CN202836903U - Cabin sealing performance test device - Google Patents

Cabin sealing performance test device Download PDF

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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
Authority
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
Application number
CN 201220520635
Other languages
Chinese (zh)
Inventor
肖小永
江凌
陈涛
于庆福
宋林
张立兵
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dalian Shipbuilding Industry Co Ltd
Original Assignee
Dalian Shipbuilding Industry Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dalian Shipbuilding Industry Co Ltd filed Critical Dalian Shipbuilding Industry Co Ltd
Priority to CN 201220520635 priority Critical patent/CN202836903U/en
Application granted granted Critical
Publication of CN202836903U publication Critical patent/CN202836903U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

The cabin tightness test device
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).
CN 201220520635 2012-10-11 2012-10-11 Cabin sealing performance test device Expired - Lifetime CN202836903U (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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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C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130327

CX01 Expiry of patent term