CN204979252U - Aircraft receiving and dispatching control system - Google Patents
Aircraft receiving and dispatching control system Download PDFInfo
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- CN204979252U CN204979252U CN201520678200.2U CN201520678200U CN204979252U CN 204979252 U CN204979252 U CN 204979252U CN 201520678200 U CN201520678200 U CN 201520678200U CN 204979252 U CN204979252 U CN 204979252U
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- aircraft
- car body
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- motor
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Abstract
The utility model provides an aircraft receiving and dispatching control system, including wall climbing robot and aircraft receiving and dispatching platform, wall climbing robot includes main automobile body, the induction port that link up about main automobile body middle part is equipped with, induction port department is equipped with the adsorption apparatus structure in the middle part of main automobile body, main automobile body lower surface is equipped with two sets of wheels and is used for drive wheels's two sets of first motor one by one, border department is equipped with and is used for driving aircraft receiving and dispatching platform pivoted second motor on the main automobile body, main automobile body periphery is equipped with and hangs the frame with main automobile body assorted, main automobile body with hang frame fixed connection, the lower border that hangs the frame is equipped with seal structure. The utility model discloses an aircraft receiving and dispatching control system, through wall climbing robot and aircraft receiving and dispatching platform can realize the aircraft freely hover with the space in freely remove to pass narrow and small space and transport formulation input point with the aircraft, have very big flexibility. In addition, its simple structure, the mechanical stability is good, so the cost is honest and clean, the price / performance ratio is very high.
Description
Technical field
The utility model relates to flying vehicles control technical field, more specifically, relates to a kind of aircraft transmitting-receiving control system.
Background technology
In the process of investigation, rescue, can the unmanned plane of quick travel due to self stability, cannot through narrow spaces such as wall seams.And it is excessively slow to have the adaptive crawler vehicle moving velocity of face strongly, and be difficult to arrive higher district as places such as high buildings.Crawler-type wall climbing robot can be stable move to floor eminence, and a large amount of load can be carried, but its moving velocity slowly always disabled person denounce.Unmanned plane is combined with crawler-type wall climbing robot, fully can combine the two advantage, and both deficiencies can be made up.So " the SUAV (small unmanned aerial vehicle) wall ambulatory transceiver base station " of our design is by track propulsion, overall flat, metope has good stability and functional reliability, is extremely adapted at the wall mobile working of narrow and small mobile space.By adopting the mode of vertically carrying unmanned plane, making entire system height be less than the width of unmanned plane itself, in the discovery of the good ball cage type aircraft of contrast comformability, more effectively can pass through the obstacles such as narrow and small wall seam.While delivery unmanned plane, also shorten the flying distance of unmanned plane to objective, saved unmanned plane finite energy, improve the utilization ratio of its energy.In addition, the prior effect in this base station is exactly the signal relay function utilized on vehicular platform, set up the signal transmission bridge inside and outside building, the ability of signal " through walls " is strengthened greatly, obtain larger scope of reconnaissance, this mode also makes unmanned plane can carry lighter signal transmitting apparatus, thus makes its more how useful quality of can unloading.
But the major defect of this climbing robot does not also have to solve the sealing problem for vacuum cavity very well, because its seal ring and main car body belong to be rigidly connected, when take turns or crawler belt run into slightly irregular metope time, entirety can be waved, thus seal ring is contacted with metope produce gap.Therefore, need to develop a kind of climbing robot improving sealing property.
Utility model content
The utility model makes to solve the above-mentioned technical matters that exists in prior art, its object is to provide a kind of aircraft to receive and dispatch control system.
To achieve these goals, the utility model provides a kind of aircraft to receive and dispatch control system, comprises climbing robot and aircraft transmit-receive platform; Described climbing robot is adsorbed on outside vertically metope, and described aircraft transmit-receive platform is connected with described climbing robot, and the level that can turn to is for the landing of external flight device.
