CN108657464B - Large-scale aircraft decontamination vehicle with multiple cleaning modes - Google Patents
Large-scale aircraft decontamination vehicle with multiple cleaning modes Download PDFInfo
- Publication number
- CN108657464B CN108657464B CN201810723967.0A CN201810723967A CN108657464B CN 108657464 B CN108657464 B CN 108657464B CN 201810723967 A CN201810723967 A CN 201810723967A CN 108657464 B CN108657464 B CN 108657464B
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- Prior art keywords
- arm
- cleaning modes
- vehicle
- multiple cleaning
- decontamination vehicle
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- 238000004140 cleaning Methods 0.000 title claims abstract description 39
- 238000005202 decontamination Methods 0.000 title claims abstract description 29
- 230000003588 decontaminative effect Effects 0.000 title claims abstract description 29
- 239000007788 liquid Substances 0.000 claims abstract description 45
- 230000007246 mechanism Effects 0.000 claims abstract description 16
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 230000009471 action Effects 0.000 claims description 2
- 230000008602 contraction Effects 0.000 claims description 2
- 230000006872 improvement Effects 0.000 description 7
- 238000011161 development Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/30—Cleaning aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
- Cleaning By Liquid Or Steam (AREA)
Abstract
The invention discloses a large-scale aircraft decontamination vehicle with multiple cleaning modes, which comprises a vehicle body, a cleaning liquid supply mechanism, a power pump mechanism and a control system, wherein the high-lift cantilever is arranged on the vehicle body; the high-lift cantilever comprises a base support arm, a multi-stage middle arm and a front end arm which are sequentially connected, and also comprises a telescopic support rod arranged at each connecting position of the base support arm, the multi-stage middle arm and the front end arm; the power pump mechanism comprises a plurality of power pumps with different powers, and the number of the power pumps is the same as the number of the cleaning modes which can be completed by the decontamination vehicle; the cleaning liquid supply mechanism comprises a liquid storage tank, a liquid supply pipeline and a liquid outlet gun which are connected in sequence, and the power pump is connected with the liquid supply pipeline. The invention can effectively and rapidly clean each position of the large-scale airplane and save energy.
Description
Technical Field
The invention belongs to the field of fire-fighting equipment, and particularly relates to a large-scale aircraft decontamination vehicle with multiple cleaning modes.
Background
Fire engines in the prior art mainly adopt conventional methods to carry out tiny operation on low-level equipment, but large-scale aircraft, especially aircraft suffering from nuclear biochemical pollution, need to be cleaned quickly and effectively. The most direct mode is to perform the flushing and brushing by adopting a high-altitude depression mode. Therefore, the invention designs a decontamination vehicle which can be used for effectively riding a large aircraft.
Disclosure of Invention
Aiming at the problems, the invention provides a large-scale aircraft decontamination vehicle with a plurality of cleaning modes.
The technical aim is achieved, and the technical effects are achieved by the following technical scheme:
the large-scale aircraft decontamination vehicle with multiple cleaning modes comprises a vehicle body, a cleaning liquid supply mechanism, a power pump mechanism and a control system, wherein the vehicle body comprises a high lifting cantilever arranged on the vehicle body; the high-lift cantilever comprises a base support arm, a multi-stage middle arm and a front end arm which are sequentially connected, and also comprises a telescopic support rod arranged at each connecting position of the base support arm, the multi-stage middle arm and the front end arm; the power pump mechanism comprises a plurality of power pumps with different powers, and the number of the power pumps is the same as the number of the cleaning modes which can be completed by the decontamination vehicle; the cleaning liquid supply mechanism comprises a liquid storage tank, a liquid supply pipeline and a liquid outlet gun which are connected in sequence, and the power pump is connected with the liquid supply pipeline; the control system comprises a PLC control computer, an angle sensor arranged at the joint of the high-lift cantilever and a distance sensor arranged around the vehicle body, wherein the output ends of the angle sensor and the distance sensor are connected with the input end of the PLC control computer, and the output end of the PLC control computer is connected with the control end of the power pump or the telescopic support rod.
As a further improvement of the invention, the liquid supply pipeline comprises a main pipeline connected with the liquid storage tank and the liquid outlet gun and a branch pipeline positioned in the middle, and the power pump is connected with the branch pipeline.
As a further improvement of the invention, the hydraulic valve is arranged in the branch pipeline at the water inlet end of the power pump, and the control end of the hydraulic valve is connected with the PLC control computer.
