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KR102640355B1 - Cryogenic compressed gas tank having insulation structure on the neck - Google Patents

Cryogenic compressed gas tank having insulation structure on the neck Download PDF

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Publication number
KR102640355B1
KR102640355B1 KR1020220187351A KR20220187351A KR102640355B1 KR 102640355 B1 KR102640355 B1 KR 102640355B1 KR 1020220187351 A KR1020220187351 A KR 1020220187351A KR 20220187351 A KR20220187351 A KR 20220187351A KR 102640355 B1 KR102640355 B1 KR 102640355B1
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KR
South Korea
Prior art keywords
neck
pressure gas
container body
container
insulation
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KR1020220187351A
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Korean (ko)
Inventor
김성철
Original Assignee
김성철
이구연
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Priority to KR1020220187351A priority Critical patent/KR102640355B1/en
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    • 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
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/12Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge with provision for thermal insulation
    • 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
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/002Details of vessels or of the filling or discharging of vessels for vessels under pressure
    • 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
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/06Closures, e.g. cap, breakable member
    • 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0109Shape cylindrical with exteriorly curved end-piece
    • 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/056Small (<1 m3)
    • 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
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0345Fibres
    • F17C2203/035Glass wool
    • 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
    • F17C2203/03Thermal insulations
    • F17C2203/0375Thermal insulations by gas
    • F17C2203/0383Air
    • 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
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0621Single wall with three layers
    • 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/228Assembling processes by screws, bolts or rivets
    • 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/012Hydrogen
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30Hydrogen technology
    • Y02E60/32Hydrogen storage

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

본 발명은 용기본체의 목부에 급격한 열손실을 차단할 수 있는 단열 구조가 설치되어 저장효율이 높아지도록 한 단열구조를 갖는 극저온 고압가스 용기를 제공한다. 본 발명의 적절한 실시 형태에 따르면, 고압가스 입출구에 나사홀이 형성된 목부를 갖도록 금속 라이너로 제작된 용기본체와, 용기본체의 외면에 목부의 일부를 노출시킨 상태에서 탄소유리섬유 복합재로 접합시킨 용기본체 외피층과 다층단열층으로 이루어지되, 용기본체의 목부에서 외부로 노출되는 부분을 감싸서 급격한 열손실을 방지하기 위해 GFRP로 제작된 목부단열캡이 목부에 나사 결합되어 있는 것을 특징으로 한다.The present invention provides a cryogenic high-pressure gas container having an insulating structure to increase storage efficiency by installing an insulating structure that can block rapid heat loss at the neck of the container body. According to a preferred embodiment of the present invention, a container body made of a metal liner having a neck with a screw hole formed at the high-pressure gas inlet and outlet, and a container bonded with a carbon glass fiber composite material with a portion of the neck exposed to the outer surface of the container body. It is composed of a body shell layer and a multi-layer insulation layer, and is characterized by a neck insulation cap made of GFRP screwed to the neck to prevent rapid heat loss by covering the externally exposed portion of the neck of the container body.

Description

목부에 단열구조를 갖는 극저온 고압가스 용기{Cryogenic compressed gas tank having insulation structure on the neck}Cryogenic compressed gas tank having insulation structure on the neck}

본 발명은 극저온 고압가스 용기에 관한 것으로, 특히 용기본체의 목부에 급격한 열손실을 차단할 수 있는 단열 구조가 설치되어 저장효율이 높아지도록 한 단열구조를 갖는 극저온 고압가스 용기에 관한 것이다.The present invention relates to a cryogenic, high-pressure gas container, and in particular, to a cryogenic, high-pressure gas container having an insulating structure that can block rapid heat loss at the neck of the container body to increase storage efficiency.

극저온 고압 수소탱크(CCH2;Cryogenic Compressed Hydrogen)는 액체수소(-253℃) 또는 극저온 수소가스(-100~-253℃)를 저장할 수 있으면서 동시에 최대 350bar까지 견딜 수 있는 저장용기이다.Cryogenic Compressed Hydrogen (CCH2) is a storage container that can store liquid hydrogen (-253℃) or cryogenic hydrogen gas (-100~-253℃) and can withstand up to 350 bar.