Wherein, described climbing robot comprises main car body, the air suctiton inlet of up/down perforation is provided with in the middle part of described main car body, in the middle part of described main car body, described air suctiton inlet place is provided with adsorbing mechanism, described main car body lower surface is provided with two groups of wheels and for driving two group of first motor of described wheel one by one, described main car body upper edge place is provided with the second motor for driving described aircraft transmit-receive platform to rotate, described main car body periphery is provided with the suspension housing matched with described main car body, described main car body is fixedly connected with described suspension housing, the lower edge of described suspension housing is provided with hermetically-sealed construction.
Described aircraft transmit-receive platform comprises stops plate and parking bracket, one end of described parking bracket is connected with described second motor by Change-over frame, described parking bracket surrounding is provided with groove, and be provided with magnet in the middle part of described parking bracket, described stop plate is fixed on described parking bracket, described middle part is stopped plate and is provided with opening, and described magnet is just in time positioned at the opening in the middle part of described stop plate.
A kind of aircraft transmitting-receiving control system of the present utility model, aircraft can be realized by described climbing robot and aircraft transmit-receive platform freely to hover and moving freely in space, and through narrow space, aircraft is transported to formulation release position, and be aided with wireless telecommunications system relaying, expand the transmission distance of signal, make signal easily " through walls ", thus can carry out real time reconnaissance to building inner case, greatly increase its flying power, there is very large alerting ability.In addition, its structure is simple, and good mechanical stability, so cost is honest and clean, cost performance is very high.
Accompanying drawing explanation
By reference to following detailed description of the invention and claims content and by reference to the accompanying drawings, other object of the present utility model and result will be understood and easy to understand more.In the accompanying drawings:
Fig. 1 is the front view of a kind of aircraft transmitting-receiving control system of the present utility model;
Fig. 2 is the front view of climbing robot in a kind of aircraft transmitting-receiving control system of the present utility model;
Fig. 3 is the upward view of climbing robot in a kind of aircraft transmitting-receiving control system of the present utility model;
Fig. 4 is the structural representation of aircraft transmit-receive platform in a kind of aircraft transmitting-receiving control system of the present utility model;
Fig. 5 is the partial schematic diagram of the bottom construction of aircraft transmit-receive platform in a kind of aircraft transmitting-receiving control system of the present utility model.
In accompanying drawing, the list of parts representated by each label is as follows:
1, main car body, 2, hang housing;
11, air suctiton inlet, 12, adsorbing mechanism, 13, wheel, the 14, first motor, the 15, second motor, the 16, first fixed contact, 21, hermetically-sealed construction, the 22, second fixed contact, 31, stop plate, 32, parking bracket, 33, Change-over frame, 34, groove, 35, magnet;
121, the 3rd motor, 122, fan.
In the accompanying drawings, identical Reference numeral indicates similar or corresponding feature or function.
Detailed description of the invention
In the following description, for purposes of illustration, in order to provide the complete understanding to one or more embodiment, many details have been set forth.But, clearly, also these embodiments can be realized when there is no these details.In other example, one or more embodiment for convenience of description, known structure and equipment illustrate in block form an.
Come below with reference to accompanying drawings to be described in detail according to each embodiment of the present utility model.
As shown in Figure 1, a kind of front view of aircraft transmitting-receiving control system, comprises climbing robot and aircraft transmit-receive platform; Climbing robot is adsorbed on outside vertically metope, and aircraft transmit-receive platform is connected with climbing robot, and the level that can turn to is for the landing of external flight device.
As shown in Figure 2,3, climbing robot comprises main car body 1, the air suctiton inlet 11 of up/down perforation is provided with in the middle part of main car body 1, in the middle part of main car body 1, air suctiton inlet 11 place is provided with adsorbing mechanism 12, main car body 1 lower surface is provided with two groups of wheels 13 and for driving two group of first motor 14 of wheel 13 one by one, main car body 1 upper edge place is provided with the second motor 15 for driving aircraft transmit-receive platform to rotate, main car body 1 periphery is provided with the suspension housing 2 matched with main car body 1, main car body 1 is fixedly connected with suspension housing 2, and the lower edge hanging housing 2 is provided with hermetically-sealed construction 21.
