GB2165262A - Means for maintaining the vacuum in an evacuated chamber - Google Patents

Means for maintaining the vacuum in an evacuated chamber Download PDF

Info

Publication number
GB2165262A
GB2165262A GB08524342A GB8524342A GB2165262A GB 2165262 A GB2165262 A GB 2165262A GB 08524342 A GB08524342 A GB 08524342A GB 8524342 A GB8524342 A GB 8524342A GB 2165262 A GB2165262 A GB 2165262A
Authority
GB
United Kingdom
Prior art keywords
vacuum
alloy
maintaining
jacket
gases
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.)
Granted
Application number
GB08524342A
Other versions
GB2165262B (en
GB8524342D0 (en
Inventor
Otto Bernauer
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Publication of GB8524342D0 publication Critical patent/GB8524342D0/en
Publication of GB2165262A publication Critical patent/GB2165262A/en
Application granted granted Critical
Publication of GB2165262B publication Critical patent/GB2165262B/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/02Alloys based on vanadium, niobium, or tantalum
    • AHUMAN NECESSITIES
    • A47FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47JKITCHEN EQUIPMENT; COFFEE MILLS; SPICE MILLS; APPARATUS FOR MAKING BEVERAGES
    • A47J41/00Thermally-insulated vessels, e.g. flasks, jugs, jars
    • A47J41/02Vacuum-jacket vessels, e.g. vacuum bottles
    • A47J41/022Constructional details of the elements forming vacuum space
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J3/00Processes of utilising sub-atmospheric or super-atmospheric pressure to effect chemical or physical change of matter; Apparatus therefor
    • B01J3/006Processes utilising sub-atmospheric pressure; Apparatus therefor

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Thermal Sciences (AREA)
  • Food Science & Technology (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Thermally Insulated Containers For Foods (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Solid-Sorbent Or Filter-Aiding Compositions (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Abstract

The use of an alloy of the formula Ti(V1@a@bFeaAlb)xCryMnz where x=greater than 1 and up to 2, y=0 to 0.2 x+y=at most 2 a=0 to 0.4 b=0 to 0.2 a+b=at most 0.5 (1-a-b).x=at least 1 Z=0 to (2-x-y) as an agent to maintain the vacuum in the vacuum jacket of thermally insulated vessels is described. A vacuum of better than 10 <4> mbar can be maintained by means of the alloy for long periods.

