CN204099890U - Support collar structure applied to cryogenic pressure vessel - Google Patents

Support collar structure applied to cryogenic pressure vessel Download PDF

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Publication number
CN204099890U
CN204099890U CN201420467842.3U CN201420467842U CN204099890U CN 204099890 U CN204099890 U CN 204099890U CN 201420467842 U CN201420467842 U CN 201420467842U CN 204099890 U CN204099890 U CN 204099890U
Authority
CN
China
Prior art keywords
collar
inner bag
low
back shaft
pressure container
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
CN201420467842.3U
Other languages
Chinese (zh)
Inventor
王斌
杨忠
陆盼望
廖玲
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.)
Sinoma Science and Technology Suzhou Co Ltd
Original Assignee
Sinoma Science and Technology Suzhou 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 Sinoma Science and Technology Suzhou Co Ltd filed Critical Sinoma Science and Technology Suzhou Co Ltd
Priority to CN201420467842.3U priority Critical patent/CN204099890U/en
Application granted granted Critical
Publication of CN204099890U publication Critical patent/CN204099890U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/014Suspension means
    • F17C2203/018Suspension means by attachment at the neck
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG

Landscapes

  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The utility model discloses the supporting sleeve ring structure being applied to low-temperature pressure container, low-temperature pressure container has inner bag and outer courage, supporting mechanism is provided with between inner bag and outer courage, the outer wall of inner bag is provided with back shaft, supporting mechanism comprises supporting frame and collar group, collar group is made up of three collars, and second collar is epoxy glass steel collar; Second collar is sliding is secured to the 3rd and first between the collar, and back shaft second collar fixes attaching.Apply supporting sleeve ring structure of the present utility model, second collar be connected with back shaft is epoxy glass steel collar, and the thermal conductivity of fiber glass epoxy, well below stainless thermal conductivity, effectively reduces the heat trnasfer between inner bag and the external world; Back shaft and second collar servo-actuated, avoid tensile stress when inner bag expands with heat and contract with cold or pressure stress to the impact of back shaft, between second collar and first collar, leave gap, decrease direct heat trnasfer between the two, meanwhile, in collar boxing termination process, second collar can not be damaged.

Description

Be applied to the supporting sleeve ring structure of low-temperature pressure container
Technical field
The utility model relates to a kind of supporting sleeve ring structure, particularly relates to a kind of supporting sleeve ring structure being applied to low-temperature pressure container.
Background technique
Along with the rapid economic development of society, sharply strengthen as gas usage such as rock gas, helium, oxygen, at present for above-mentioned gas, there is multiple storage and receive container, wherein, low-temperature pressure container, by low-temperature storage liquid gas, is compared, the storage volume of its compression is larger, and safer, especially as automobile-used LNG gas cylinder, use amount rises year by year.Low-temperature pressure container use principle carrys out storing liquefied gas by low temperature, so thermal insulation property just seems particularly important, low-temperature pressure container all adopts the sandwich structure of inside and outside two courages, inner bag adopts support or 2 supporting structures usually at 8, and reduce heat trnasfer except relying on laminated vacuum layer, be secondly exactly control the heat trnasfer in supporting structure.
In prior art, generally adopt full-metallic to design for supporting structure, the heat trnasfer of metal is very high, can have a strong impact on the static evaporation rate of low-temperature pressure container.
Model utility content
The purpose of this utility model is to solve above-mentioned technical problem, proposes the supporting sleeve ring structure being applied to low-temperature pressure container.
The purpose of this utility model, will be achieved by the following technical programs:
1. be applied to the supporting sleeve ring structure of low-temperature pressure container, described low-temperature pressure container has inner bag and outer courage, is provided with supporting mechanism between described inner bag and outer courage,
It is characterized in that: the outer wall of described inner bag is provided with back shaft, described supporting mechanism comprises supporting frame and is fixedly installed on the collar group of supporting frame, described collar group comprises first collar and the 3rd collar that fix attaching, and second collar of sliding installation in first collar and the 3rd collar, described back shaft to be connected in collar group and to be fixedly connected with second collar.
Preferably, described second collar is epoxy glass steel collar.
Preferably, described second collar sliding installation in the 3rd collar and the end of second collar be limited in first collar towards the ring wall of the 3rd collar and the 3rd collar towards the end face of first collar between.
Preferably, between the end of described second collar and the ring wall of first collar, there is 2mm gap.
Preferably, the end sidewalls of described second collar and the internal ring wall of first collar have gap.
Preferably, between described first collar and the 3rd collar for being welded and fixed.
The beneficial effects of the utility model are mainly reflected in:
1. second collar be connected with back shaft is epoxy glass steel collar, and the thermal conductivity of fiber glass epoxy, well below stainless thermal conductivity, effectively reduces the heat trnasfer between inner bag and the external world;
2. second collar has linear displacement first and the 3rd in the collar, and back shaft and second collar servo-actuated, when inner bag expands with heat and contract with cold, back shaft carrys out adjusted position by the displacement of second collar, avoids the impact of tensile stress or pressure stress;
3. leave gap between second collar and first collar, decrease direct heat trnasfer between the two, meanwhile, in first collar and the 3rd collar welding process, can not produce second collar and damage.
Accompanying drawing explanation
Fig. 1 is the structural representation that the utility model is applied to the supporting sleeve ring structure of low-temperature pressure container.
Fig. 2 is the structural representation that the utility model is applied to collar group in the supporting sleeve ring structure of low-temperature pressure container.
Embodiment
The utility model provides a kind of supporting sleeve ring structure being applied to low-temperature pressure container, reduces inner bag and extraneous heat trnasfer, prevents inner bag from expanding with heat and contract with cold to low-temperature pressure container generation damage simultaneously.
As depicted in figs. 1 and 2, be applied to the supporting sleeve ring structure of low-temperature pressure container, low-temperature pressure container has inner bag 1 and outer courage 2, supporting mechanism 3 is provided with between inner bag 1 and outer courage 2, the outer wall of inner bag 1 is provided with back shaft 4, supporting mechanism 3 comprises supporting frame 5 and is fixedly installed on the collar group 6 of supporting frame 5, collar group 6 comprises first collar 61 and the 3rd collar 63 that fix attaching, and second collar 61 of sliding installation in first collar 61 and the 3rd collar 63, back shaft 4 to be connected in collar group 6 and to be fixedly connected with second collar 62.Back shaft and second collar servo-actuated, when inner bag expands with heat and contract with cold, back shaft regulates self-position by the displacement of second collar, avoids the impact of tensile stress or pressure stress.
Wherein, the second collar 62 sliding installation in the 3rd collar 63 and the end 621 of second collar 62 be limited in first collar 61 towards the ring wall 611 of the 3rd collar 63 and the 3rd collar 63 towards the end face 631 of first collar 61 between.Second collar 62 is epoxy glass steel collar, and the thermal conductivity of fiber glass epoxy, well below stainless thermal conductivity, effectively reduces the heat trnasfer between inner bag and the external world.The endoporus that second collar 62 is prolonging the 3rd collar slides, and the end face that the end of second collar is subject to the ring wall of first collar and the 3rd collar is spacing, and back shaft and second collar servo-actuated, when inner bag expands with heat and contract with cold, back shaft regulates self-position by the displacement of second collar, avoids the impact of tensile stress or pressure stress.
In addition, between the end 621 of second collar 62 and the ring wall 611 of first collar 61, there is 2mm gap.End 621 sidewall of second collar 62 and the internal ring wall 612 of first collar 61 have gap 613.Gap decreases the direct heat trnasfer between first collar 61 and second collar 62, meanwhile, in first collar 61 and the 3rd collar 63 welding process, can not produce damage second collar 62.
Finally, between first collar 61 and the 3rd collar 63 for being welded and fixed.
The utility model still has numerous embodiments, all employing equivalents or equivalent transformation and all technological schemes formed, and all drops within protection domain of the present utility model.

