CN107244425A - A kind of aircraft surfaces steam cleaner - Google Patents
A kind of aircraft surfaces steam cleaner Download PDFInfo
- Publication number
- CN107244425A CN107244425A CN201710567542.0A CN201710567542A CN107244425A CN 107244425 A CN107244425 A CN 107244425A CN 201710567542 A CN201710567542 A CN 201710567542A CN 107244425 A CN107244425 A CN 107244425A
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- CN
- China
- Prior art keywords
- pipeline
- handle
- bottom plate
- spring
- tap
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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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
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cleaning By Liquid Or Steam (AREA)
Abstract
A kind of aircraft surfaces steam cleaner, including buried water tank and spring；The top surface of the bottom plate is provided with bearing block by bolt, and pipeline is fitted on the inner chamber top surface of bottom plate by bearing block；The pipeline is at three, wherein being water inlet pipeline at middle one；Spring base is mounted on the inwall of the pipeline and the left and right wall of tap；The tap is arranged on the top surface of floor cavities, evaporator and compression pump；Pipeline front end termination is provided with handle about described, the water pipeline used is for about, and handle is fitted with, and stood on using spring elongation principle on ground, pipeline is arranged on the inside of chassis by bearing block, both hands shake handle makes water pipeline vacillate now to the left, now to the right, water spray is set to flow to form multiaspect injection, so as to the thorough hydro-peening in aircraft bottom, this double handle is L-shaped structure and stood on ground, using the wiggly mode of spring, instead of original hinge stent mode.
Description
Technical field
The present invention relates to aircraft cleaning technique field, more particularly to a kind of aircraft surfaces steam cleaner.
Background technology
Agricultural aircraft is in flight course, due to jet, the reason such as spray, easily produced in its bottom substantial amounts of dust or
Decoction dirt, these dirts cannot be cleaned for a long time influences attractive in appearance, and the effect of chemicals easily makes fuselage bottom paint
Layer is aoxidized, and is caused spot to fall paint, is caused to fall paint position to be got rusty.
The inventors discovered that, the existing cleaning device for agricultural pesticide sprayer bottom is simple in construction, and it is typically using small
Type movable type jetter, causes water resource waste, and using being placed in external water tank on the ground, area occupied is larger, is adopted jet pipe more more
Connected with hinge stent, during rotation, not easy to operate.
Then, inventor in view of this, adhere to the relevant industries for many years it is abundant design and develop and actual fabrication experience,
It is buried to be studied improvement there is provided a kind of water tank for existing structure and missing, and recycled with water resource
Aircraft surfaces steam cleaner, to reach the purpose for having more more practical value.
The content of the invention
It is an object of the invention to provide a kind of aircraft surfaces steam cleaner, to solve to propose in above-mentioned background technology
The existing cleaning device for agricultural pesticide sprayer bottom it is simple in construction, its typically use miniature movable type jetter, make
Into water resource waste, using being placed on the ground external water tank, area occupied is larger, is connected more than jet pipe using hinge stent more, during rotation,
Not easy to operate the problem of.
The purpose and effect of aircraft surfaces steam cleaner of the present invention, are reached by technological means in detail below：
A kind of aircraft surfaces steam cleaner, wherein, the aircraft surfaces steam cleaner includes：
Bottom plate, pipeline, bearing block, jet pipe, spring base, tap, shower nozzle, compression pump, evaporator, handle, effluent filter, pin
Pedal, buried water tank and spring；
The top surface of the bottom plate is provided with bearing block by bolt, and pipeline is fitted in the inner chamber top surface of bottom plate by bearing block
On；The pipeline is at three, wherein in the middle of be water inlet pipeline at one, and about on pipe wall through installing with spray
The jet pipe of head；Spring base is mounted on the inwall of the pipeline and the left and right wall of tap；The tap is arranged on bottom plate
On the top surface of inner chamber, and tap be located at about pipeline centre position；Spring base between the tap and pipeline
Between spring is installed；The buried water tank locates below ground level, and the front openings position of itself and bottom plate connects；It is described
The top surface of buried water tank, which is equipped with, bottom-up on pedal, and the output channel of buried water tank is connected with sewage mistake in turn
Filter, evaporator and compression pump；Pipeline front end termination is provided with handle about described.
Further, handle uses L-shaped structure about described, and its pipeline with about is connected, but not phase
It is logical, and this at two handle inwardly pulled at two due to pipeline spring, handle one is stood on ground at two, and it
In " interior eight word " shape symmetrical configuration distribution.
Further, the jet pipe runs through for staggeredly mode and is arranged on the tube wall of everywhere pipeline.
Further, bearing is inlaid with the bearing block, it is realized by bearing and the pipeline being applied in its inner chamber
It is flexibly connected.
