CN109029873A - Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure - Google Patents
Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure Download PDFInfo
- Publication number
- CN109029873A CN109029873A CN201810407728.4A CN201810407728A CN109029873A CN 109029873 A CN109029873 A CN 109029873A CN 201810407728 A CN201810407728 A CN 201810407728A CN 109029873 A CN109029873 A CN 109029873A
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- CN
- China
- Prior art keywords
- clamping plate
- burning chamber
- chamber shell
- water pressure
- airborne
- 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
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/32—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
The present invention relates to missile propulsive plant technical fields, especially vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure, including sink, bracket, swivel mount, first burning chamber shell fixture and the second burning chamber shell fixture, bracket is placed in sink, the middle position two sides of swivel mount pass through rotating steadying bar and are located on bracket, first combustion chamber fixture is mounted on the upper end of swivel mount by screw and washer, second burning chamber shell fixture is mounted on the lower end of swivel mount by screw and washer, structure type between first burning chamber shell fixture and the second burning chamber shell fixture is identical.Water pressure test room is carried out to burning chamber shell the invention has the advantages that: the present invention, support is fixed; convenient for pouring after the water pressure test, securely and reliably, workpiece is protected; it is easy to operate, quick, versatile, it is suitable for the fixed clamping of the different size burning chamber shell water pressure test.
Description
Technical field
The present invention relates to missile propulsive plant technical field, especially vehicles, airborne 140 caliber missile propulsive plant hydraulic pressure detection dress
It sets.
Background technique
Traditional mode of operation is that it is raw not to be suitable for batch by artificial fixed combustion room housing, complicated for operation, low efficiency
Produce detection operation.
Therefore, it is necessary to propose vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure in response to the above problems.
Summary of the invention
Object of the present invention is to overcome deficiency in the prior art, vehicle, airborne 140 caliber missile propulsive plant hydraulic pressure are provided
Detection device.
In order to solve the above-mentioned technical problem, the present invention is achieved through the following technical solutions:
Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure, including sink, bracket, swivel mount, the first burning chamber shell
Fixture and the second burning chamber shell fixture, the bracket are placed in sink, and the middle position two sides of the swivel mount are logical
It crosses rotating steadying bar to be located on bracket, first combustion chamber fixture is mounted on the upper end of swivel mount by screw and washer, described
Second burning chamber shell fixture is mounted on the lower end of swivel mount, the first burning chamber shell fixture and by screw and washer
Structure type between two burning chamber shell fixtures is identical.
Preferably, the first burning chamber shell fixture includes first clamping plate, second clamping plate, the first rotating dog and the first card
Button, a side of the first clamping plate are connected by a side of the first rotating dog and second clamping plate, the first clamping plate it is another
A side is connect by the first buckle with another side of second clamping plate.
Preferably, the second burning chamber shell fixture includes third clamping plate, the 4th clamping plate, the second rotating dog and the second card
Button, a side of the third clamping plate are connect by the first rotating dog with a side of the 4th clamping plate, the third clamping plate it is another
A side is connect by the second buckle with another side of the 4th clamping plate.
Preferably, the bracket includes the first tripod, the second tripod and the first frame, first tripod and the
Two tripods are separately connected the left and right sides of the first frame.
Preferably, the rotation axis is erected on bracket by strut connecting bolt, the bolt.
Preferably, the swivel mount includes the second frame, and the middle position of second frame is provided with multiple cross bars.
Preferably, the length of the sink is 2000mm, width 706mm, depth 300mm.
Preferably, the length of first frame is 1100mm, width 529mm, and the length of second frame is
1070mm, width 325mm.
Water pressure test room is carried out to burning chamber shell the invention has the advantages that: the present invention, support is fixed, is convenient for hydraulic pressure
It pours after test, securely and reliably, workpiece is protected, it is easy to operate, quick, versatile, it is suitable for different size and burns
Clamping is fixed in the room housing water pressure test.
It is described further below with reference to technical effect of the attached drawing to design of the invention, specific structure and generation, with
It is fully understood from the purpose of the present invention, feature and effect.
