiting stopper can prevent cabin body lifting table from continuing to run when stroke switch failure, pulled open and be fixed on bottom surface by the rope of body lower end, cabin, makes cabin body keep stable.Staff climbs up from aerial ladder and steps on cabin platform, steps on cabin platform and promotes, personnel are delivered to body place, cabin, facilitate personnel to enter cabin body.First cabin body unclamps the expansion lock between outer arm and glidepath when declining, shrink hydraulic strut, with gathering lock sealed cabin body lifting table, finally packs up hydraulic support leg.
The utility model can be applicable to the fields such as airport, air force, fire-fighting, People's Armed Police, maritime affairs, city emergency, interim command scheduling control function can be realized, lifting table Stability Analysis of Structures, in the body of cabin, equipment has shock-absorbing function, can good stability be kept in transportation and lifting process, the working space that good is provided.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification sheets and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. controHower control center is moved on an airport, it is characterized in that, comprise: car chassis, cabin body lifting table, step on cabin platform and cabin body, described cabin body lifting table and step on cabin platform and be fixed on car chassis, described cabin body is arranged on the body lifting table of cabin; Described cabin body lifting table comprises hydraulic strut, two pairs of yokes, two pairs of slide rails and two pairs of rotating bases, and two pairs of yokes, two pairs of slide rails and two pairs of rotating bases are symmetrical arranged mutually; Described yoke comprises outer arm mutually arranged in a crossed manner and inner arm, and outer arm is connected by rotating shaft with inner arm; Described slide rail comprises slide rail and glidepath, and upper slide rail and glidepath are separately fixed on described cabin body and car chassis, upper slide rail and glidepath symmetrical; Described rotating base comprises rotating base and lower rotating base, and upper rotating base and lower rotating base are separately fixed on described cabin body and car chassis; Described outer arm lower end is arranged on glidepath, and outer arm upper end is arranged on rotating base; Described inner arm lower end is arranged on lower rotating base, and inner arm upper end is arranged on slide rail; Be connected with connecting rod between the outer arm of two pairs of yokes, described hydraulic strut one end is fixed on car chassis, and the hydraulic strut other end is fixed on connecting rod; Be fixed with hydraulic control system under described car chassis, described hydraulic control system is connected with described hydraulic strut and hydraulic control strut flexible.
2. controHower control center is moved on airport according to claim 1, it is characterized in that: described cabin body lifting table is provided with travel switch, limiting stopper and latch gear; Described travel switch and limiting stopper are all arranged on the side near inner arm lower end on glidepath, and described travel switch is connected with the hydraulic control system of described hydraulic strut; Described latch gear comprises gathering lock pin and launches lock pin, draws lock pin in and is arranged between outer arm and inner arm, launches lock pin and is arranged between outer arm and glidepath.
3. controHower control center is moved on airport according to claim 1, it is characterized in that: in the body of described cabin, be provided with rack, seat, bench board, tower control seat, control tower clearance seat, ups power, air-conditioning and water closet, body top, cabin is provided with illuminating lamp, and body all sides in cabin are provided with window blind; VHF voice communication system, meteorological system, radar system and ancillary system is equipped with in the body of described cabin; The external side roof part in described cabin is provided with pick up camera, radar, antenna, alarm obstruction lamp, search lamp and elevation mast; Be provided with bumper between described cabin body and rack, bumper is arranged on corner and body wall place, cabin bottom rack.
4. controHower control center is moved on airport according to claim 1, it is characterized in that: body top, described cabin is provided with mounting strap, described mounting strap cross-sectional plane is I shape, and mounting strap side is distributed with electric wiring and fixes hole clipping, has some discharge port bottom mounting strap.
5. controHower control center is moved on airport according to claim 1, it is characterized in that: fixed by twistlock bottom the body of described cabin and between upper slide rail.
6. controHower control center is moved on airport according to claim 1, it is characterized in that: body top, described cabin is positioned at body corner, cabin place and is provided with rope mechanism.
7. controHower control center is moved on airport according to claim 1, it is characterized in that: body four sides in described cabin is provided with glass port, and described glass port entirety is obliquely installed obliquely, and inwardly arranges bottom glass port; Turnoverly on the cabin body of described glass port lower end be set with door-plate, the cabin body of glass port upper end is provided with buckle; Fixed by snap on the body of cabin when described door-plate upwards overturns, and door-plate covers described glass port.
8. controHower control center is moved on airport according to claim 1, it is characterized in that: be fixed with hydraulic support leg under described car chassis, and hydraulic support leg can to external expansion, and hydraulic support leg is connected with described hydraulic control system.
9. controHower control center is moved on airport according to claim 1, it is characterized in that: described in step on cabin platform be fixed hydraulic bay-lift, fixed hydraulic bay-lift is provided with overload fender guard, hydraulic line bursts protective valve and emergent lowering means; Described fixed hydraulic bay-lift is fixed with guardrail and aerial ladder.
10. controHower control center is moved on airport according to claim 3, it is characterized in that: described bumper is Rubber shock-absorbing pad.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520267485.0U CN204750595U (en) | 2015-04-29 | 2015-04-29 | Control tower commander control center is moved on airport |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520267485.0U CN204750595U (en) | 2015-04-29 | 2015-04-29 | Control tower commander control center is moved on airport |
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| CN204750595U true CN204750595U (en) | 2015-11-11 |
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| CN201520267485.0U Active CN204750595U (en) | 2015-04-29 | 2015-04-29 | Control tower commander control center is moved on airport |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105446189A (en) * | 2015-12-16 | 2016-03-30 | 中国人民解放军空军勤务学院 | Airport elevating loading and unloading platform integrated control system |
| CN107808992A (en) * | 2017-12-01 | 2018-03-16 | 重庆固恒通信设备有限公司 | For justifying the top antenna structure excessively of battle array electronic scanning antenna |
| CN109544997A (en) * | 2018-12-27 | 2019-03-29 | 四川九洲空管科技有限责任公司 | A kind of mobile control tower based on blank pipe communication and surveillance technology |
-
2015
- 2015-04-29 CN CN201520267485.0U patent/CN204750595U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105446189A (en) * | 2015-12-16 | 2016-03-30 | 中国人民解放军空军勤务学院 | Airport elevating loading and unloading platform integrated control system |
| CN105446189B (en) * | 2015-12-16 | 2019-01-29 | 中国人民解放军空军勤务学院 | A kind of airport elevating platform complex control system |
| CN107808992A (en) * | 2017-12-01 | 2018-03-16 | 重庆固恒通信设备有限公司 | For justifying the top antenna structure excessively of battle array electronic scanning antenna |
| CN109544997A (en) * | 2018-12-27 | 2019-03-29 | 四川九洲空管科技有限责任公司 | A kind of mobile control tower based on blank pipe communication and surveillance technology |
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