Further, the bottom plate is to drag pocket closed-in construction.
With existing structure in comparison, the invention has the advantages that：
1. in the present invention, the water tank used is buried, instead of original ground type, make the larger water tank of volume not in ground
Under, using the bottom plate of tower structure as the supporter for installing each part, the water that shower nozzle sprays is flowed back by chassis
Recycling is filtered into buried water tank, and by filter, water circulation is used.
2. in the present invention, the water pipeline used is fitted with handle for about, and utilizes spring elongation
Principle is stood on ground, and pipeline is arranged on the inside of chassis by bearing block, and both hands shake handle makes water pipeline or so
Wave, make water spray flow to form multiaspect injection, so as to the thorough hydro-peening in aircraft bottom, this double handle is L-shaped structure and stood on
On ground, using the wiggly mode of spring, instead of original hinge stent mode, make more convenient operation.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is the present invention only base arrangement schematic diagram；
Fig. 3 is spring seat structure schematic diagram of the present invention.
In figure：1st, bottom plate, 2, pipeline, 3, bearing block, 4, jet pipe, 5, spring base, 6, tap, 7, shower nozzle, 8, compression pump,
9th, evaporator, 10, handle, 11, effluent filter, 12, pedal, 13, buried water tank, 14, spring.
Embodiment
Below, embodiments of the invention are will be explained in, the example is shown in the accompanying drawings and the description below.Although will combine
The exemplary embodiment description present invention, it is to be understood that the description is not really wanted to limit the invention to the exemplary implementation
Example.On the contrary, the present invention will not only cover the exemplary embodiment, but also cover various replacements, change, it is equivalent and
Other embodiment, it can be included in the spirit and scope of the present invention that appended claims are limited.
Referring to Fig. 1 to accompanying drawing 3, a kind of aircraft surfaces steam cleaner includes：
Bottom plate 1, pipeline 2, bearing block 3, jet pipe 4, spring base 5, tap 6, shower nozzle 7, compression pump 8, evaporator 9, handle 10, dirt
Water filter 11, pedal 12, buried water tank 13 and spring 14；
The top surface of bottom plate 1 is provided with bearing block 3 by bolt, and pipeline 2 is fitted in the inner chamber top surface of bottom plate 1 by bearing block 3
On；Pipeline 2 is at three, wherein in the middle of be water inlet pipeline at one, and about carry shower nozzle through installing on the tube wall of pipeline 2
7 jet pipe 4；Spring base 5 is mounted on the inwall of pipeline 2 and the left and right wall of tap 6；Tap 6 is arranged on the inner chamber of bottom plate 1
Top surface on, and tap 6 be located at about pipeline 2 centre position；Between spring base 5 between tap 6 and pipeline 2
Spring 14 is installed；Buried water tank 13 locates below ground level, and the front openings position of itself and bottom plate 1 connects；It is buried
The top surface of water tank 13, which is equipped with, bottom-up on pedal 12, and the output channel 2 of buried water tank 13 is connected with sewage in turn
Filter 11, evaporator 9 and compression pump 8；About the front end termination of pipeline 2 handle 10 is installed.
The preferred embodiment of aircraft surfaces steam cleaner described above, wherein, about handle 10 use L-shaped knot
Structure, and its pipeline 2 with about is connected, but be not communicated with, and this at two handle 10 inwardly pulled at two due to spring 14
The reason for pipeline 2, handle 10 1 is stood on ground at two, and they are distributed in " interior eight word " shape symmetrical configuration, utilize L-shaped
The handle 10 and the active force of collaboration spring 14 stood on ground, forms yaw movements, big model is carried out to aircraft bottom
The sprinkling enclosed.
The preferred embodiment of aircraft surfaces steam cleaner as described above, wherein, jet pipe 4 runs through for staggeredly mode
On the tube wall for being arranged in everywhere pipeline 2, spraying range is improved；
The preferred embodiment of aircraft surfaces steam cleaner as described above, wherein, bearing is inlaid with bearing block 3, its
Realized and be flexibly connected with the pipeline 2 being applied in its inner chamber by bearing.When being easy to hand cranking handle 10, the pipeline 2 of the left and right sides
The realization that can more smoothly stablize is vacillated now to the left, now to the right.
The preferred embodiment of aircraft surfaces steam cleaner as described above, wherein, bottom plate is to drag pocket closed-in construction,
Open rearward end is designed, for agricultural aircraft turnover, and there is the peripheral frame enclosed left and right sides and front side, is oriented to the water of ejection and is flowed into ground
In buried water tank 12.