As shown in Figure 4, aircraft transmit-receive platform comprises stops plate 31 and parking bracket 32, one end of parking bracket 32 is connected with the second motor 15 by Change-over frame 33, parking bracket 32 surrounding is provided with groove 34, and be provided with magnet 35 in the middle part of parking bracket 32, stopping plate 31 is fixed on parking bracket 32, and middle part is stopped plate 31 and is provided with opening, and magnet 35 is just in time positioned at the opening stopped in the middle part of plate 31.
In the present embodiment, main car body 1 upper edge place is also provided with multiple first fixed contact 16, and suspension housing 2 upper edge place is provided with second fixed contact 22, first fixed contact 16 identical with the first fixed contact 16 quantity and is fixedly connected with the second fixed contact 22 one_to_one corresponding.Can main car body 1 periphery be fixed on by hanging housing 2 by the first fixed contact 16 and the second fixed contact 22 and support below main car body 1 and form cavity.
Preferably, the first fixed contact 16 is arranged on main car body 1 upper edge place uniformly, and the second fixed contact 22 is also arranged on the upper edge place of suspension housing 2 uniformly and aligns with the first fixed contact 16.Main car body 1 can be made by the way and hang housing 2, and uniform stressed when creeping on body of wall, guaranteeing that climbing robot pulsation-free on wall is creeped, for subsequent flights device stable landing or get up to provide basis.
Preferably, the first fixed contact 16 is fixedly connected with by glue rod with the second fixed contact 22.Both can reach fixing intensity by glue rod, be convenient to again later stage disassembly, cleaning, very convenient.Can certainly be fixedly connected with by other means, these are all within protection domain of the present utility model.
In the present embodiment, adsorbing mechanism 12 comprises the 3rd motor 121 and fan 122, and fan comprises multi-disc impeller, and the 3rd motor 121 is positioned at fan center and drive fan 122 is rotated, and makes to form vacuum cavity below main car body 1.When the 3rd motor 121 drives the vane rotary of fan 122, gas between the impeller Leaf of High Rotation Speed also and then rotates, and under the influence of centrifugal force these gases are thrown to impeller surrounding, gas flow rate increases, make gas, in flowing, kinetic energy is converted to static energy, then along with the supercharging of fluid, static energy is made to be converted to again speed energy, the gas below main car body 1 in cavity is discharged by air suctiton inlet 11, form vacuum cavity, and certain negative pressure is defined in the middle of impeller, due to air suctiton inlet 11, place is negative pressure, main car body 1 is just pressed to body of wall by external pressure, the absorption of whole climbing robot limit on the wall.
Hermetically-sealed construction 21 comprises supporting layer, and one end of supporting layer is connected with the lower edge hanging housing 2, and the other end and the both sides of supporting layer are all coated with plastic sheeting, and the other end of supporting layer is attached on outside metope by plastic sheeting pressure.When adsorbing mechanism 12 works, main car body 1 is pressed to body of wall by barometric pressure, and now supporting layer is played a supporting role, and makes to keep vacuum cavity below main car body 1, makes main car body 1 can continue absorption on the wall.
It is to be noted, here supporting layer is not play sealing function, only play the effect of support, the plastic sheeting inside supporting layer can move in box haul, and the plastic sheeting outside supporting layer is due to the plastic sheeting of inner side and blocking of supporting layer, be difficult to inwardly motion, therefore metope is being close to, due to the characteristic that plastic sheeting is soft, smooth, can close proximity to ground, adapt to the concavo-convex metope of part, whole climbing robot can be made to creep at rough metope pulsation-free.
Preferably, supporting layer is bristles material.The hardness of bristles can support whole main car body 1 and hang the weight of housing 2, therefore establishes circle bristles can play good supporting role in suspension below.
