CN108941134A - The positioning mechanism of space shuttle engine turbine leaf cleaning equipment - Google Patents
The positioning mechanism of space shuttle engine turbine leaf cleaning equipment Download PDFInfo
- Publication number
- CN108941134A CN108941134A CN201811032844.9A CN201811032844A CN108941134A CN 108941134 A CN108941134 A CN 108941134A CN 201811032844 A CN201811032844 A CN 201811032844A CN 108941134 A CN108941134 A CN 108941134A
- Authority
- CN
- China
- Prior art keywords
- rectangular slab
- sewage collecting
- cleaning equipment
- arc panel
- positioning mechanism
- 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
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B13/00—Accessories or details of general applicability for machines or apparatus for cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
- B08B3/02—Cleaning by the force of jets or sprays
- B08B3/022—Cleaning travelling work
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B2203/00—Details of cleaning machines or methods involving the use or presence of liquid or steam
- B08B2203/02—Details of machines or methods for cleaning by the force of jets or sprays
- B08B2203/0264—Splash guards
Landscapes
- Cleaning In General (AREA)
Abstract
The present invention provides the positioning mechanism of space shuttle engine turbine leaf cleaning equipment, including lower rectangular slab, hydraulic scissors mechanism, upper rectangular slab, sewage collecting shell, valve, sewage collecting groove, telescopic rod, support rod, arc panel, rubber layer, silica gel baffler and metal stereotypes hoses；Angle position in edge is mounted on the universal wheel with position-limit mechanism to the lower rectangular slab bottom face everywhere；The upper later half position of rectangular slab top end face is fixedly connected with one piece of sewage collecting shell.The present invention is when carrying out cleaning operation, can make arc panel and two pieces of silica gel bafflers carries out coverage package to aircraft engine turbine position, conducive to when to aircraft engine turbo blade cleaning operation, the water lotion to flash will touch on arc panel and two pieces of silica gel bafflers, then it slides along its surface to sewage collecting groove, centralized collection is got up, when will not be as conventional clean, water lotion flashes around on ground, leads to subsequent be not easily cleaned.
Description
Technical field
The invention belongs to engine turbine leaf cleaning technical fields, and more specifically, in particular to space shuttle starts
The positioning mechanism of machine turbo blade cleaning equipment.
Background technique
Currently, flying under the adverse circumstances such as more dirt or coastal moist salt fog since dust, salt fog etc. are easily accessible
In the airflow channel of machine turbo oar engine, deposit and salt marsh are easy to produce at the components in airflow channel.In hot conditions
Under, above-mentioned deposit and salt marsh are easy to corrode on engine air circulation road components, so that will lead to components
Strength reduction.When seriously corroded, the position that components are corroded even will form tired source, and then split components generation
Line, seriously affects the performance of engine, to influence the security performance of aircraft.
Based on above-mentioned, the inventors discovered that, when outfield carries out washing and cleaning operation to engine turbine blade, engine is dry and cold
Turn, reach standard in engine speed, after obtaining the password of test run personnel " starting to inject water lotion ", ground staff passes through cleaning
Equipment starts to inject water lotion to engine, and by immersion in 5 minutes, cold forwarding motivation injected water lotion again, impregnates 5 again
Minute, by water lotion twice flushing and three times the flushing of clear water complete to engine turbine leaf cleaning operation, but this is clear
During washing, dry and cold turn of engine, cause water lotion and the clear water of cleaning that can flash everywhere, so that massive laundering liquid flashed in week
On exclosure face, lead to subsequent be not easily cleaned.
Then, in view of this, being studied improvement for existing structure and missing, space shuttle engine turbine is provided
The positioning mechanism of leaf cleaning equipment, to achieve the purpose that with more more practical value.
Summary of the invention
In order to solve the above technical problem, the present invention provides the localization machines of space shuttle engine turbine leaf cleaning equipment
Structure dry and cold turn of engine, leads to water lotion and cleaning to solve tradition when carrying out washing and cleaning operation to engine turbine blade
Clear water can flash everywhere, so that massive laundering liquid flashes around on ground, cause subsequent to be not easily cleaned problem.
The purpose and effect of the positioning mechanism of space shuttle engine turbine leaf cleaning equipment of the present invention, by detail below
Technological means is reached:
The positioning mechanism of space shuttle engine turbine leaf cleaning equipment, including lower rectangular slab, universal wheel, hydraulic scissor machine
Structure, upper rectangular slab, sewage collecting shell, valve, sewage collecting groove, telescopic rod, support rod, arc panel, rubber layer, silica gel resistance
Partition and metal stereotypes hoses；It is provided with one piece of upper rectangular slab consistent with its size right above the lower rectangular slab,
And it is connected between the lower rectangular slab and the upper rectangular slab by the hydraulic scissors mechanism；The lower rectangular slab bottom face
Angle position in edge is mounted on the universal wheel with position-limit mechanism everywhere；The upper later half position of rectangular slab top end face
It is fixedly connected with one piece of sewage collecting shell.