기존 액체수소탱크의 경우, 스테인레스강 2중 진공벽 구조의 고성능 단열기능을 갖는 용기로 사용압은 15bar 이하이다. 따라서 액체수소가 기화되어 용기 내부의 증기압이 상승하여 15bar 이상이 되면, 안전밸브 또는 릴리프 밸브를 작동시켜 기화된 수소가스를 배출해야 한다. 일반적으로 하루 이내에 15bar 이상에 도달하여 수소 가스 배출이 시작된다. CCH2 탱크는 극저온을 저장하면서 동시에 내압구조를 가지기 때문에 액체수소 저장시 릴리프 밸브가 열리는 시점이 7일 이상 늦춰진다. CCH2 탱크에 액체수소가 아닌 극저온 수소가스를 고압으로 저장할 수 있는데 이 경우, 이론적으로 저장효율이 상온 고압용기 대비 150~200%에 달한다. 유럽, 미국에서는 20여년전부터 CCH2 탱크(용기)의 연구개발이 진행되어 왔고, 최근 CCH2 용기에 대한 인증기준 수립과 상용화를 준비하고 있다.In the case of the existing liquid hydrogen tank, it is a container with a stainless steel double vacuum wall structure and high performance insulation function, and the operating pressure is 15 bar or less. Therefore, when liquid hydrogen is vaporized and the vapor pressure inside the container rises to over 15 bar, the safety valve or relief valve must be operated to discharge the vaporized hydrogen gas. Typically, hydrogen gas emissions begin when the temperature reaches 15 bar or more within a day. Because the CCH2 tank stores extremely low temperatures and has a pressure-resistant structure, the opening of the relief valve is delayed by more than 7 days when storing liquid hydrogen. Cryogenic hydrogen gas, rather than liquid hydrogen, can be stored at high pressure in the CCH2 tank. In this case, theoretically, the storage efficiency reaches 150 to 200% compared to room temperature and high pressure containers. In Europe and the United States, research and development on CCH2 tanks (vessels) have been underway for over 20 years, and certification standards for CCH2 containers have recently been established and preparations are being made for commercialization.

현재 4가지 유형의 구조를 갖는 수소 저장 탱크가 제안되어 있다. 제1 타입은 용기 전체가 금속재질(스틸, 알루미늄) 라이너로 구성된 것이고, 제2 타입은 금속재질(스틸, 알루미늄) 라이너에 몸통부분을 유리(탄소)섬유 복잡재료로 보강한 형태이고, 제3 타입은 금속 라이너 전체에 탄소(유리)섬유 복합재료를 보강한 형태이고, 제4 타입은 플라스틱과 같은 비금속 라이너에 탄소(유리)섬유 복합재료로 용기 전체를 보강한 형태이다. 여기서, 제3 타입의 경우, 추가적으로 그 외부를 고성능 단열재(예로, 단열매트, 진공단열판, 이중 진공 단열층 등)로 감싸는 구조가 연구되고 있다.Hydrogen storage tanks with four types of structures are currently proposed. The first type is one in which the entire container is made up of a metal material (steel, aluminum) liner, the second type is a type in which the body is reinforced with a glass (carbon) fiber complex material on a metal material (steel, aluminum) liner, and the third type is a container made of metal (steel, aluminum). Type 4 is a type in which the entire container is reinforced with a carbon (glass) fiber composite material on a metal liner, and the fourth type is a type in which the entire container is reinforced with a carbon (glass) fiber composite material on a non-metal liner such as plastic. Here, in the case of the third type, a structure that additionally surrounds the outside with a high-performance insulating material (e.g., insulating mat, vacuum insulating plate, double vacuum insulating layer, etc.) is being studied.

그런데, 연구된 제3 타입의 경우에도 기존의 내압구조나 다층 단열구조로도 외부밸브 또는 배관이 연결되는 넥(neck)부의 열손실을 차단할 수 없어 저장효율을 높이는데 한계가 있다. 따라서 CCH2 탱크에 있어 복합재료로 금속 라이너를 보강하되 넥부의 열손실을 차단할 수 있는 방안이 필요하다.However, even in the case of the third type studied, there is a limit to increasing storage efficiency because heat loss at the neck where external valves or pipes are connected cannot be blocked even with the existing pressure-resistant structure or multi-layer insulation structure. Therefore, in the CCH2 tank, a method is needed to reinforce the metal liner with composite materials and block heat loss at the neck.