Detailed description of the invention
Fig. 1 is structure chart of the invention;
Fig. 2 is main view of the invention;
Fig. 3 is top view of the invention;
Fig. 4 is rack assumption diagram of the invention;
Fig. 5 is the second frame construction drawing of the invention;
Fig. 6 is the first burning chamber shell clamp structure figure of the invention;
Fig. 7 is the second burning chamber shell clamp structure figure of the invention.
Specific embodiment
The embodiment of the present invention is described in detail below in conjunction with attached drawing, but the present invention can be defined by the claims
Implement with the multitude of different ways of covering.
Such as Fig. 1 is simultaneously combined shown in Fig. 2 to Fig. 7, vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure, including sink
1, bracket 2, swivel mount 3, the first burning chamber shell fixture 4 and the second burning chamber shell fixture 5, the bracket 2 are placed on sink 1
Interior, the middle position two sides of the swivel mount 3 pass through rotation axis 6 and are erected on bracket 1, first combustion chamber fixture 4
The upper end of swivel mount 3 is mounted on by screw 8 and washer 9,5 fixture of the second burning chamber shell is pacified by screw 8 and washer 9
Structure type mounted in the lower end of swivel mount 3, between the first burning chamber shell fixture 4 and the second burning chamber shell fixture 5
It is identical.
Further, the first burning chamber shell fixture 4 includes first clamping plate 15, second clamping plate 16, the first rotating dog
17 and first buckle 18, and a side of the first clamping plate 15 is connected by the first rotating dog 17 and a side of second clamping plate 16
It connecing, another side of the first clamping plate 15 is connect by the first buckle 18 with another side of second clamping plate 16, and described second
Burning chamber shell fixture 5 includes third clamping plate 19, the 4th clamping plate 20, the second rotating dog 21 and the second buckle 22, the third folder
A side of plate 19 is connect by the first rotating dog 21 with a side of the 4th clamping plate 20, another side of the third clamping plate 19
It is connect by the second buckle 22 with another side of the 4th clamping plate 20.
Wherein, the bracket 2 includes the first tripod 11, the second tripod 12 and the first frame 10, first triangle
Frame 11 and the second tripod 12 are separately connected the left and right sides of the first frame 10, and the rotation axis 6 passes through strut connecting bolt
7, the bolt 7 is erected on bracket 2.
In addition, the swivel mount 3 includes the second frame 13, the middle position of second frame 13 is provided with multiple cross bars
14, the length of the sink 1 is 2000mm, width 706mm, depth 300mm.
Wherein, the length of first frame 10 is 1100mm, width 529mm, and the length of second frame 13 is
1070mm, width 325mm.
The present invention carries out water pressure test room to burning chamber shell and support is fixed, convenient for pouring after the water pressure test, safety
Reliably, workpiece is protected, it is easy to operate, quick, versatile, it is solid to be suitable for the water pressure test of different size burning chamber shell
Determine clamping.
It is easy to operate by using the hydraulic pressure fixing tool, facilitate the progress of the water pressure test, swivel mount design facilitates water
Pouring tooling after pressure, the design of sink avoid after the water pressure test water sinuous flow everywhere.By selecting different fixtures to be able to use
The clamping of different housings is fixed, and the tooling versatility is improved.
Application method: vehicle, the airborne 140 caliber rocket projectile motor burning chamber shell hydraulic devices course of work: according to combustion
Burning room housing size selects suitable burning chamber shell fixture clamping on swivel mount, and burning chamber shell is then fixed to fixture
It is upper to carry out subsequent water pressure test operation, after the water pressure test is complete, the water in burning chamber shell can be poured out by rotating swivel mount, most
Shell is removed afterwards.
The preferred embodiment of the present invention has been described in detail above.It should be appreciated that those skilled in the art without
It needs creative work according to the present invention can conceive and makes many modifications and variations.Therefore, all technologies in the art
Personnel are available by logical analysis, reasoning, or a limited experiment on the basis of existing technology under this invention's idea
Technical solution, all should be within the scope of protection determined by the claims.