Further, sewage collecting housing tip face offers the sewage collecting groove at one, and the sewage
Assembling supporting member right side is provided with the valve being connected with the sewage collecting groove.
Further, at left and right sides of sewage collecting housing tip face intermediate position be fixedly connected to one described in stretch
Contracting bar, and two telescopic rod top ends are connected with the support rod jointly.
Further, support rod bottom face centre is welded with one piece of arc panel, and in the arc panel
End face, which is sticked, one layer of rubber layer.
Further, the arc panel left and right ends is fixedly connected to one piece of silica gel baffler；Described in every piece
Four metal stereotypes hoses in the distribution of front and back rectangular array are provided with inside silica gel baffler.
Compared with prior art, the invention has the following beneficial effects:
The present invention when carrying out cleaning operation, can make arc panel and two pieces of silica gel bafflers to aircraft engine turbine position into
Row covers package, is conducive to when to aircraft engine turbo blade cleaning operation, the water lotion to flash will touch arc panel
And on two pieces of silica gel bafflers, then slide along its surface to sewage collecting groove, centralized collection is got up, will not be as traditional clear
When washing, water lotion flashes around on ground, leads to subsequent be not easily cleaned.
Detailed description of the invention
Fig. 1 is schematic view of the front view of the invention.
Fig. 2 is sewage collecting shell schematic cross-sectional view in Fig. 1 of the invention.
Fig. 3 is overlooking structure diagram of the invention.
Fig. 4 is silica gel baffler schematic cross-sectional view of the invention.
In figure, the corresponding relationship of component names and accompanying drawing number are as follows:
Rectangular slab under 1-, 101- universal wheel, the hydraulic scissors mechanism of 2-, the upper rectangular slab of 3-, 4- sewage collecting shell, 401- valve,
402- sewage collecting groove, 5- telescopic rod, 6- support rod, 7- arc panel, 701- rubber layer, 8- silica gel baffler, 801- metal
Stereotypes hoses.
Specific embodiment
Embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples.Following embodiment is used for
Illustrate the present invention, but cannot be used to limit the scope of the invention.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more；Term " on ",
The orientation or positional relationship of the instructions such as "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and should not be understood as instruction or
Imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connected " " connects
Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected；It can be machine
Tool connection, is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment:
As shown in attached drawing 1 to attached drawing 4:
The present invention provides the positioning mechanism of space shuttle engine turbine leaf cleaning equipment, including lower rectangular slab 1, universal wheel
101, hydraulic scissors mechanism 2, upper rectangular slab 3, sewage collecting shell 4, valve 401, sewage collecting groove 402, telescopic rod 5, branch
Strut 6, arc panel 7, rubber layer 701, silica gel baffler 8 and metal stereotypes hoses 801；It is arranged right above the lower rectangular slab 1
There is one piece of upper rectangular slab 3 consistent with its size, and passes through institute between the lower rectangular slab 1 and the upper rectangular slab 3
Hydraulic scissors mechanism 2 is stated to be connected；Angle position in edge is mounted on a band position restrainer to 1 bottom face of lower rectangular slab everywhere
The universal wheel 101 of structure；The later half position of 3 top end face of upper rectangular slab is fixedly connected with one piece of sewage collecting shell 4.
Wherein, 4 top end face of sewage collecting shell offers the sewage collecting groove 402 at one, and the sewage
4 right side of assembling supporting member is provided with the valve 401 being connected with the sewage collecting groove 402.
Wherein, at left and right sides of 4 top end face of sewage collecting shell intermediate position be fixedly connected to one it is described flexible
Bar 5, and two 5 tops of telescopic rod are connected with the support rod 6 jointly.
Wherein, the 6 bottom face centre of support rod is welded with one piece of arc panel 7, and 7 inner end of the arc panel
Face, which is sticked, one layer of rubber layer 701.
Wherein, 7 left and right ends of arc panel is fixedly connected to one piece of silica gel baffler 8；Every block of silicon
Four metal stereotypes hoses 801 in the distribution of front and back rectangular array are provided with inside glue baffler 8.