Claims (6)

1. be applied to the supporting sleeve ring structure of low-temperature pressure container, described low-temperature pressure container has inner bag and outer courage, is provided with supporting mechanism between described inner bag and outer courage,
It is characterized in that: the outer wall of described inner bag is provided with back shaft, described supporting mechanism comprises supporting frame and is fixedly installed on the collar group of supporting frame, described collar group comprises first collar and the 3rd collar that fix attaching, and second collar of sliding installation in first collar and the 3rd collar, described back shaft to be connected in collar group and to be fixedly connected with second collar.
2. be applied to the supporting sleeve ring structure of low-temperature pressure container according to claim 1, it is characterized in that: described second collar is epoxy glass steel collar.
3. be applied to the supporting sleeve ring structure of low-temperature pressure container according to claim 1, it is characterized in that: described second collar sliding installation in the 3rd collar and the end of second collar be limited in first collar towards the ring wall of the 3rd collar and the 3rd collar towards the end face of first collar between.
4. according to claim 1 or 3, be applied to the supporting sleeve ring structure of low-temperature pressure container, it is characterized in that: between the end of described second collar and the ring wall of first collar, there is 2mm gap.
5. according to claim 1 or 3, be applied to the supporting sleeve ring structure of low-temperature pressure container, it is characterized in that: the end sidewalls of described second collar and the internal ring wall of first collar have gap.
6. be applied to the supporting sleeve ring structure of low-temperature pressure container according to claim 1, it is characterized in that: for being welded and fixed between described first collar and the 3rd collar.
CN201420467842.3U 2014-08-19 2014-08-19 Support collar structure applied to cryogenic pressure vessel Expired - Lifetime CN204099890U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420467842.3U CN204099890U (en) 2014-08-19 2014-08-19 Support collar structure applied to cryogenic pressure vessel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420467842.3U CN204099890U (en) 2014-08-19 2014-08-19 Support collar structure applied to cryogenic pressure vessel

Publications (1)

Publication Number Publication Date
CN204099890U true CN204099890U (en) 2015-01-14

Family

ID=52268319

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420467842.3U Expired - Lifetime CN204099890U (en) 2014-08-19 2014-08-19 Support collar structure applied to cryogenic pressure vessel

Country Status (1)

Country Link
CN (1) CN204099890U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105114803A (en) * 2015-07-07 2015-12-02 郑州轻工业学院 Vertical low-temperature storage tank with sliding lantern ring supporting mechanism
CN106382455A (en) * 2016-09-05 2017-02-08 荆门宏图特种飞行器制造有限公司 Vertical cryogenic container
CN111853527A (en) * 2020-08-10 2020-10-30 江苏国富氢能技术装备有限公司 A movable end insulation support structure of a vacuum insulation container

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105114803A (en) * 2015-07-07 2015-12-02 郑州轻工业学院 Vertical low-temperature storage tank with sliding lantern ring supporting mechanism
CN106382455A (en) * 2016-09-05 2017-02-08 荆门宏图特种飞行器制造有限公司 Vertical cryogenic container
CN106382455B (en) * 2016-09-05 2018-09-11 荆门宏图特种飞行器制造有限公司 Vertical low temperature container
CN111853527A (en) * 2020-08-10 2020-10-30 江苏国富氢能技术装备有限公司 A movable end insulation support structure of a vacuum insulation container

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C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20150114

CX01 Expiry of patent term