CN202836903U - Cabin sealing performance test device - Google Patents
Cabin sealing performance test device Download PDFInfo
- Publication number
- CN202836903U CN202836903U CN 201220520635 CN201220520635U CN202836903U CN 202836903 U CN202836903 U CN 202836903U CN 201220520635 CN201220520635 CN 201220520635 CN 201220520635 U CN201220520635 U CN 201220520635U CN 202836903 U CN202836903 U CN 202836903U
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- CN
- China
- Prior art keywords
- test device
- performance test
- cabin
- sealing performance
- cabin sealing
- 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.)
- Expired - Lifetime
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Abstract
The utility model discloses a cabin sealing performance test device. The cabin sealing performance test device is provided with a sealing cover (1) connected with a hatch flange (3) through bolts (2). Stripper rubber (4) is arranged between the sealing cover (1) and the hatch flange (3). A hollow round tube (5) is arranged on the sealing cover (1) and connected with one end of a U-shaped tube pressure gage (7) through a soft pipe (6). The cabin sealing performance test device has the advantages that the device can reflect the amount of pressure in real time in the process of pressure rising, and an excessive pressure rising phenomenon is avoided; experiment efficiency is improved; and the device is low in cost, reusable and easy and convenient to use.
Description
Technical field:
The utility model relates to a kind of in the shipbuilding process, is used for the test unit of the close property in cabin of test.
Background technology:
In order to check whether the cabin exists the problems such as leakage, seepage, need the close property in chamber in test boats and ships cabin.Tested traditional mode in the past and be the cabin pressurization, and the Bonding pressure table carries out reading, reading again after after a while, relatively twice measured value has or not obvious decline.Have the delay of certain hour because of tensimeter its reading in pressurization, easily cause excessively boosting, and then cause tensimeter to damage, and the cabin is because of the excessive generation distortion of pressure.
Summary of the invention:
The utility model provides a kind of avoiding excessively to boost for the above-mentioned deficiency of prior art, simple in structure, easy to operate cabin tightness test device.
Technical solution of the present utility model is: a kind of cabin tightness test device, be provided with gland bonnet, it is connected with the hatch flange by bolt, between gland bonnet and hatch flange stripper rubber is set, be provided with hollow circular-tube at gland bonnet, hollow circular-tube is connected with an end of U-shaped tube manometer by flexible pipe.
The utility model mainly is the fitting device that designs for the cabin of carrying out in the shipbuilding process close property experiment, is that scale by U-shaped tube manometer reads the two ends mercury pressure poor, to calculate pressure value.The utility model has the advantage of: 1. device can reflect pressure size immediately in the process of boosting, the generation of the phenomenon of avoiding excessively boosting; 2. improve conventional efficient; 3. this installation cost is cheap, and can reuse, and is easy to use.
Description of drawings:
Fig. 1 is structural representation of the present utility model.
Embodiment:
Further specify embodiment of the present utility model below in conjunction with accompanying drawing.
As shown in Figure 1, a kind of cabin tightness test device is provided with gland bonnet 1, it is connected with hatch flange 3 by bolt 2,3 of gland bonnet 1 and hatch flanges arrange stripper rubber 4, are provided with hollow circular-tube 5 at gland bonnet 1, and hollow circular-tube 5 is connected with an end of U-shaped tube manometer 7 by flexible pipe 6.
Claims (1)
1. cabin tightness test device, it is characterized in that: be provided with gland bonnet (1), it is connected with hatch flange (3) by bolt (2), between gland bonnet (1) and hatch flange (3) stripper rubber (4) is set, be provided with hollow circular-tube (5) at gland bonnet (1), hollow circular-tube (5) is connected with an end of U-shaped tube manometer (7) by flexible pipe (6).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220520635 CN202836903U (en) | 2012-10-11 | 2012-10-11 | Cabin sealing performance test device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220520635 CN202836903U (en) | 2012-10-11 | 2012-10-11 | Cabin sealing performance test device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202836903U true CN202836903U (en) | 2013-03-27 |
Family
ID=47948585
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220520635 Expired - Lifetime CN202836903U (en) | 2012-10-11 | 2012-10-11 | Cabin sealing performance test device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202836903U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103454045A (en) * | 2013-08-21 | 2013-12-18 | 贵州虹智精密轴承有限责任公司 | Leakproofness detection device of clutch bearing of silicone oil fan and method thereof |
CN106840555A (en) * | 2016-12-27 | 2017-06-13 | 重庆维庆液压机械有限公司 | Hydraulic cylinder air tightness detection apparatus |
CN113776757A (en) * | 2021-09-17 | 2021-12-10 | 大连船舶重工集团有限公司 | Leakage monitoring and processing system of B-type independent storage cabin |
-
2012
- 2012-10-11 CN CN 201220520635 patent/CN202836903U/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103454045A (en) * | 2013-08-21 | 2013-12-18 | 贵州虹智精密轴承有限责任公司 | Leakproofness detection device of clutch bearing of silicone oil fan and method thereof |
CN106840555A (en) * | 2016-12-27 | 2017-06-13 | 重庆维庆液压机械有限公司 | Hydraulic cylinder air tightness detection apparatus |
CN106840555B (en) * | 2016-12-27 | 2018-12-07 | 重庆维庆液压机械有限公司 | Hydraulic cylinder air tightness detection apparatus |
CN113776757A (en) * | 2021-09-17 | 2021-12-10 | 大连船舶重工集团有限公司 | Leakage monitoring and processing system of B-type independent storage cabin |
CN113776757B (en) * | 2021-09-17 | 2023-09-01 | 大连船舶重工集团有限公司 | Leakage monitoring processing system of B-type independent storage cabin |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term |
Granted publication date: 20130327 |
|
CX01 | Expiry of patent term |