The specifically used mode and effect of the present embodiment:
When outfield carries out cleaning operation to space shuttle engine turbine blade, cleaning equipment is fixedly mounted on upper square first
3 first half position of shape plate controls hydraulic scissors mechanism 2 by control cabinet and drives later according to the position of aircraft engine turbo blade
Dynamic upper rectangular slab 3 carries out the adjusting operation of height, with guarantee cleaning equipment cleaning port it is corresponding aircraft engine turbine leaf
The position of piece；Support rod 6 is adjusted by pulling, so that two telescopic rods 5 is followed stretching, extension or contraction, makes 7 inner end of arc panel and aircraft
The outer protective shell at engine turbine position is in contact, and hides position above aircraft engine turbine open end, and arc panel 7
Inner face, which sticks, one layer of rubber layer 701, therefore guarantees that 7 inner end of arc panel will not be with the outer protective shell at aircraft engine turbine position
It directly contacts, scratch will not be caused to it；7 left and right ends of arc panel is fixedly connected to one piece of silica gel baffler 8, and every piece
Four metal stereotypes hoses 801 in the distribution of front and back rectangular array, therefore silica gel baffler 8 are provided with inside silica gel baffler 8
Shape carried out shaping via metal stereotypes hoses 801, so that two pieces of silica gel bafflers 8 is wrapped up the periphery of aircraft engine turbine,
And the characteristic of 8 material of silica gel baffler, therefore scratch will not be caused to it, pass through the screening of arc panel 7 and two pieces of silica gel bafflers 8
Package is covered, is conducive to when to aircraft engine turbo blade cleaning operation, the water lotion to flash will touch arc panel 7 and two
It on block silica gel baffler 8, then slides along its surface to sewage collecting groove 402, centralized collection is got up, will not be as traditional clear
When washing, water lotion flashes around on ground, leads to subsequent be not easily cleaned；It, can be by opening 401 row of valve after cleaning
Out in sewage collecting groove 402 centralized collection sewage.
The embodiment of the present invention is given for the purpose of illustration and description, and is not exhaustively or by this to send out
It is bright to be limited to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Choosing
Selecting and describe embodiment is and to make those skilled in the art to more preferably illustrate the principle of the present invention and practical application
It will be appreciated that the present invention is to design various embodiments suitable for specific applications with various modifications.
Claims (5)
1. the positioning mechanism of space shuttle engine turbine leaf cleaning equipment, it is characterised in that: the space shuttle engine whirlpool
The positioning mechanism of impeller blade cleaning equipment includes lower rectangular slab, universal wheel, hydraulic scissors mechanism, upper rectangular slab, sewage collecting shell
Body, valve, sewage collecting groove, telescopic rod, support rod, arc panel, rubber layer, silica gel baffler and metal stereotypes hoses；Institute
State and be provided with one piece of upper rectangular slab consistent with its size right above lower rectangular slab, and the lower rectangular slab with it is described on
It is connected between rectangular slab by the hydraulic scissors mechanism；The lower rectangular slab bottom face is respectively mounted at angle position in edge everywhere
There is the universal wheel with position-limit mechanism；The upper later half position of rectangular slab top end face is fixedly connected with one block of sewage
Assembling supporting member.
2. the positioning mechanism of space shuttle engine turbine leaf cleaning equipment as described in claim 1, it is characterised in that: described
Sewage collecting housing tip face offers the sewage collecting groove at one, and sewage collecting shell right side is provided with one
A valve being connected with the sewage collecting groove.
3. the positioning mechanism of space shuttle engine turbine leaf cleaning equipment as described in claim 1, it is characterised in that: described
Intermediate position is fixedly connected to the telescopic rod, and two telescopic rods at left and right sides of sewage collecting housing tip face
Top is connected with the support rod jointly.
4. the positioning mechanism of space shuttle engine turbine leaf cleaning equipment as described in claim 1, it is characterised in that: described
Support rod bottom face centre is welded with one piece of arc panel, and the arc panel inner face sticks one layer of rubber
Layer.
5. the positioning mechanism of space shuttle engine turbine leaf cleaning equipment as described in claim 1, it is characterised in that: described
Arc panel left and right ends is fixedly connected to one piece of silica gel baffler；It is provided with inside every piece of silica gel baffler
Four metal stereotypes hoses in the distribution of front and back rectangular array.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811032844.9A CN108941134A (en) | 2018-09-05 | 2018-09-05 | The positioning mechanism of space shuttle engine turbine leaf cleaning equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811032844.9A CN108941134A (en) | 2018-09-05 | 2018-09-05 | The positioning mechanism of space shuttle engine turbine leaf cleaning equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108941134A true CN108941134A (en) | 2018-12-07 |
Family
ID=64475202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811032844.9A Withdrawn CN108941134A (en) | 2018-09-05 | 2018-09-05 | The positioning mechanism of space shuttle engine turbine leaf cleaning equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108941134A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109622438A (en) * | 2018-12-27 | 2019-04-16 | 北京金风科创风电设备有限公司 | Cleaning device and system, cleaning control device, method and system |
| CN117564003A (en) * | 2024-01-17 | 2024-02-20 | 山西禧佑源民机完工中心有限公司 | Shell cleaning device for aircraft decoration |
-
2018
- 2018-09-05 CN CN201811032844.9A patent/CN108941134A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109622438A (en) * | 2018-12-27 | 2019-04-16 | 北京金风科创风电设备有限公司 | Cleaning device and system, cleaning control device, method and system |
| CN117564003A (en) * | 2024-01-17 | 2024-02-20 | 山西禧佑源民机完工中心有限公司 | Shell cleaning device for aircraft decoration |
| CN117564003B (en) * | 2024-01-17 | 2024-03-22 | 山西禧佑源民机完工中心有限公司 | Shell cleaning device for aircraft decoration |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181207 |