As a further improvement of the invention, the invention also comprises an objective table arranged at the forefront end of the front end arm, the liquid outlet gun is arranged at the forefront end of the objective table, and a main pipeline connected with the liquid outlet gun is arranged along the extending direction of the high-lift cantilever.
As a further improvement of the present invention, a telescopic support bar is further included that is disposed between the front arm and the stage.
As a further improvement of the invention, the telescopic supporting rod adopts a hydraulic rod.
As a further improvement of the invention, the multistage intermediate arm comprises a telescopic arm with at least telescopic performance, and the control end of the telescopic arm is connected with a PLC control computer.
As a further improvement of the invention, the PLC control computer is arranged in the cab.
As a further development of the invention, the distance sensor is a radar distance meter.
As a further development of the invention, the angle sensor is a photoelectric sensor.
The invention has the beneficial effects that: according to the invention, through the high lifting cantilever capable of adjusting the angle and the height on the decontamination car and matching with the movement of the decontamination car, each position of a large-sized airplane can be effectively and rapidly cleaned. Various cleaning modes are designed to meet the requirements of cleaning height, and different cleaning liquid supply management and power pumps are opened to convey liquid, so that the effect of comprehensive cleaning is achieved, and energy can be saved.
Drawings
FIG. 1 is a schematic view of an embodiment of the present invention;
FIG. 2 is a schematic structural view of a second embodiment of the present invention;
FIG. 3 is a schematic diagram of a control system according to the present invention;
wherein: the vehicle comprises a vehicle body 1-a high-lift cantilever, a base support arm 201-a multi-stage middle arm 202-a front end arm 203-a telescopic support rod 204-a 3-power pump 4-PLC control computer 5-angle sensor 6-distance sensor 7-objective table 8-liquid storage tank 9-liquid supply pipeline 10-liquid outlet gun.
Detailed Description
The present invention will be described in further detail with reference to the following examples in order to make the objects, technical solutions and advantages of the present invention more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the invention.
The principle of application of the invention is described in detail below with reference to the accompanying drawings.
A large aircraft decontamination vehicle with multiple cleaning modes comprises a vehicle body 1, wherein a high-lift cantilever 2, a cleaning liquid supply mechanism, a power pump 3 mechanism and a control system are arranged in the vehicle body 1.
The high-lift cantilever 2 comprises a base supporting arm 201, a multi-stage middle arm 202 and a front end arm 203 which are sequentially connected, and further comprises a telescopic supporting rod 204 arranged at the joint of the base supporting arm 201, the multi-stage middle arm 202 and the front end arm 203, wherein the multi-stage middle arm 202 comprises at least one telescopic arm with telescopic performance. The bending degree of the high-lift cantilever 2 is adjusted by adjusting the length of the telescopic supporting rod 204, and the height of the high-lift cantilever 2 is adjusted by matching with the multi-stage middle arm 202 with telescopic performance, so that the cleaning requirement of different height areas of a large-scale airplane is met. In order to ensure stability, the telescopic support rod 204 adopts a high-pressure hydraulic rod.
In order to adapt to the cleaning height requirements of different areas, each area adopts different cleaning modes, and the power pump 3 with different powers is needed to meet the requirements of the water pressure in each cleaning mode. The power pump 3 mechanism of the invention thus comprises a number of power pumps 3 of different power, the number of power pumps 3 being the same as the number of washing modes that can be performed by the decontamination vehicle.
The cleaning liquid supply mechanism comprises a liquid storage tank 8, a liquid supply pipeline 9 and a liquid outlet gun 10 which are sequentially connected, and the power pump 3 is connected with the liquid supply pipeline 9. The liquid supply pipeline 9 specifically comprises a main pipeline connected with the liquid storage tank 8 and the liquid outlet gun 10 and a branch pipeline positioned in the middle, and the power pump 3 is connected with the branch pipeline. In addition, the water inlet end of the power pump 3 also comprises a hydraulic valve arranged in the branch pipeline.
The liquid outlet cavity is arranged at the forefront end of the front end arm 203, and the object stage 7 is arranged at the position. The liquid outlet gun 10 is arranged at the forefront end of the objective table 7, and a main pipeline connected with the liquid outlet gun 10 is arranged along the extending direction of the high-lift cantilever 2. And is also connected between the front arm 203 and the stage 7 via a telescopic support bar 204.