본 발명의 배경이 되는 기술로는 한국 등록특허 등록번호 제10-0469636호(특허문헌 1)로서, '복합재료 고압용기용 고밀폐도 금속성 노즐보스'가 제안되어 있다. 이는 라이너 내부에서 탄성재료로 된 실링과 조임쇠를 이용하여 노즐보스와 라이너가 만나는 경계지점을 견고하게 밀폐시킴과 동시에 금속성 노즐보스를 사용한 복합재료 용기를 장시간 사용할 때 노즐보스와 라이너 사이의 계면 분리로 인하여 발생하는 가스의 누출을 방지하도록 한 것이다. 그러나 이 배경기술은 노즐보스의 노즐 머리부가 외부에 그대로 노출되어 열손실을 차단할 수 없다. The technology behind the present invention is Korean Patent Registration No. 10-0469636 (Patent Document 1), which proposes 'high-tightness metallic nozzle boss for composite material high-pressure vessel'. This uses seals and fasteners made of elastic material inside the liner to firmly seal the boundary point where the nozzle boss and liner meet, and at the same time, when a composite container using a metallic nozzle boss is used for a long time, the interface between the nozzle boss and the liner is separated. This is to prevent gas leakage. However, this background technology cannot prevent heat loss because the nozzle head of the nozzle boss is exposed to the outside.

본 발명의 배경이 되는 다른 기술로는 한국 등록특허 등록번호 제10-2432512호(특허문헌 2)로서, '다중 가압구조의 노즐보스를 갖는 고압가스 저장탱크'가 제안되어 있다. 이는 노즐보스와 라이너 사이의 밀폐성 저하가 발생되지 않으며, 밸브 착탈로 인하여 반복적인 비틀림 하중이 가해지는 노즐보스와 라이너 사이의 계면이 상호 분리되는 현상을 방지할 수 있도록 한 것이다. 그러나 이 배경기술은 제2가압결합부재를 적용하여 노즐보스가 매립되어 있는 라이너의 내/외측면과 노즐보스의 가압 밀착력이 점차적으로 증가되도록 한 것으로 제2가압결합부재가 외부에 그대로 노출되어 열손실을 차단할 수 없다. Another technology that forms the background of the present invention is Korean Patent Registration No. 10-2432512 (Patent Document 2), which proposes a 'high-pressure gas storage tank with a nozzle boss of a multi-pressure structure'. This prevents deterioration of the airtightness between the nozzle boss and the liner, and prevents the phenomenon of separation of the interface between the nozzle boss and the liner, where repeated torsional loads are applied due to valve attachment and detachment. However, this background technology applies a second pressure coupling member to gradually increase the pressure adhesion between the inner and outer surfaces of the liner in which the nozzle boss is embedded and the nozzle boss. The second pressure coupling member is exposed to the outside, causing heat. Loss cannot be prevented.

한국 등록특허 등록번호 제10-0469636호Korean Patent Registration No. 10-0469636 한국 등록특허 등록번호 제10-2432512호Korean Patent Registration No. 10-2432512

본 발명은 용기본체의 목부에 급격한 열손실을 차단할 수 있는 단열 구조가 설치되어 저장효율이 높아지도록 한 단열구조를 갖는 극저온 고압가스 용기를 제공함에 그 목적이 있다.The purpose of the present invention is to provide a cryogenic high-pressure gas container having an insulating structure that can block rapid heat loss at the neck of the container body to increase storage efficiency.