Preferably, double-plastic is polytetrafluoroethylene PTFE material.Polytetrafluoroethylene has the feature of antiacid alkali resistant, anti-various organic solvent, and be dissolved in all solvents hardly, service life is longer, has resistant to elevated temperatures feature, and its friction coefficient is extremely low, so have good lubricating effect.Therefore, when what resistance climbing robot does not almost have when metope is creeped, can creep by pulsation-free very much.
Preferably, parking bracket 32 be provided with the 4th motor the 36, four motor 36 for drive magnet 35 make its along near or move away from stopping the direction of plate 31.Particularly, as shown in Figure 5, the 4th motor 36 is connected with worm and gear 37, makes magnet 35 away from stop plate 31 by worm and gear 37.When aircraft transmit-receive platform is horizontal, aircraft steadily can be rested on transmit-receive platform by gravity, now, by controlling the 4th motor drive magnets 35 away from stop plate 31, thus the distance increased on magnet 35 and aircraft between iron plate, its mutual attractive force is diminished, when the gravitation on magnet 35 and aircraft between iron plate be less than aircraft play non-critical value time, aircraft can the taking off of safety and steady.
Preferably, first motor 14 is DC brushless motor, DC brushless motor has the advantage of Traditional DC motor, eliminate carbon brush again simultaneously, slip ring structure, can the high-power operation of low speed, volume is little, lightweight, exert oneself large, torque characteristics is excellent, in, low speed torque performance is good, detent torque is large, starting current is little, infinite speed variation, speed adjustable range is wide, overload capacity is strong, efficiency is high, motor itself does not have excitation loss and carbon brush loss, eliminate multi-stage speed-reducing consumption, integrated power-saving rate can reach 20% ~ 60%, reliability is high, good stability, strong adaptability, maintenance is simple, resistance to vibrations of jolting, noise is low, shake little, smooth movement, life-span is long.
A kind of aircraft transmitting-receiving control system of the present utility model, aircraft can be realized by climbing robot and aircraft transmit-receive platform freely to hover and moving freely in space, and through narrow space, aircraft is transported to formulation release position, and be aided with wireless telecommunications system relaying, expand the transmission distance of signal, make signal easily " through walls ", thus can carry out real time reconnaissance to building inner case, greatly increase its flying power, there is very large alerting ability.In addition, its structure is simple, and good mechanical stability, so cost is honest and clean, cost performance is very high.
Although disclosed content shows exemplary embodiment of the present utility model above, it should be noted that under the prerequisite not deviating from the scope that claim limits, can multiple change and amendment be carried out.Need not perform with any particular order according to the function of the claim to a method of utility model embodiment described herein, step and/or action.In addition, although element of the present utility model with individual formal description or requirement, can also it is contemplated that to have multiple element, be individual element unless explicitly limited.
Claims (10)
1. an aircraft transmitting-receiving control system, is characterized in that: comprise climbing robot and aircraft transmit-receive platform; Described climbing robot is adsorbed on outside vertically metope, and described aircraft transmit-receive platform is connected with described climbing robot, and the level that can turn to is for the landing of external flight device;
Described climbing robot comprises main car body (1), described main car body (1) middle part is provided with the air suctiton inlet (11) of up/down perforation, at described main car body (1) middle part, described air suctiton inlet (11) place is provided with adsorbing mechanism (12), described main car body (1) lower surface is provided with two groups of wheels (13) and for driving two group of first motor (14) of described wheel (13) one by one, described main car body (1) upper edge place is provided with the second motor (15) for driving described aircraft transmit-receive platform to rotate, described main car body (1) periphery is provided with the suspension housing (2) matched with described main car body (1), described main car body (1) is fixedly connected with described suspension housing (2), the lower edge of described suspension housing (2) is provided with hermetically-sealed construction (21),
Described aircraft transmit-receive platform comprises stops plate (31) and parking bracket (32), one end of described parking bracket (32) is connected with described second motor (15) by Change-over frame (33), described parking bracket (32) surrounding is provided with groove (34), and described parking bracket (32) middle part is provided with magnet (35), described stop plate (31) is fixed on described parking bracket (32), described middle part is stopped plate (31) and is provided with opening, and described magnet (35) is just in time positioned at the opening at described stop plate (31) middle part.
