JPS63247588A - High-temperature heat-insulating structure - Google Patents
High-temperature heat-insulating structureInfo
- Publication number
- JPS63247588A JPS63247588A JP8126387A JP8126387A JPS63247588A JP S63247588 A JPS63247588 A JP S63247588A JP 8126387 A JP8126387 A JP 8126387A JP 8126387 A JP8126387 A JP 8126387A JP S63247588 A JPS63247588 A JP S63247588A
- Authority
- JP
- Japan
- Prior art keywords
- carbon
- hollow
- heat
- hollow container
- temperature
- 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.)
- Pending
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 17
- 229910052799 carbon Inorganic materials 0.000 claims description 17
- 238000009413 insulation Methods 0.000 claims description 17
- 229910052751 metal Inorganic materials 0.000 claims description 7
- 239000002184 metal Substances 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 5
- 239000011261 inert gas Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- 239000011810 insulating material Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 239000012774 insulation material Substances 0.000 description 2
- 229910052741 iridium Inorganic materials 0.000 description 2
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 229910052762 osmium Inorganic materials 0.000 description 2
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000010000 carbonizing Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- -1 etc. Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、高温断熱構造に関し、更に詳しくは、100
0〜3000℃の高温かつ不活性ガスまたは真空雰囲気
下で優れた断熱性能を有する高温断熱構造に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a high temperature insulation structure, and more specifically,
The present invention relates to a high-temperature insulation structure having excellent insulation performance at high temperatures of 0 to 3000°C and under an inert gas or vacuum atmosphere.
従来、1000〜3000℃の高温かつ不活性ガスまた
は真空雰囲気下における断熱材は炭素系断熱材が用いら
れており、その中でも炭素繊維をフェルト状にして積層
し、さらに所望の形に成型したものは高温真空炉などに
よく用いられている。また、タングステン、モリブデン
などの高融点金属もコイル状に巻いて熱遮蔽板として高
温真空ホットプレスなどに用いられている。Conventionally, carbon-based insulation materials have been used as insulation materials at high temperatures of 1000 to 3000°C and in an inert gas or vacuum atmosphere. Among these, carbon fibers are laminated in the form of felt and then molded into the desired shape. is often used in high-temperature vacuum furnaces. In addition, high-melting point metals such as tungsten and molybdenum are also wound into coils and used as heat shielding plates in high-temperature vacuum hot presses and the like.
第2図に従来から用いられているHIP(HotIso
static Press) (熱間等方圧成型、以下
HIPという)装置の一例を示している。第2図では、
4は発熱体、5は加圧部、6は成型用サンプル、7は断
熱壁、8は熱遮蔽コイルである。Figure 2 shows HIP (HotIso), which has been used conventionally.
An example of a static press (hot isostatic press, hereinafter referred to as HIP) device is shown. In Figure 2,
4 is a heating element, 5 is a pressurizing part, 6 is a sample for molding, 7 is a heat insulating wall, and 8 is a heat shielding coil.
上述した炭素繊維成型体は取扱い易さの点では優れてい
るが、毛羽立ちが多く短繊維となって飛散するので雰囲
気や被処理物を汚染し易いという難点がある。Although the above-mentioned carbon fiber molded product is excellent in terms of ease of handling, it has a drawback in that it has a lot of fuzz and becomes short fibers that are scattered and easily contaminate the atmosphere and the object to be treated.
また、成型に多くの工程を必要とし高価となるほか高融
点金属板での遮蔽は、熱輻射はある程度防ぐことができ
るが対流による熱伝導は防ぐことができないという問題
がある。In addition, it requires many molding steps and is expensive, and shielding with a high melting point metal plate can prevent heat radiation to a certain extent, but it cannot prevent heat conduction by convection.
さらに、炭素微小中空体をバインダで成型し、加熱炭化
して得たカーボンフオームも断熱材として使用されてい
るが、大型成型品や任意形状の成型品の製造が技術的に
困難であり、かつ高価である。Furthermore, carbon foam obtained by molding carbon micro hollow bodies with a binder and heating and carbonizing them is also used as a heat insulating material, but it is technically difficult to manufacture large molded products or molded products of arbitrary shapes, and It's expensive.
従来のHIP装置の例では、第2図に示すように熱遮蔽
コイル8は断熱特性が不十分であり、熱流の一部を遮蔽
するに過ず、従って、熱遮蔽コイル8の外側をさらに断
熱壁7で断熱する必要があった。In the example of a conventional HIP device, as shown in FIG. 2, the heat shielding coil 8 has insufficient insulation properties and only blocks part of the heat flow, so the outside of the heat shielding coil 8 is further insulated. It was necessary to insulate it with wall 7.