본 발명의 적절한 실시 형태에 따르면, 고압가스 입출구에 나사홀이 형성된 목부를 갖도록 금속 라이너로 제작된 용기본체와, 용기본체의 외면에 목부의 일부를 노출시킨 상태에서 탄소유리섬유 복합재로 접합시킨 용기본체 외피층으로 이루어지되, 용기본체의 목부에서 외부로 노출되는 부분을 감싸서 급격한 열손실을 방지하기 위해 GFRP로 제작된 목부단열캡이 목부에 나사 결합되어 있고, 상기 용기본체의 목부 내면에는 저온에서도 금속탄성력을 발휘하여 극저온 고압가스 용기에 접속되는 고압유출입튜브와의 실링기능을 유지하는 에너자이즈드링이 설치되고, 고압유출입튜브의 외면에 목부를 벗어난 구간으로 유리섬유 50중량부 이상이 포함된 유리섬유복합재로 피복된 복합단열층이 형성되어 있는 것을 특징으로 한다.According to a preferred embodiment of the present invention, a container body made of a metal liner having a neck with a screw hole formed at the high-pressure gas inlet and outlet, and a container bonded with a carbon glass fiber composite material with a portion of the neck exposed to the outer surface of the container body. The main body is made of an outer skin layer, and a neck insulation cap made of GFRP is screwed to the neck to prevent rapid heat loss by covering the externally exposed part of the neck of the container body, and the inner surface of the neck of the container body is covered with metal even at low temperatures. An energized ring is installed to maintain the sealing function with the high-pressure inflow and outflow tube connected to the cryogenic high-pressure gas container by exerting elasticity, and the section beyond the neck is installed on the outer surface of the high-pressure inflow and outflow tube. Glass containing more than 50 parts by weight of glass fiber. It is characterized in that a composite insulation layer covered with a fiber composite material is formed.

또한, 상기 목부단열캡은 목부의 노출된 외주면을 감싸는 원통형의 목부견착부, 목부견착부에서 절곡 연장되어 목부의 선단에 밀착되는 목부링판, 목부링판에서 고압가스 입출구를 향해 절곡되어 외면에 수나사부를 형성하는 목부체결부를 이루는 것을 특징으로 한다.In addition, the neck insulation cap has a cylindrical neck shoulder portion surrounding the exposed outer peripheral surface of the neck, a neck ring plate that is bent and extended from the neck shoulder portion and is in close contact with the tip of the neck, and a neck ring plate that is bent toward the high-pressure gas inlet and outlet to form a male thread on the outer surface. It is characterized by forming a neck fastening part.

삭제delete

또한, 다층단열층은 슈퍼 단열 매트(Super insulation mat), 에어로젤(Aerogel), 진공단열패널(Vaccum insulation pannel) 중 어느 하나로 이루어진 것을 특징으로 한다.In addition, the multi-layer insulation layer is characterized by being made of one of a super insulation mat, airgel, and vacuum insulation panel.

본 발명의 목부에 단열구조를 갖는 극저온 고압가스 용기에 따르면, 용기본체의 목부에 목부단열캡이 설치되어 급격한 열손실을 차단할 수 있다. 또한 에너자이드링의 설치로 목부와 고압유출입튜브의 사이로 누출되는 고압 가스를 방지할 수 있고, 고압유출입튜브에 유리섬유복합재로 피복된 복합단열층이 형성되어 수송배관을 통한 열손실을 차단할 수 있어 극저온 고압가스의 저장효율이 향상된다.According to the cryogenic high-pressure gas container having an insulating structure at the neck of the present invention, a neck insulation cap is installed on the neck of the container body to prevent rapid heat loss. In addition, the installation of an energized ring can prevent high-pressure gas leaking between the neck and the high-pressure inlet/outlet tube, and a composite insulation layer covered with a glass fiber composite material is formed on the high-pressure inlet/outlet tube to block heat loss through the transport piping, thereby preventing cryogenic temperatures. Storage efficiency of high-pressure gas is improved.