Description

SPECIFICATION Means for maintaining the vacuum in an evacuated chamber The invention relates to a means for maintaining the vacuum in an evacuated chamber.
Double-walled vessels, in which the interspace between the walls is evacuated, are of the type of vessel having the best thermal insulation capacities. Whereas relatively small vessels are usually made from glass, larger vessels can be made only with walls of steel.
It has been found, however, that the vacuum in the vacuum jacket of insulating vessels of steel deteriorates in the long term, especially also if radiation-reflecting shields are additionally fitted in the vacuum space. This deterioration in the vacuum is to be ascribed to the fact that, on the one hand, gases absorbed in the wall and in the radiation shields are released and, on the other hand, that gases, for example hydrogen, can diffuse through the steel walls. However, the thermal insulation by means of vacuum drops sharply at the moment when the pressure in the vacuum jacket rises above 10 4 mbar. It has therefore also already been disclosed to introduce means for maintaining the vacuum, for example activated carbon, into the vacuum jacket.
It is the object of the invention to provide a further, inexpensive, highly effective means which is capable, when introduced into the vacuum jacket, of absorbing gases appearing there and maintaining a vacuum of better than 10 4 mbar.
According to the invention there is provided an alloy of the formula Ti(v, a ,,,Fe,,AI,,),Cr,Mn, where x = greater than 1 and up to 2, y = O to 0.2 x+y = at most 2 a = O to 0.4 b = O to 0.2 a+b = at most 0.5 (1-a-b).x = at least 1 z = O to (2-x-y) for maintaining the vacuum in the vacuum jacket of thermally insulated vessels.
The alloy may be used here in the form of powder, preferably in a quantity of 2 to 4 g per I. of the volume of the vacuum space.
After the alloy has been introduced into the vacuum space and vacuum has been applied, the alloy is either activated at 300"C or, before it is introduced into the vacuum space, the alloy is charged with hydrogen at temperatures from 20 to 100 C and then activated automatically in the course of evacuation of the vacuum jacket (pumping out of the gases) at room temperature or at temperatures up to 100"C.
The preparation of the alloy is carried out by fusing the alloy constituents or appropriately selected master alloys under a blanketing gas, a melt of the higher-melting constituents being produced first, into which melt the lower-melting constituents are then introduced, in order to minimise the evaporation rates. To reduce the oxygen content of the alloy, the melt is then deoxidised by the addition of known deoxidising agents (lanthanum, mischmetal and the like).
The solidified melt is then comminuted under a blanketing gas. The material obtained can be comminuted further by repeated absorption and desorption of hydrogen, so that the particle size of the alloy can be reduced to less than 1 m by repeated charging and discharging of the alloy with hydrogen. Desorption is here carried out at temperatures of about 100 to 150 C. For use of the alloy as a means for maintaining the vacuum in the vacuum jacket, however, a particularly finely dispersed powder is not absolutely necessary since the deterioration of the vacuum in the vacuum jacket takes place only very slowly and a high rate of absorption of the gases by the alloy is therefore not necessary. (This applies above all to hydrogen).
The alloy reliably absorbs the gases usually appearing in the vacuum jacket, such as oxygen, hydrogen, water vapour, carbon monoxide and the like, so that a vacuum of better than 10 6 mbar, frequently even 10 7 to 10 8 mbar, can be maintained. Alloys of the compositions TiV1 5Fe04Mn0 , TiV,6FeO4 or TiV16FeO2 CrO1 MnO1 have here proved particularly suitable.
1. An alloy of the formula Tl(VI , "FedAIb) , CrMn, where x = greater than 1 and up to 2, y = O to 0.2 x+y = at most 2 a = O to 0.4 b = O to 0.2 a+b = at most 0.5 (1-a-b).x = at least 1 z = O to (2-x-y) for maintaining the vacuum in the vacuum jacket of thermally insulated vessels.
2. An alloy according to claim 1 in a quantity of 2 to 4 g per I. of vacuum space.
3. An alloy according to claim 1 or 2, characterised by the composition TiV1 sFeO4MnO,.
4. An alloy according to claim 1 or 2, characterised by the composition TiV1 6Fe04.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (7)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Means for maintaining the vacuum in an evacuated chamber The invention relates to a means for maintaining the vacuum in an evacuated chamber. Double-walled vessels, in which the interspace between the walls is evacuated, are of the type of vessel having the best thermal insulation capacities. Whereas relatively small vessels are usually made from glass, larger vessels can be made only with walls of steel. It has been found, however, that the vacuum in the vacuum jacket of insulating vessels of steel deteriorates in the long term, especially also if radiation-reflecting shields are additionally fitted in the vacuum space. This deterioration in the vacuum is to be ascribed to the fact that, on the one hand, gases absorbed in the wall and in the radiation shields are released and, on the other hand, that gases, for example hydrogen, can diffuse through the steel walls. However, the thermal insulation by means of vacuum drops sharply at the moment when the pressure in the vacuum jacket rises above 10 4 mbar. It has therefore also already been disclosed to introduce means for maintaining the vacuum, for example activated carbon, into the vacuum jacket. It is the object of the invention to provide a further, inexpensive, highly effective means which is capable, when introduced into the vacuum jacket, of absorbing gases appearing there and maintaining a vacuum of better than 10 4 mbar. According to the invention there is provided an alloy of the formula Ti(v, a ,,,Fe,,AI,,),Cr,Mn, where x = greater than 1 and up to 2, y = O to 0.2 x+y = at most 2 a = O to 0.4 b = O to 0.2 a+b = at most 0.5 (1-a-b).x = at least 1 z = O to (2-x-y) for maintaining the vacuum in the vacuum jacket of thermally insulated vessels. The alloy may be used here in the form of powder, preferably in a quantity of 2 to 4 g per I. of the volume of the vacuum space. After the alloy has been introduced into the vacuum space and vacuum has been applied, the alloy is either activated at 300"C or, before it is introduced into the vacuum space, the alloy is charged with hydrogen at temperatures from 20 to 100 C and then activated automatically in the course of evacuation of the vacuum jacket (pumping out of the gases) at room temperature or at temperatures up to 100"C. The preparation of the alloy is carried out by fusing the alloy constituents or appropriately selected master alloys under a blanketing gas, a melt of the higher-melting constituents being produced first, into which melt the lower-melting constituents are then introduced, in order to minimise the evaporation rates. To reduce the oxygen content of the alloy, the melt is then deoxidised by the addition of known deoxidising agents (lanthanum, mischmetal and the like). The solidified melt is then comminuted under a blanketing gas. The material obtained can be comminuted further by repeated absorption and desorption of hydrogen, so that the particle size of the alloy can be reduced to less than 1 m by repeated charging and discharging of the alloy with hydrogen. Desorption is here carried out at temperatures of about 100 to 150 C. For use of the alloy as a means for maintaining the vacuum in the vacuum jacket, however, a particularly finely dispersed powder is not absolutely necessary since the deterioration of the vacuum in the vacuum jacket takes place only very slowly and a high rate of absorption of the gases by the alloy is therefore not necessary. (This applies above all to hydrogen). The alloy reliably absorbs the gases usually appearing in the vacuum jacket, such as oxygen, hydrogen, water vapour, carbon monoxide and the like, so that a vacuum of better than 10 6 mbar, frequently even 10 7 to 10 8 mbar, can be maintained. Alloys of the compositions TiV1 5Fe04Mn0 , TiV,6FeO4 or TiV16FeO2 CrO1 MnO1 have here proved particularly suitable. CLAIMS
1. An alloy of the formula Tl(VI , "FedAIb) , CrMn, where x = greater than 1 and up to 2, y = O to 0.2 x+y = at most 2 a = O to 0.4 b = O to 0.2 a+b = at most 0.5 (1-a-b).x = at least 1 z = O to (2-x-y) for maintaining the vacuum in the vacuum jacket of thermally insulated vessels.
2. An alloy according to claim 1 in a quantity of 2 to 4 g per I. of vacuum space.
3. An alloy according to claim 1 or 2, characterised by the composition TiV1 sFeO4MnO,.
4. An alloy according to claim 1 or 2, characterised by the composition TiV1 6Fe04.
5. An alloy according to claim 1 or 2, characterised by the composition TiV16Fe0,2Cr0,1Mn0,1
6. Means for maintaining a vacuum in an evacuated chamber comprising placing an alloy as claimed in claim 1 in said chamber.
7. Means for maintaining a vacuum in an evacuated chamber by the use of an alloy substantially as described herein.
GB8524342A 1984-10-06 1985-10-02 Means for maintaining the vacuum in an evacuated chamber Expired GB2165262B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3436754A DE3436754C1 (en) 1984-10-06 1984-10-06 Means for maintaining the vacuum in the vacuum jacket of thermal insulating containers