The control system comprises a PLC control computer 4, an angle sensor 5 arranged at the joint of the high-lift cantilever 2, and a distance sensor 6 arranged around the vehicle body, wherein the output ends of the angle sensor 5 and the distance sensor 6 are connected with the input end of the PLC control computer 4, and the output end of the PLC control computer 4 is connected with the power pump 3, the telescopic support rod 204 and the control end of the hydraulic valve. And also comprises an alarm system connected with the PLC control computer 4. Under the action of the PLC control computer 4, each cleaning mode is rapidly switched and communicated with corresponding components.
The decontamination vehicle moves around the aircraft to clean the decontamination vehicle through the movement of the decontamination vehicle, the distance sensor 6 is used for monitoring the distance between each position of the vehicle body and the aircraft, the safe distance is 2 meters, and the alarm system can give an alarm when the positions of the decontamination vehicle are too close. The PLC control computer 4 calculates the angle relation of each connecting position of the high-lift cantilever 2 according to the position relation conveyed by the distance sensor 6 and the decontamination mode to be carried out, and adjusts the expansion and contraction amount.
In one embodiment of the present invention, the PLC control computer 4 is disposed in the cab. The distance sensor 6 adopts a radar range finder. The angle sensor 5 is a photoelectric sensor.
The foregoing has shown and described the basic principles and main features of the present invention and the advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present invention, and various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined in the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (10)
1. Large aircraft decontamination vehicle with multiple cleaning modes, comprising a body (1), characterized in that: comprises a high-lift cantilever (2) arranged on a vehicle body (1), a cleaning liquid supply mechanism, a power pump (3) mechanism and a control system;
the high-lift cantilever (2) comprises a base support arm (201), a multistage middle arm (202) and a front end arm (203) which are sequentially connected, and also comprises a telescopic support rod (204) arranged at each connecting position of the base support arm (201), the multistage middle arm (202) and the front end arm (203);
the power pump (3) mechanism comprises a plurality of power pumps (3) with different powers, and the number of the power pumps (3) is the same as the number of the cleaning modes which can be completed by the decontamination vehicle; the cleaning liquid supply mechanism comprises a liquid storage tank (8), a liquid supply pipeline (9) and a liquid outlet gun (10) which are sequentially connected, and the power pump (3) is connected with the liquid supply pipeline (9);
the control system comprises a PLC control computer (4), and further comprises an angle sensor (5) arranged at the joint of the high-lift cantilever (2), a distance sensor (6) arranged around the vehicle body, wherein the output ends of the angle sensor (5) and the distance sensor (6) are connected with the input end of the PLC control computer (4), and the output end of the PLC control computer (4) is connected with the control end of the power pump (3) or the telescopic support rod (204);
under the action of the PLC control computer (4), each cleaning mode is rapidly switched; the PLC control computer (4) calculates the angle relation of each connecting position of the high-lift cantilever (2) according to the position relation conveyed by the distance sensor (6) and the cleaning mode required to be carried out, and adjusts the expansion and contraction amount.
2. The large aircraft decontamination vehicle with multiple cleaning modes of claim 1, wherein: the liquid supply pipeline (9) comprises a main pipeline connected with the liquid storage tank (8) and the liquid outlet gun (10) and a branch pipeline positioned in the middle, and the power pump (3) is connected with the branch pipeline.
3. The large aircraft decontamination vehicle with multiple cleaning modes of claim 2, wherein: the water inlet end of the power pump (3) further comprises a hydraulic valve arranged in the branch pipeline, and the control end of the hydraulic valve is connected with the PLC control computer (4).
4. The large aircraft decontamination vehicle with multiple cleaning modes of claim 2, wherein: the device also comprises an objective table (7) arranged at the forefront end of the front end arm (203), wherein the liquid outlet gun (10) is arranged at the forefront end of the objective table (7), and a main pipeline connected with the liquid outlet gun (10) is arranged along the extending direction of the high-lift cantilever (2).
5. The large aircraft decontamination vehicle with multiple cleaning modes of claim 4, wherein: also comprises a telescopic supporting rod (204) arranged between the front end arm (203) and the objective table (7).
6. The large aircraft decontamination vehicle with multiple cleaning modes of any one of claims 1 or 5, wherein: the telescopic support rod (204) adopts a hydraulic rod.