本発明は上述の問題点を解決するために提案されたもの
であり、以下に要約したような性質を有する高温断熱構
造を提供することを目的とするものである。The present invention has been proposed in order to solve the above-mentioned problems, and it is an object of the present invention to provide a high-temperature heat insulating structure having the properties summarized below.
■ダストが発生しにくい。■Dust is less likely to be generated.
■炭素微小中空体のままでは形状が維持できないので自
立型とする。■Since the shape cannot be maintained as a carbon micro hollow body, it is made into a self-supporting type.
■低熱伝導性とする。■Low thermal conductivity.
■カーボンフオームにせず炭素微小中空体を粒状のまま
用い優れた断熱性を保有させる。■Using fine hollow carbon particles in their granular form without converting them into carbon foam provides excellent heat insulation properties.
■簡便で取扱い易い。■Simple and easy to handle.
■加工性、施工性が優れている。■Excellent workability and workability.
■高温(1000〜3000℃)に耐える。■Withstands high temperatures (1000-3000℃).
本発明は上述の問題点を解決するものであり、1000
℃以上、3000℃以下の高温下の不活性ガスまたは真
空雰囲気下で使用する高温断熱構造に適用され次の技術
手段を採った。すなわち、1000℃以上でかつ使用温
度より高い融点を持つ金属(タングステン、モリブデン
、チタン、ニッケル、クロム、鉄、コバルト、銅、イリ
ジウム、オスミウム、ニオビウム、タンタルなどおよび
これらの合金)、セラミックス、炭素(黒鉛を含む)、
硼素、C/Cコンポジットなどからなる板でそれぞれ底
面、側面、上面を形成した中空容器の中空部に炭素微小
中空体を充填した。The present invention solves the above-mentioned problems and has 1000
The following technical measures were applied to high-temperature insulation structures used in inert gas or vacuum atmospheres at high temperatures between 3000°C and above. In other words, metals (tungsten, molybdenum, titanium, nickel, chromium, iron, cobalt, copper, iridium, osmium, niobium, tantalum, etc. and their alloys), ceramics, and carbon (such as tungsten, molybdenum, titanium, nickel, chromium, iron, cobalt, copper, iridium, osmium, niobium, tantalum, etc., and alloys thereof), which have a melting point of 1000°C or higher and higher than the operating temperature. (contains graphite),
The hollow part of a hollow container whose bottom, side, and top surfaces were formed with plates made of boron, C/C composite, etc., was filled with carbon microhollow bodies.
なお、中空容器の材質として、1000℃以上でかつ使
用温度より高い融点を持つ金属を使用したのは、任意形
状の容器を容易に造ることができるからである。Note that the reason why a metal having a melting point of 1000° C. or higher and higher than the operating temperature was used as the material for the hollow container is that a container of any shape can be easily manufactured.
本発明の高温断熱構造は、耐熱性材料で構成された中空
容器に充填した炭素微小中空体が熱伝導を妨げ良好な断
熱作用を果すことができる。また、炭素微小中空体をバ
インダなどで成型してカーボンフオームとしないので製
造コストを軽減することができる。In the high-temperature insulation structure of the present invention, the carbon micro hollow bodies filled in the hollow container made of a heat-resistant material prevent heat conduction and can achieve a good insulation effect. Further, since the carbon micro hollow bodies are not molded with a binder or the like to form carbon foam, manufacturing costs can be reduced.
第1図は本発明に基づく中空容器1を中空円筒としてH
IP装芒に適用した例である。laは上部蓋、2はクッ
ション材、3は炭素微小中空体、4は発熱体、5は加圧
部、6は成型品である。FIG. 1 shows a hollow container 1 according to the present invention as a hollow cylinder.
This is an example applied to IP awning. la is an upper lid, 2 is a cushioning material, 3 is a carbon micro hollow body, 4 is a heating element, 5 is a pressurizing part, and 6 is a molded product.
第2図に示す従来例とは異なり、中空容器1のみで優れ
た断熱壁を兼ねることができる。Unlike the conventional example shown in FIG. 2, the hollow container 1 alone can serve as an excellent heat insulating wall.
第1図は本発明の一例示に過ぎず、形状は使用部位と使
用方法によって任意に構成することができる0例えば、
炉壁の平面部であれば、立方体や直方体の中空容器に炭
素微小中空体を充填し、適宜止め具で炉壁に固定すれば
断熱性のよい炉壁を構築することができる。また、飛行
体の機体を高熱から保護する断熱材として使用するには
、機体の形状に合せた金属の中空成型体に炭素微小中空
体を充填して固定すればよい6例えば、大気圏突入時の
ような短時間の高熱下では外殻をなす高融点金属が溶融
しないという条件下で断熱材として使用可能である。FIG. 1 is only one example of the present invention, and the shape can be arbitrarily configured depending on the site and method of use. For example,
In the case of a flat part of the furnace wall, a furnace wall with good heat insulation can be constructed by filling a cubic or rectangular parallelepiped hollow container with carbon micro hollow bodies and fixing it to the furnace wall with appropriate fasteners. In addition, in order to use it as a heat insulating material to protect the fuselage of an aircraft from high heat, carbon micro hollow bodies can be filled and fixed in a metal hollow molded body that matches the shape of the aircraft6.For example, when entering the atmosphere, It can be used as a heat insulating material under the condition that the high melting point metal forming the outer shell does not melt under such short-term high heat conditions.