The operation principle of the present embodiment：
Bottom plate 1 is installed on the ground, and B horizontal planes are higher than front side A horizontal planes at rear openings, is easy to water spray to be formed on bottom plate 1
During current, it is flowed into from the front to the back in buried water tank 13, carries out water circulation collection, start external power source, outside suction pump
Water in buried water tank 13 is pumped into effluent filter 11 by pipeline 2, progress in evaporator 9 is entered after being handled
Evaporation process, forms steam and is pumped to by compression pump 8 in left and right pipeline 2, sprayed eventually through the shower nozzle 7 on jet pipe 4, this mistake
Hand cranking handle 10 in journey, make left and right pipeline 2 be realized on bearing block 3 and swing, so that what jet pipe 4 was sprayed by shower nozzle 7
Steam sprays to aircraft bottom and cleaned comprehensively, and the current of formation are flowed on bottom plate 1, enters eventually into buried water tank 13
In, recycle, this process human body station is operated on pedal 12, and pedal 12 is placed on buried water tank 13 and pushed up
Side.
It should be noted that the standardized element that the present invention is used can commercially, shaped piece is according to explanation
Book and accompanying drawing record can carry out customized, and the specific connected mode of each part is using spiral shell ripe in the prior art
The conventional meanses such as bolt, rivet, welding, machinery, part and equipment are used in the prior art, conventional model, and inventor is herein
No longer it is described in detail, the suction pump particularly mentioned in the design, compression pump, the circuit connection of evaporator and internal structure are existing
There is technology, the design does not make separately to state.
In summary, although the present invention is described in detail with reference to the foregoing embodiments, for the technology of this area
For personnel, it can still modify to the technical scheme described in foregoing embodiments, or to which part technology
Feature carries out equivalent substitution, within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc.,
It should be included within protection scope of the present invention.
Claims (5)
1. a kind of aircraft surfaces steam cleaner, it is characterised in that：Described aircraft surfaces steam cleaner includes：
Bottom plate, pipeline, bearing block, jet pipe, spring base, tap, shower nozzle, compression pump, evaporator, handle, effluent filter, pin
Pedal, buried water tank and spring；
The top surface of the bottom plate is provided with bearing block by bolt, and pipeline is fitted in the inner chamber top surface of bottom plate by bearing block
On；The pipeline is at three, wherein in the middle of be water inlet pipeline at one, and about on pipe wall through installing with spray
The jet pipe of head；Spring base is mounted on the inwall of the pipeline and the left and right wall of tap；The tap is arranged on bottom plate
On the top surface of inner chamber, and tap be located at about pipeline centre position；Spring base between the tap and pipeline
Between spring is installed；The buried water tank locates below ground level, and the front openings position of itself and bottom plate connects；It is described
The top surface of buried water tank, which is equipped with, bottom-up on pedal, and the output channel of buried water tank is connected with sewage mistake in turn
Filter, evaporator and compression pump；Pipeline front end termination is provided with handle about described.
2. aircraft surfaces steam cleaner according to claim 1, it is characterised in that：Handle is used about described
L-shaped structure, and its pipeline with about is connected, but be not communicated with, and this at two handle inwardly pulled at two due to spring
The reason for pipeline, handle one is stood on ground at two, and they are distributed in " interior eight word " shape symmetrical configuration.
3. the aircraft surfaces steam cleaner according to claim, it is characterised in that：The jet pipe passes through for staggeredly mode
Wear and be arranged on the tube wall of everywhere pipeline.
4. the aircraft surfaces steam cleaner according to claim, it is characterised in that：Axle is inlaid with the bearing block
Hold, it is realized with the pipeline being applied in its inner chamber by bearing and is flexibly connected.
5. the aircraft surfaces steam cleaner according to claim, it is characterised in that：The bottom plate is to drag pocket frame knot
Structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710567542.0A CN107244425A (en) | 2017-07-12 | 2017-07-12 | A kind of aircraft surfaces steam cleaner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710567542.0A CN107244425A (en) | 2017-07-12 | 2017-07-12 | A kind of aircraft surfaces steam cleaner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107244425A true CN107244425A (en) | 2017-10-13 |
Family
ID=60015404
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710567542.0A Withdrawn CN107244425A (en) | 2017-07-12 | 2017-07-12 | A kind of aircraft surfaces steam cleaner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107244425A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804476A (en) * | 2017-10-31 | 2018-03-16 | 河南飞防兵科技有限公司 | A kind of unmanned plane shell cleaning device |
-
2017
- 2017-07-12 CN CN201710567542.0A patent/CN107244425A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804476A (en) * | 2017-10-31 | 2018-03-16 | 河南飞防兵科技有限公司 | A kind of unmanned plane shell cleaning device |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171013 |
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| WW01 | Invention patent application withdrawn after publication |