7. The large aircraft decontamination vehicle with multiple cleaning modes of claim 1, wherein: the multistage middle arm (202) comprises a telescopic arm with at least telescopic performance, and the control end of the telescopic arm is connected with the PLC control computer (4).
8. The large aircraft decontamination vehicle with multiple cleaning modes of claim 1, wherein: the PLC control computer (4) is arranged in the cab.
9. The large aircraft decontamination vehicle with multiple cleaning modes of claim 1, wherein: the distance sensor (6) adopts a radar range finder.
10. The large aircraft decontamination vehicle with multiple cleaning modes of claim 1, wherein: the angle sensor (5) adopts a photoelectric sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810723967.0A CN108657464B (en) | 2018-07-04 | 2018-07-04 | Large-scale aircraft decontamination vehicle with multiple cleaning modes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810723967.0A CN108657464B (en) | 2018-07-04 | 2018-07-04 | Large-scale aircraft decontamination vehicle with multiple cleaning modes |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108657464A CN108657464A (en) | 2018-10-16 |
| CN108657464B true CN108657464B (en) | 2024-02-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810723967.0A Active CN108657464B (en) | 2018-07-04 | 2018-07-04 | Large-scale aircraft decontamination vehicle with multiple cleaning modes |
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| Country | Link |
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| CN (1) | CN108657464B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109760579A (en) * | 2019-01-23 | 2019-05-17 | 上海格拉曼国际消防装备有限公司 | A kind of washing and disinfection car and control method |
| CN109878404A (en) * | 2019-02-28 | 2019-06-14 | 贵州黎阳天翔科技有限公司 | A kind of jet exhaust decontamination vehicle |
| CN110027724A (en) * | 2019-03-14 | 2019-07-19 | 铱格斯曼航空科技集团有限公司 | A kind of robot cleaning device for aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115531A (en) * | 1989-06-21 | 1992-05-26 | Suzuki Mechanical Engineering Co., Ltd. | Aircraft washing equipment |
| JPH06211198A (en) * | 1993-01-20 | 1994-08-02 | Kawasaki Heavy Ind Ltd | Controlling method for aircraft washing device |
| CN101966833A (en) * | 2010-10-27 | 2011-02-09 | 中国民航大学 | Airplane deicing vehicle with vehicle chassis adopting wire control technology |
| KR20120006153U (en) * | 2011-02-24 | 2012-09-03 | 주식회사 진우에스엠씨 | Moving Type Aircraft Engine Washing Device |
| CN202464139U (en) * | 2011-12-27 | 2012-10-03 | 中国人民解放军沈阳军区空军专用车辆技术保障队 | Multifunctional ice removing car for large aircraft |
| CN208470133U (en) * | 2018-07-04 | 2019-02-05 | 上海格拉曼国际消防装备有限公司 | Large aircraft washing and disinfection car with a variety of cleaning models |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7850122B2 (en) * | 2007-12-14 | 2010-12-14 | The Boeing Company | Compliance mechanism |
| FR3060429B1 (en) * | 2016-12-20 | 2019-07-26 | Airbus Operations | MACHINE TOOL HAVING MOUNTING CONFIGURATION WITH DOOR-A-FALSE TOOL |
-
2018
- 2018-07-04 CN CN201810723967.0A patent/CN108657464B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115531A (en) * | 1989-06-21 | 1992-05-26 | Suzuki Mechanical Engineering Co., Ltd. | Aircraft washing equipment |
| JPH06211198A (en) * | 1993-01-20 | 1994-08-02 | Kawasaki Heavy Ind Ltd | Controlling method for aircraft washing device |
| CN101966833A (en) * | 2010-10-27 | 2011-02-09 | 中国民航大学 | Airplane deicing vehicle with vehicle chassis adopting wire control technology |
| KR20120006153U (en) * | 2011-02-24 | 2012-09-03 | 주식회사 진우에스엠씨 | Moving Type Aircraft Engine Washing Device |
| CN202464139U (en) * | 2011-12-27 | 2012-10-03 | 中国人民解放军沈阳军区空军专用车辆技术保障队 | Multifunctional ice removing car for large aircraft |
| CN208470133U (en) * | 2018-07-04 | 2019-02-05 | 上海格拉曼国际消防装备有限公司 | Large aircraft washing and disinfection car with a variety of cleaning models |
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| Publication number | Publication date |
|---|---|
| CN108657464A (en) | 2018-10-16 |
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