CN104843194A - Airport mobile control tower command and control center - Google Patents
Airport mobile control tower command and control center Download PDFInfo
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- CN104843194A CN104843194A CN201510211615.3A CN201510211615A CN104843194A CN 104843194 A CN104843194 A CN 104843194A CN 201510211615 A CN201510211615 A CN 201510211615A CN 104843194 A CN104843194 A CN 104843194A
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Abstract
The invention discloses an airport mobile control tower command and control center. The airport mobile control tower command and control center comprises an automotive chassis, a cabin lifting platform, a boarding platform and a cabin body, wherein the cabin lifting platform and the boarding platform are fixed on the automotive chassis, the cabin body is arranged on the cabin lifting platform, the cabin lifting platform comprises a hydraulic support rod, two pairs of fork arms, two pairs of slide rails and two pairs of rotary bottom seats, each fork arm comprises an outer arm and an inner arm which are arranged in intercrossed mode, each slide rail comprises an upper slide rail and a lower slide rail, each rotary bottom seat comprises an upper rotary bottom seat and a lower rotary bottom seat, the lower end of each outer arm is arranged on each lower slide rail, the upper end of each outer arm is arranged on each upper rotary bottom seat, the lower end of each inner arm is arranged on each lower rotary bottom seat, the upper end of each inner arm is arranged on each upper slide rail, a connection rod is connected between the inner arms of the two pairs of the fork arms, one end of the hydraulic support rod is fixed on the automotive chassis, and the other end of the hydraulic support rod is fixed on the connection rod. By adopting the above mode, the airport mobile control tower command and control center can achieve a temporary command and dispatch control function, and comprises the lifting platform stable in structure, and furthermore devices in the cabin body have shock absorption functions.
Description
Technical field
The present invention relates to approach tower command centre field, particularly relate to a kind of airport and move 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.
Summary of the invention
The technical matters that the present invention 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 present invention 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 invention has the beneficial effects as follows: the present invention 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 airport of the present invention;
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 invention is described in detail, can be easier to make advantages and features of the invention be readily appreciated by one skilled in the art, thus more explicit defining is made to protection scope of the present invention.
Refer to Fig. 1 to Fig. 5, the embodiment of the present invention 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 present invention 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 embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize specification sheets of the present invention 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 invention.
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 |
|---|---|---|---|
| CN201510211615.3A CN104843194A (en) | 2015-04-29 | 2015-04-29 | Airport mobile control tower command and control center |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510211615.3A CN104843194A (en) | 2015-04-29 | 2015-04-29 | Airport mobile control tower command and control center |
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| CN104843194A true CN104843194A (en) | 2015-08-19 |
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| CN201510211615.3A Pending CN104843194A (en) | 2015-04-29 | 2015-04-29 | Airport mobile control tower command and control center |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105438478A (en) * | 2015-12-29 | 2016-03-30 | 苏州江南航天机电工业有限公司 | Sick and wounded conveying module |
| CN105544985A (en) * | 2016-03-02 | 2016-05-04 | 赵健 | Lifting type construction platform car used on construction site |
| CN105607052A (en) * | 2015-10-28 | 2016-05-25 | 安徽四创电子股份有限公司 | Mobile type large air control secondary radar |
| CN106364696A (en) * | 2016-11-09 | 2017-02-01 | 中国商用飞机有限责任公司民用飞机试飞中心 | Comprehensive guarantee device of high-horizontal-tail and tail-suspended engine aircraft |
| CN106697981A (en) * | 2017-02-23 | 2017-05-24 | 上海三剑制药设备有限公司 | Movable double-cabin-body feeding device |
| CN109153415A (en) * | 2016-04-28 | 2019-01-04 | 鲍曼有限公司 | The motor vehicles with lifting cabin for conveying people and cargo |
| 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 |
| CN111781944A (en) * | 2019-06-24 | 2020-10-16 | 北京京东尚科信息技术有限公司 | Unmanned aerial vehicle ground control station and system |
| CN113410607A (en) * | 2021-06-29 | 2021-09-17 | 中国电子科技集团公司第三十八研究所 | Large-scale radar antenna transportation maintenance device |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105607052A (en) * | 2015-10-28 | 2016-05-25 | 安徽四创电子股份有限公司 | Mobile type large air control secondary radar |
| CN105438478A (en) * | 2015-12-29 | 2016-03-30 | 苏州江南航天机电工业有限公司 | Sick and wounded conveying module |
| CN105544985A (en) * | 2016-03-02 | 2016-05-04 | 赵健 | Lifting type construction platform car used on construction site |
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| 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 |
| CN111781944A (en) * | 2019-06-24 | 2020-10-16 | 北京京东尚科信息技术有限公司 | Unmanned aerial vehicle ground control station and system |
| CN111781944B (en) * | 2019-06-24 | 2024-07-19 | 北京京东尚科信息技术有限公司 | Unmanned aerial vehicle ground control station and system |
| CN113410607A (en) * | 2021-06-29 | 2021-09-17 | 中国电子科技集团公司第三十八研究所 | Large-scale radar antenna transportation maintenance device |
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Application publication date: 20150819 |
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