본 명세서에서 첨부되는 다음의 도면들은 본 발명의 바람직한 실시 예를 예시하는 것이며, 발명의 상세한 설명과 함께 본 발명의 기술사상을 더욱 이해시키는 역할을 하는 것이므로, 본 발명은 첨부한 도면에 기재된 사항에만 한정되어서 해석되어서는 아니 된다.
도 1은 본 발명의 실시 예에 따른 극저온 고압가스 용기의 사시도.
도 2는 도 1의 분해사시도.
도 3은 도 1에 적용된 용기본체의 사시도.
도 4는 도 1의 극저온 고압가스 용기에서 목부 결합부분의 단면도.
도 5는 도 1에 적용된 목부단열캡의 부분절단된 사시도.
The following drawings attached to this specification illustrate preferred embodiments of the present invention, and serve to further understand the technical idea of the present invention along with the detailed description of the invention. Therefore, the present invention is limited to the matters described in the attached drawings. It should not be interpreted as limited.
1 is a perspective view of a cryogenic high-pressure gas container according to an embodiment of the present invention.
Figure 2 is an exploded perspective view of Figure 1.
Figure 3 is a perspective view of the container body applied to Figure 1.
Figure 4 is a cross-sectional view of the neck joint portion of the cryogenic high-pressure gas container of Figure 1.
Figure 5 is a partially cut perspective view of the neck insulation cap applied to Figure 1.

아래에서 본 발명은 첨부된 도면에 제시된 실시 예를 참조하여 상세하게 설명이 되지만 제시된 실시 예는 본 발명의 명확한 이해를 위한 예시적인 것으로 본 발명은 이에 제한되지 않는다.Below, the present invention will be described in detail with reference to embodiments shown in the attached drawings, but the presented embodiments are illustrative for a clear understanding of the present invention, and the present invention is not limited thereto.

본 발명에 따른 극저온 고압가스 용기(10)는 액체수소(-253℃) 또는 극저온 수소가스(-100~-253℃)를 저장할 수 있으면서 동시에 최대 350bar까지 견딜 수 있는 저장용기이다.The cryogenic high-pressure gas container 10 according to the present invention is a storage container that can store liquid hydrogen (-253°C) or cryogenic hydrogen gas (-100 to -253°C) and can withstand up to 350 bar.

극저온 고압가스 용기(10)는 도 1 내지 도 4와 같이 고압가스 입출구(121a)에 나사홀(121b)이 형성된 목부(121)를 갖도록 금속 라이너로 제작된 용기본체(12)와, 용기본체(12)의 외면에 목부(121)의 일부를 노출시킨 상태에서 탄소유리섬유 복합재로 접합시킨 용기본체 외피층(14)과 다층단열층(15)으로 이루어진다.The cryogenic high-pressure gas container 10 includes a container body 12 made of a metal liner having a neck 121 with a screw hole 121b formed at the high-pressure gas inlet and outlet 121a, as shown in FIGS. 1 to 4, and the container body ( It consists of a container body outer skin layer 14 and a multi-layer insulation layer 15 bonded with a carbon glass fiber composite material with a portion of the neck 121 exposed to the outer surface of 12).

다층단열층(15)은 슈퍼 단열 매트(Super insulation mat), 에어로젤(Aerogel), 진공단열패널(Vaccum insulation pannel) 중 어느 하나로 이루어질 수 있다.The multi-layer insulation layer 15 may be made of any one of a super insulation mat, airgel, and vacuum insulation panel.

또한, 용기본체(12)의 목부(121)에서 외부로 노출되는 부분을 감싸서 급격한 열손실을 방지하기 위해 GFRP(유리섬유복합재)로 제작된 목부단열캡(16)이 목부(121)에 나사 결합되어 설치된다. 이때 목부단열캡(16)은 높은 비강도와 비강성을 위해 유리섬유 성분이 50중량부 이상이 함유된 GFRP(유리섬유복합재)로 제작됨이 바람직하다.In addition, in order to prevent rapid heat loss by covering the externally exposed portion of the neck 121 of the container body 12, a neck insulation cap 16 made of GFRP (glass fiber composite) is screwed to the neck 121. and installed. At this time, the neck insulation cap 16 is preferably made of GFRP (glass fiber composite) containing more than 50 parts by weight of glass fiber components for high specific strength and specific rigidity.