本発明の炭素微小中空体を中空容器に充填する手段は従
来のカーボンフオームに比べ熱伝導率は約1/3になり
、断熱性が向上する。The means for filling a hollow container with the carbon microhollow bodies of the present invention has a thermal conductivity that is approximately 1/3 that of conventional carbon foam, and the heat insulation properties are improved.
なお、本発明に使用した炭素微小中空体は、本出願人が
特開昭61−14110号公報で提案した製造方法によ
って製造したものである。The carbon microhollow bodies used in the present invention were manufactured by the manufacturing method proposed by the applicant in Japanese Patent Application Laid-open No. 14110/1983.
〔発明の効果〕 本発明は次のような優れた効果を奏する。〔Effect of the invention〕 The present invention has the following excellent effects.
■炭素微小中空体をカーボンフオームにせず粒状のまま
用いているため、断熱性のよい高温断熱構造を極めて安
価で提供することができる。■Since the carbon micro hollow bodies are used in granular form without being converted into carbon foam, a high temperature insulation structure with good insulation properties can be provided at an extremely low cost.
■中空容器の形状や固定具の工夫により応用範囲の広い
多彩な断熱施工が可能となる。■A variety of insulation constructions with a wide range of applications are possible by changing the shape of the hollow container and the fixings.
■ダストの発生が殆どなく、かつ吸湿性の低い高温断熱
構造が得られ炭素繊維成型体の持つ欠点をカバーするこ
とができる。(2) A high-temperature insulation structure with almost no dust generation and low hygroscopicity can be obtained, making it possible to overcome the drawbacks of carbon fiber molded bodies.
第1図は本発明をHIP装置に適用したものであり、第
1図(a)は縦断面図、第1図(b)t4横断面図、第
2図は従来のHIP装置を示し第2図(a)は縦断面図
、第2図(b)は横断面図である。
l・・・中空容器 1a・・・上部蓋2・・・ク
ッション材 3・・・炭素微小中空体4・・・発熱体
5・・・加圧部6・・・成型用サンプル 7
・・・断8壁8・・・熱遮蔽コイルFigure 1 shows the application of the present invention to a HIP device, where Figure 1 (a) is a longitudinal sectional view, Figure 1 (b) is a t4 cross sectional view, and Figure 2 shows a conventional HIP device. FIG. 2(a) is a longitudinal cross-sectional view, and FIG. 2(b) is a cross-sectional view. l...Hollow container 1a...Top lid 2...Cushion material 3...Carbon micro hollow body 4...Heating element 5...Pressure part 6...Molding sample 7
... Section 8 Wall 8 ... Heat shielding coil
Claims (1)
ガスまたは真空雰囲気下で使用する高温断熱構造におい
て、 外殻を形成する中空容器と、該中空容器に充填された炭
素微小中空体とからなることを特徴とする高温断熱構造
。 2 中空容器の材質が融点1000℃以上の金属である
特許請求の範囲第1項に記載の高温断熱構造。[Claims] 1. A high-temperature insulation structure used in an inert gas or vacuum atmosphere at a high temperature of 1000°C or higher and 3000°C or lower, comprising: a hollow container forming an outer shell; and carbon filled in the hollow container. A high-temperature insulation structure characterized by consisting of micro hollow bodies. 2. The high-temperature insulation structure according to claim 1, wherein the material of the hollow container is a metal with a melting point of 1000° C. or higher.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8126387A JPS63247588A (en) | 1987-04-03 | 1987-04-03 | High-temperature heat-insulating structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8126387A JPS63247588A (en) | 1987-04-03 | 1987-04-03 | High-temperature heat-insulating structure |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63247588A true JPS63247588A (en) | 1988-10-14 |
Family
ID=13741474
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8126387A Pending JPS63247588A (en) | 1987-04-03 | 1987-04-03 | High-temperature heat-insulating structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63247588A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0889012A1 (en) * | 1997-07-01 | 1999-01-07 | Daimler-Benz Aktiengesellschaft | Process for filling cavities in workpieces or semi-finished products and components for mounting in a vehicle |
-
1987
- 1987-04-03 JP JP8126387A patent/JPS63247588A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0889012A1 (en) * | 1997-07-01 | 1999-01-07 | Daimler-Benz Aktiengesellschaft | Process for filling cavities in workpieces or semi-finished products and components for mounting in a vehicle |
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