Method for thermally insulating an evacuable container

Information

  • Patent Grant
  • 11920735
  • Patent Number
    11,920,735
  • Date Filed
    Wednesday, May 30, 2018
    6 years ago
  • Date Issued
    Tuesday, March 5, 2024
    3 months ago
Abstract
Method for thermal insulation of an evacuable container comprising an inner container, an outer container and a cavity disposed between the inner container and the outer container, wherein said method comprises a) using a vacuum pump to reduce a pressure in the cavity and after achieving a first value of the pressure interrupting the connection to the vacuum pump,b) subsequently making a connection from a reservoir container of the thermally insulating particulate material to a filling opening provided in the region of the cavity,c) setting the evacuable container into motion, wherein the thermally insulating particulate material flows into the cavity according to a) and the pressure in the cavity increases due to the air introduced with the thermally insulating particulate material,d) terminating the filling at a second value of the pressure by interrupting the connection from the cavity to the reservoir container,e) repeating step a), wherein the output of the vacuum pump with which the cavity is deaerated is controlled such that the profile over time of the mass flow exiting from the cavity of air introduced with the thermally insulating particulate material is at a maximum,f) subsequently repeating steps b)-e) up to the desired degree of filling andg) as the final step sealing the evacuated cavity.
Description
CROSS REFERENCE TO RELATED APPLICATIONS

The present application is US national stage of international application PCT/EP2018/064248, which had an international filing date of May 30, 2018, and which was published on Dec. 13, 2018. The application claims priority to German application DE 10 2017 209 782.5, filed on Jun. 9, 2017.


The invention relates to a method for thermal insulation of an evacuable container.


EP-A-645576 discloses a method for filling and compressing insulating powder into hollow walls of a boxlike body with subsequent evacuation of the gaseous medium so that the powder forms a vacuum insulation in the walls. The powder is pumped in at a first pressure and compressed at a second pressure.


DE-A-102010040346 discloses a method for manufacturing a thermally insulating shaped body which comprises the method steps of providing a mold, filling a pourable porous material, for example a granulate of an open-pored rigid plastics foam, an aerogel, a zeolite or a silica, into the mold, consolidating the pourable porous material in the mold and evacuating and sealing the mold.


DE-A-102013016705 discloses a method for insulating a hot water storage means. The hot water storage means comprises an inner container and an outer container, wherein between the inner container and the outer container a cavity for receiving an insulating layer made of an otherwise unspecified pourable fine-grained granulate is provided. The method contains the method steps: Filling the granulate into the cavity, compressing the granulate in the cavity, evacuating and sealing the cavity. The method may be implemented such that initially the granulate is filled into the cavity and compressed and subsequently the cavity is evacuated and sealed or initially the cavity is evacuated, subsequently the granulate is filled and compressed and finally the cavity is sealed.


The prior art also recites methods wherein a thermally insulating material is introduced into a cavity. The material may initially be introduced into the cavity with subsequent evacuation or else the cavity is initially evacuated and the thermally insulating material is introduced into the evacuated cavity. Both methods show disadvantages in execution. Disadvantages are for example in terms of filling duration, settling behaviour or discharging of previously introduced thermally insulating material.


It is accordingly an object of the present invention to provide a method having a short filling duration wherein discharging of thermally insulating material is minimized.







The invention provides a method for thermal insulation of an evacuable container, preferably a hot water container, comprising an inner container, an outer container and a cavity disposed between the inner container and the outer container, wherein the cavity is provided to receive a thermally insulating particulate material and for receiving the thermally insulating particulate material the steps of evacuating the cavity, filling the thermally insulating particulate material into the cavity, compressing the thermally insulating particulate material in the cavity, evacuating the cavity and sealing the cavity are performed,

    • wherein said method comprises
    • a) using a vacuum pump to reduce a pressure in the cavity and after achieving a first value of the pressure interrupting the connection to the vacuum pump,
    • b) subsequently making a connection from a reservoir container of the thermally insulating particulate material to a filling opening provided in the region of the cavity,
    • c) setting the evacuable container into motion, wherein the thermally insulating particulate material flows into the cavity according to a) and the pressure in the cavity increases due to the air introduced with the thermally insulating particulate material,
    • d) terminating the filling at a second value of the pressure by interrupting the connection from the cavity to the reservoir container,
    • e) repeating step a), wherein the output of the vacuum pump with which the cavity is deaerated is controlled such that the profile over time of the mass flow exiting from the cavity of air introduced with the thermally insulating particulate material is at a maximum,
    • f) subsequently repeating steps b)-e) up to the desired degree of filling and
    • g) as the final step sealing the evacuated cavity.


It may be advantageous to likewise set the reservoir container into motion. This motion may be a vibration or rotation both for the evacuable container and for the reservoir container. Stirring, tilting, pressurizing with gas or fluidizing by other means could also be carried out in the reservoir container.



FIG. 1 is a schematic diagram of the method according to the invention when using a throttle valve in the evacuation procedure before sealing the cavity in section C of the figure. In the figure: [atm]=atmospheric pressure; {dot over (V)}VP [%]=aspirated volume flow; {dot over (m)}air, EV [%]=air mass flow; throttle [%]=throttle valve opening.