도 4 및 도 5와 같이 목부단열캡(16)은 목부(121)의 노출된 외주면을 감싸는 원통형의 목부견착부(161), 목부견착부(161)에서 절곡 연장되어 목부(121)의 선단에 밀착되는 목부링판(162), 목부링판(162)에서 고압가스 입출구(121a)를 향해 절곡되어 외면에 수나사부(153a)를 형성하는 목부체결부(163)를 이루어져 있다.4 and 5, the neck insulation cap 16 has a cylindrical neck shoulder portion 161 surrounding the exposed outer peripheral surface of the neck portion 121, and is bent and extended from the neck shoulder portion 161 to the tip of the neck portion 121. It consists of a neck ring plate 162 that is in close contact, and a neck fastening portion 163 that is bent from the neck ring plate 162 toward the high-pressure gas inlet and outlet 121a to form a male thread portion 153a on the outer surface.

따라서 도 4와 같이 목부단열캡(16)은 목부체결부(163)가 용기본체(12)의 목부(121)에 형성된 나사홀(121b)에 나사 체결됨으로써 용기본체(12)에 결합된다. 이때 목부단열캡(16)은 용기본체(12)의 목부(121)와 접하는 부분에 극저온 환경에서도 점착력을 유지하는 접착제가 접착되어 설치될 수 있다.Therefore, as shown in FIG. 4, the neck insulation cap 16 is coupled to the container body 12 by screwing the neck fastening portion 163 into the screw hole 121b formed in the neck 121 of the container body 12. At this time, the neck insulation cap 16 may be installed by attaching an adhesive that maintains adhesion even in a cryogenic environment to the portion in contact with the neck 121 of the container body 12.

이와 같이 목부단열캡(16)이 용기본체(12)의 목부(121)에 결합되어져 설치되면, 목부견착부(161), 목부링판(162) 및 목부체결부(163)를 목부(121)가 외부로 노출되는 방지할 뿐만 아니라 자체의 단열 작용에 의해 용기본체(12)의 목부(121)에서 열손실을 차단할 수 있고, 이로 인해 극저온 고압가스 용기(10)에 충진된 극저온 고압가스의 저장효율의 저하를 방지할 수 있다.In this way, when the neck insulation cap 16 is coupled and installed to the neck 121 of the container body 12, the neck shoulder portion 161, neck ring plate 162, and neck fastening portion 163 are connected to the neck 121. Not only does it prevent exposure to the outside, but it can also block heat loss from the neck 121 of the container body 12 through its own insulation effect, thereby increasing the storage efficiency of the cryogenic high-pressure gas filled in the cryogenic high-pressure gas container 10. Deterioration can be prevented.

한편, 용기본체(12)의 목부(121) 내면에는 저온에서도 금속탄성력을 발휘하여 극저온 고압가스 용기(10)에 접속되는 고압유출입튜브(20)와의 실링기능을 유지하는 에너자이즈드링(energized ring)(18)이 설치됨이 바람직하다. 에너자이즈드링(18)은 메탈스프링 또는 오링을 테프론 자켓과 조합하여 극저온에서도 계속적인 반발탄성을 유지할 수 있도록 제작된 것이다. 따라서 극저온 고압가스 용기(10)의 목부(121)와 고압유출입튜브(20)와의 사이로 극저온 고압가스가 누출되는 현상을 에너자이즈드링(18)의 강력한 밀폐 기능으로 방지할 수 있다.Meanwhile, on the inner surface of the neck 121 of the container body 12, there is an energized ring that exhibits metallic elasticity even at low temperatures and maintains a sealing function with the high-pressure inflow and outflow tube 20 connected to the cryogenic high-pressure gas container 10. ) (18) is preferably installed. The Energized Ring (18) is manufactured by combining a metal spring or O-ring with a Teflon jacket to maintain continuous rebound elasticity even at extremely low temperatures. Therefore, leakage of cryogenic high-pressure gas between the neck 121 of the cryogenic high-pressure gas container 10 and the high-pressure inflow/outlet tube 20 can be prevented by the strong sealing function of the energized ring 18.