2. a kind of aircraft transmitting-receiving control system according to claim 1, it is characterized in that: described main car body (1) upper edge place is also provided with multiple first fixed contact (16), described suspension housing (2) upper edge place is provided with and identical second fixed contact (22) of described first fixed contact (16) quantity, and described first fixed contact (16) is fixedly connected with described second fixed contact (22) one_to_one corresponding.
3. a kind of aircraft transmitting-receiving control system according to claim 2, it is characterized in that: described first fixed contact (16) is arranged on described main car body (1) upper edge place uniformly, and described second fixed contact (22) is also arranged on the upper edge place of described suspension housing (2) uniformly and aligns with described first fixed contact (16).
4. a kind of aircraft transmitting-receiving control system according to claim 3, is characterized in that: described first fixed contact (16) is fixedly connected with by glue rod with described second fixed contact (22).
5. a kind of aircraft transmitting-receiving control system according to claim 1, it is characterized in that: described adsorbing mechanism (12) comprises the 3rd motor (121) and fan (122), described fan comprises multi-disc impeller, described 3rd motor (121) is positioned at described fan center and drives described fan (122) to rotate, and makes described main car body (1) below form vacuum cavity.
6. a kind of aircraft transmitting-receiving control system according to claim 1, it is characterized in that: described hermetically-sealed construction (21) comprises supporting layer, one end of described supporting layer is connected with the lower edge of described suspension housing (2), the other end and the both sides of described supporting layer are all coated with plastic sheeting, and the other end of described supporting layer is attached on outside metope by described plastic sheeting pressure.
7. a kind of aircraft transmitting-receiving control system according to claim 6, is characterized in that: described supporting layer is bristles material.
8. a kind of aircraft transmitting-receiving control system according to claim 6, is characterized in that: described plastic sheeting is polytetrafluoroethylene PTFE material.
9. a kind of aircraft transmitting-receiving control system according to claim 1, it is characterized in that: described parking bracket (32) is provided with the 4th motor, described 4th motor is used for drive magnet (35) makes it move along close or away from described stop plate (31) direction.
10. a kind of aircraft transmitting-receiving control system according to any one of claim 1 to 9, is characterized in that: described first motor (14) is DC brushless motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520678200.2U CN204979252U (en) | 2015-09-02 | 2015-09-02 | Aircraft receiving and dispatching control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520678200.2U CN204979252U (en) | 2015-09-02 | 2015-09-02 | Aircraft receiving and dispatching control system |
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| Publication Number | Publication Date |
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| CN204979252U true CN204979252U (en) | 2016-01-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520678200.2U Withdrawn - After Issue CN204979252U (en) | 2015-09-02 | 2015-09-02 | Aircraft receiving and dispatching control system |
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| CN (1) | CN204979252U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105346724A (en) * | 2015-09-02 | 2016-02-24 | 蔡兆旸 | Aircraft transmit-receive control system |
| CN111688827A (en) * | 2020-06-18 | 2020-09-22 | 中国计量大学 | Repeater transceiver |
-
2015
- 2015-09-02 CN CN201520678200.2U patent/CN204979252U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105346724A (en) * | 2015-09-02 | 2016-02-24 | 蔡兆旸 | Aircraft transmit-receive control system |
| CN105346724B (en) * | 2015-09-02 | 2017-05-10 | 蔡兆旸 | Aircraft transmit-receive control system |
| CN111688827A (en) * | 2020-06-18 | 2020-09-22 | 中国计量大学 | Repeater transceiver |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160120 Effective date of abandoning: 20170510 |
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| AV01 | Patent right actively abandoned |