Claims (6)
1. vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: including sink, bracket, swivel mount,
One burning chamber shell fixture and the second burning chamber shell fixture, the bracket are placed in sink, the interposition of the swivel mount
It sets two sides and passes through rotating steadying bar and be located on bracket, first combustion chamber fixture is mounted on swivel mount by screw and washer
Upper end, the second burning chamber shell fixture is mounted on the lower end of swivel mount, first combustion chamber by screw and washer
Structure type between shell clamp and the second burning chamber shell fixture is identical;The first burning chamber shell fixture includes first
A side of clamping plate, second clamping plate, the first rotating dog and the first buckle, the first clamping plate passes through the first rotating dog and the second folder
A side of plate connects, and another side of the first clamping plate is connect by the first buckle with another side of second clamping plate;Institute
State the second burning chamber shell fixture include third clamping plate, the 4th clamping plate, the second rotating dog and second buckle, the third clamping plate
A side is connect by the first rotating dog with a side of the 4th clamping plate, and another side of the third clamping plate passes through the second buckle
It is connect with another side of the 4th clamping plate.
2. vehicle as described in claim 1, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: the branch
Frame includes the first tripod, the second tripod and the first frame, and first tripod and the second tripod are separately connected first
The left and right sides of frame.
3. vehicle as described in claim 1, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: described turn
Moving axis is erected on bracket by strut connecting bolt, the bolt.
4. vehicle as described in claim 1, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: the rotation
Pivoted frame includes the second frame, and the middle position of second frame is provided with multiple cross bars.
5. vehicle as described in claim 1, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: the water
The length of slot is 2000mm, width 706mm, depth 300mm.
6. vehicle as described in claim 1, airborne 140 caliber missile propulsive plant device for detecting water pressure, it is characterised in that: described
The length of one frame is 1100mm, and width 529mm, the length of second frame is 1070mm, width 325mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810407728.4A CN109029873A (en) | 2018-05-02 | 2018-05-02 | Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810407728.4A CN109029873A (en) | 2018-05-02 | 2018-05-02 | Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure |
Publications (1)
Publication Number | Publication Date |
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CN109029873A true CN109029873A (en) | 2018-12-18 |
Family
ID=64629685
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201810407728.4A Pending CN109029873A (en) | 2018-05-02 | 2018-05-02 | Vehicle, airborne 140 caliber missile propulsive plant device for detecting water pressure |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201757692U (en) * | 2010-07-13 | 2011-03-09 | 柳州六和方盛机械有限公司 | Reservoir leakage testing groove for air reservoir |
CN203426991U (en) * | 2013-08-13 | 2014-02-12 | 中国航空动力机械研究所 | Assembly vehicle used for assembling combustion chambers of aircraft engines |
CN204149072U (en) * | 2014-09-10 | 2015-02-11 | 天津市懿峰工贸有限公司 | A kind of auto production line frock clamp |
CN107462115A (en) * | 2017-08-04 | 2017-12-12 | 天津航天瑞莱科技有限公司 | A kind of guided missile simulation emission test system |
CN206804443U (en) * | 2017-06-26 | 2017-12-26 | 天津市华赛尔气体有限公司 | A kind of pouring device for gas cylinder inspection |
CN206847864U (en) * | 2017-06-05 | 2018-01-05 | 永高股份有限公司 | A kind of pipe fitting pressure testing machine |
-
2018
- 2018-05-02 CN CN201810407728.4A patent/CN109029873A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201757692U (en) * | 2010-07-13 | 2011-03-09 | 柳州六和方盛机械有限公司 | Reservoir leakage testing groove for air reservoir |
CN203426991U (en) * | 2013-08-13 | 2014-02-12 | 中国航空动力机械研究所 | Assembly vehicle used for assembling combustion chambers of aircraft engines |
CN204149072U (en) * | 2014-09-10 | 2015-02-11 | 天津市懿峰工贸有限公司 | A kind of auto production line frock clamp |
CN206847864U (en) * | 2017-06-05 | 2018-01-05 | 永高股份有限公司 | A kind of pipe fitting pressure testing machine |
CN206804443U (en) * | 2017-06-26 | 2017-12-26 | 天津市华赛尔气体有限公司 | A kind of pouring device for gas cylinder inspection |
CN107462115A (en) * | 2017-08-04 | 2017-12-12 | 天津航天瑞莱科技有限公司 | A kind of guided missile simulation emission test system |
Non-Patent Citations (1)
Title |
---|
何岩: "高效气瓶外测法的研究与应用", 《低温与特气》, vol. 36, no. 2, pages 8 - 10 * |
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