이때 도 2 및 도 4와 같이 고압유출입튜브(20)의 외면에는 목부(121)를 벗어난 구간으로 유리섬유 50중량부 이상이 포함된 유리섬유복합재로 피복된 복합단열층(201)이 형성되어 구성됨이 바람직하다. 물론 추가적인 단열이 필요한 경우, 고압유출입튜브(20)에도 이중 진공벽 구조의 단열층을 추가로 부착할 수 있다.At this time, as shown in Figures 2 and 4, a composite insulation layer 201 coated with a glass fiber composite containing more than 50 parts by weight of glass fiber is formed on the outer surface of the high pressure inflow and outflow tube 20 in a section beyond the neck 121. desirable. Of course, if additional insulation is required, an additional insulation layer with a double vacuum wall structure can be attached to the high pressure inflow and outflow tube 20.

이같이 고압유출입튜브(20)에도 복합단열층(201)이 형성된 경우, 용기본체(12)의 목부(121) 뿐만 아니라 고압유출입튜브(20)를 통해 이동하는 수송구간에도 단열이 이루어져 열손실을 최대로 억제함으로써 극저온 고압 가스의 저장효율을 극대화할 수 있다.In this way, when the composite insulation layer 201 is formed in the high pressure inflow and outflow tube 20, not only the neck 121 of the container body 12 but also the transportation section moving through the high pressure inflow and outflow tube 20 is insulated to maximize heat loss. By suppressing this, the storage efficiency of cryogenic, high-pressure gas can be maximized.

지금까지 본 발명은 제시된 실시 예를 참조하여 상세하게 설명이 되었지만 이 분야에서 통상의 지식을 가진 자는 제시된 실시 예를 참조하여 본 발명의 기술적 사상을 벗어나지 않는 범위에서 다양한 변형 및 수정 발명을 만들 수 있을 것이다. 본 발명은 이와 같은 변형 및 수정 발명에 의하여 제한되지 않으며 다만 아래에 첨부된 청구범위에 의하여 제한된다. So far, the present invention has been described in detail with reference to the presented embodiments, but those skilled in the art can make various variations and modifications without departing from the technical spirit of the present invention with reference to the presented embodiments. will be. The present invention is not limited by such variations and modifications, but is limited by the claims appended below.

10: 극저온 고압가스 용기
121: 목부
121a: 고압가스 입출구
121b: 나사홀
14: 용기본체 외피층
15: 다층단열층
16: 목부단열캡
161: 목부견착부
162: 목부링판
163: 목부체결부
18: 에너자이즈드링
20: 고압유출입튜브
201: 복합단열층
10: Cryogenic high-pressure gas container
121: xylem
121a: High-pressure gas inlet and outlet
121b: screw hole
14: Container body outer layer
15: Multi-layer insulation layer
16: Neck insulation cap
161: Neck shoulder attachment
162: neck ring plate
163: Neck fastening part
18: Energize Drink
20: High pressure inflow and outflow tube
201: Composite insulation layer

Claims (5)