Publications (3)

Publication Number Publication Date
GB8524342D0 GB8524342D0 (en) 1985-11-06
GB2165262A true GB2165262A (en) 1986-04-09
GB2165262B GB2165262B (en) 1989-05-24

Family

ID=6247301

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8524342A Expired GB2165262B (en) 1984-10-06 1985-10-02 Means for maintaining the vacuum in an evacuated chamber

Country Status (6)

Country Link
JP (1) JPS6190621A (en)
CA (1) CA1253361A (en)
DE (1) DE3436754C1 (en)
FR (1) FR2571385B1 (en)
GB (1) GB2165262B (en)
IT (1) IT1184652B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3775639B2 (en) * 2000-02-22 2006-05-17 株式会社日本製鋼所 Method for producing hydrogen storage alloy

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117002A (en) * 1982-03-20 1983-10-05 Daimler Benz Ag Hydrogen storage material

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4358316A (en) * 1980-12-29 1982-11-09 University Patents, Inc. Alloys for hydrogen storage
US4360445A (en) * 1981-06-16 1982-11-23 The United States Of America As Represented By The United States Department Of Energy Oxygen stabilized zirconium-vanadium-iron alloy
DE3425055C1 (en) * 1984-07-07 1985-07-25 Daimler-Benz Ag, 7000 Stuttgart Getter substance

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117002A (en) * 1982-03-20 1983-10-05 Daimler Benz Ag Hydrogen storage material

Also Published As

Publication number Publication date
DE3436754C1 (en) 1985-08-14
GB2165262B (en) 1989-05-24
IT1184652B (en) 1987-10-28
GB8524342D0 (en) 1985-11-06
CA1253361A (en) 1989-05-02
FR2571385B1 (en) 1992-12-31
IT8548627A1 (en) 1987-04-03
FR2571385A1 (en) 1986-04-11
IT8548627A0 (en) 1985-10-03
JPS6190621A (en) 1986-05-08
JPH0159006B2 (en) 1989-12-14

Similar Documents

Publication Publication Date Title
KR100188443B1 (en) Vaccum heat insulation panel
US4306887A (en) Getter device and process for using such
RU2146722C1 (en) Nonvaporizing getter alloy and device containing such alloy
US4079523A (en) Iron-titanium-mischmetal alloys for hydrogen storage
DE1134398B (en) Heat-insulated containers, especially for storing low-boiling liquefied gases
PT1817439E (en) Non-evaporable getter alloys for hydrogen sorption
PL315498A1 (en) Combination of gas absorbing materials
US4161401A (en) Nickel-calcium alloy for hydrogen storage
US4717551A (en) Titanium-based alloy used as a gettering material
JP2631055B2 (en) Sorption method of residual gas by non-evaporable barium getter alloy
JPS61104053A (en) Zirconium-type hydrogen occluding alloy
JP2627703B2 (en) Sorption method of residual gas, especially nitrogen gas by non-evaporable barium getter alloy
GB2165262A (en) Means for maintaining the vacuum in an evacuated chamber
JPS61143544A (en) Material for reversibly occluding and releasing hydrogen
JP3322486B2 (en) Hydrogen storage alloy with excellent poisoning resistance and regenerative recovery
JP2743123B2 (en) Materials for hydrogen storage
JPS62284033A (en) Reversible hydrogen occluding and releasing material
JPH0577732B2 (en)
US4656023A (en) Hyperstoichiometric zirconium-titanium-chromium iron alloys
JP3000680B2 (en) Materials for hydrogen storage
JPH0693366A (en) Hydrogen storage alloy
RU2082249C1 (en) Sorption method for residual gas, including gaseous nitrogen by means of nonevaporated gas-absorbing barium alloy
JPS5599597A (en) Material of anti-corrosive fin for cathode
JPS58167740A (en) Hydrogen occluding alloy of four elements basing on titanium
CA1095879A (en) Iron-titanium-mischmetal alloys for hydrogen storage

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Effective date: 20051001