극저온 고압가스 용기(10)에 있어서,
고압가스 입출구(121a)에 나사홀(121b)이 형성된 목부(121)를 갖도록 금속 라이너로 제작된 용기본체(12)와, 용기본체(12)의 외면에 목부(121)의 일부를 노출시킨 상태에서 탄소유리섬유 복합재로 접합시킨 용기본체 외피층(14)과 다층단열층(15)으로 이루어지되,
용기본체(12)의 목부(121)에서 외부로 노출되는 부분을 감싸서 급격한 열손실을 방지하기 위해 GFRP(유리섬유복합재)로 제작된 목부단열캡(16)이 목부(121)에 나사 결합되어 있고,
상기 용기본체(12)의 목부(121) 내면에는 저온에서도 금속탄성력을 발휘하여 극저온 고압가스 용기(10)에 접속되는 고압유출입튜브(20)와의 실링기능을 유지하는 에너자이즈드링(18)이 설치되고, 고압유출입튜브(20)의 외면에 목부(121)를 벗어난 구간으로 유리섬유 50중량부 이상이 포함된 유리섬유복합재로 피복된 복합단열층(201)이 형성되어 있는 것을 특징으로 하는 목부에 단열구조를 갖는 극저온 고압가스 용기.
In the cryogenic high-pressure gas container (10),
A container body 12 made of a metal liner having a neck 121 with a screw hole 121b formed at the high-pressure gas inlet/outlet 121a, and a portion of the neck 121 exposed on the outer surface of the container body 12. It consists of a container body outer skin layer (14) and a multi-layer insulation layer (15) bonded with carbon glass fiber composite,
To prevent rapid heat loss by covering the externally exposed portion of the neck 121 of the container body 12, a neck insulation cap 16 made of GFRP (glass fiber composite) is screwed to the neck 121. ,
On the inner surface of the neck 121 of the container body 12, there is an energized ring 18 that exhibits metallic elasticity even at low temperatures and maintains a sealing function with the high pressure inflow and outflow tube 20 connected to the cryogenic high pressure gas container 10. A composite insulation layer (201) is formed on the outer surface of the high-pressure inflow and outflow tube (20), covered with a glass fiber composite material containing more than 50 parts by weight of glass fiber, in a section beyond the neck portion (121). A cryogenic, high-pressure gas container with an insulating structure.
제 1항에 있어서,
상기 목부단열캡(16)은 목부(121)의 노출된 외주면을 감싸는 원통형의 목부견착부(161), 목부견착부(161)에서 절곡 연장되어 목부(121)의 선단에 밀착되는 목부링판(162), 목부링판(162)에서 고압가스 입출구(121a)를 향해 절곡되어 외면에 수나사부를 형성하는 목부체결부(163)를 이루는 것을 특징으로 하는 목부에 단열구조를 갖는 극저온 고압가스 용기.
According to clause 1,
The neck insulation cap 16 includes a cylindrical neck shoulder portion 161 surrounding the exposed outer peripheral surface of the neck portion 121, and a neck ring plate 162 that is bent and extended from the neck shoulder portion 161 and is in close contact with the tip of the neck portion 121. ), a cryogenic high-pressure gas container with an insulating structure at the neck, characterized in that the neck ring plate 162 is bent toward the high-pressure gas inlet/outlet (121a) to form a neck fastening portion 163 forming a male screw portion on the outer surface.
삭제delete 제 1항에 있어서,
상기 다층단열층(15)은 슈퍼 단열 매트(Super insulation mat), 에어로젤(Aerogel), 진공단열패널(Vaccum insulation pannel) 중 어느 하나로 이루어진 것을 특징으로 하는 목부에 단열구조를 갖는 극저온 고압가스 용기.
According to clause 1,
The multi-layer insulation layer (15) is a cryogenic high-pressure gas container having an insulation structure at the neck, characterized in that it is made of one of a super insulation mat, airgel, and vacuum insulation panel.
삭제delete
KR1020220187351A 2022-12-28 2022-12-28 Cryogenic compressed gas tank having insulation structure on the neck KR102640355B1 (en)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100469636B1 (en) 2004-03-11 2005-02-02 주식회사 케이시알 The high gas-tighten metallic nozzle-boss for the high pressure composite vessel
CN102147048A (en) * 2011-01-17 2011-08-10 丁雨福 Vertical low-temperature heat insulation air bottle with special neck pipe
KR20170020092A (en) * 2015-08-13 2017-02-22 하이리움산업(주) Storage vessel for liquid hydrogen
JP2019007557A (en) * 2017-06-26 2019-01-17 中国工業株式会社 Pressure vessel and manufacturing method of the same
KR102432512B1 (en) 2022-01-26 2022-08-17 신병천 High-pressure gas storage tank with multiple pressurized nozzle boss

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100469636B1 (en) 2004-03-11 2005-02-02 주식회사 케이시알 The high gas-tighten metallic nozzle-boss for the high pressure composite vessel
CN102147048A (en) * 2011-01-17 2011-08-10 丁雨福 Vertical low-temperature heat insulation air bottle with special neck pipe
KR20170020092A (en) * 2015-08-13 2017-02-22 하이리움산업(주) Storage vessel for liquid hydrogen
JP2019007557A (en) * 2017-06-26 2019-01-17 中国工業株式会社 Pressure vessel and manufacturing method of the same
KR102432512B1 (en) 2022-01-26 2022-08-17 신병천 High-pressure gas storage tank with multiple pressurized nozzle boss

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