Section A shows the pressure (II) in the cavity during evacuation of the cavity not yet filled with the thermally insulating particulate material from atmospheric pressure (atm) to less than 100 mbar, in particular to less than 20 mbar, in particular to less than 5 mbar. A high mass flow of air (III) is initially present and said mass flow falls with falling pressure (II) in each case depending on the volume of the cavity and the aspirated volume flow {dot over (v)}VP (I) of the vacuum pump.


Section B shows the filling of the cavity with the thermally insulatin. particulate material.


To this end a connection between the reservoir container and the cavity is opened, thus effecting a pressure equalization. A slight negative pressure is generally established in the cavity. The negative pressure depends inter alia on the geometry of the containers, their arrangement with respect to one another and the thermally insulating particulate material. The magnitude of the negative pressure (dashed rectangle) is not determined and is not relevant for performing the method according to the invention.


The mass flow of the outflowing air is zero.


Section C shows the evacuation of the filled annular slot. The evacuation is divided into three sections for example.


Section 1: Evacuation procedure in progress, valve position of throttle increases to 25%. A small mass flow of air is observed.


Section 2: Evacuation procedure in progress, valve position of throttle increases to 50%. A markedly increasing mass flow of air is observed.


Section 3: Evacuation procedure in progress, valve position of throttle increases to 100%. It is observed that the mass flow of air increases further and reaches a maximum. Evacuation procedure remains in progress until target pressure, for example less than 100 mbar, in particular less than 20 mbar, in particular less than 5 mbar, is achieved. It is observed that the mass flow of air reduces.



FIG. 2 is a schematic diagram of the method according to the invention when using a controllable vacuum pump in the evacuation procedure before sealing the cavity in section C of the figure.


In the figure: [atm]=atmospheric pressure; {dot over (V)}VP [%]=aspirated volume flow; {dot over (m)}air, EV [%]=air mass flow.


The comments made in respect of FIG. 1 apply for sections A and B.


Section C shows the evacuation of the filled annular slot. As the pressure stage decreases, the aspirated volume flow {dot over (V)}VP of the vacuum pump is increased. Mass flow initially increases but then decreases since the proportion of air in the cavity decreases.


A controlled mass flow of air is important for the filling procedure. Said mass flow is thus limited for example to a predetermined low value at commencement of the evacuation, in particular via an output limiting means of the vacuum pump or a throttle valve so that no thermally insulating particulate material is entrained. In a second step when a particular value of the vacuum has already been achieved, the pump output is increased or the throttling is reduced further. This need not necessarily be associated with a mass flow increase of the air since as the vacuum decreases the pump output must increase in order that air may still be aspirated from the cavity against the vacuum.


According to an advantageous concept of the invention, the commencement of the evacuation is commenced with a starting volume flow of air. In the course of the evacuation, the volume flow of air, starting from the starting volume flow, is advantageously further increased, in particular the volume flow of air is increased by approximately 2 to 5 times the starting volume flow or else up to 10 or 20 times the starting volume flow. The mass flow of air advantageously reduces.


The thermally insulating particulate material employed in the method according to the invention is preferably a compressed silica-comprising powder having a tamped density of 50-150 g/l. The tamped density may be determined according to ISO 697/EN ISO 60; DIN 53468.


Such a material has a low thermal conductivity, good flow properties during filling, while discharge during evacuation of the cavity is minimal or entirely negligible. The compressed powder preferably has a thermal conductivity of less than 5 mW/m·K at a pressure of 100 hPa or less than 25 mW/m·K at a pressure of 1000 hPa. The compressed powder is distinct from a granulate in respect of its tamped density and its flow behaviour.


The silica is preferably a pyrogenic silica. Pyrogenically produced silicas are preferably employed. Pyrogenic silicas are generally in aggregated form or at least partly aggregated. “Aggregated” is to be understood as meaning that so-called primary particles formed initially during generation make strong interconnections in the further course of the reaction to form a three-dimensional network. The description “at least partly aggregated” is intended to elucidate that in addition to aggregates isolated individual particles may also be present, wherein at least 80% of the hydrophobized silicon dioxide particles should be present in the form of aggregates. Such a silica shows good values in respect of both thermal insulation and mechanical stability of the three-dimensional network. The ratio of aggregate to isolated individual particles may be determined for example by quantitative evaluation of TEM micrographs (TEM=transmission electron microscopy). The silicon dioxide particles are amorphous.


The term “pyrogenically” encompasses production of silica by means of flame hydrolysis and flame oxidation. Here, oxidizable and/or hydrolysable starting materials are oxidized or hydrolysed generally in a hydrogen/oxygen flame. Starting materials that may be used for pyrogenic methods include organic and inorganic substances. Silicon tetrachloride is particularly suitable. The thus obtained hydrophilic silica is very largely pore-free and has free hydroxyl groups on its surface. The BET surface area of pyrogenic silica is generally 30 to 500 m2/g. For the method according to the invention, in particular a BET surface area of at least 150 m2/g is preferred.


The silica used in the method according to the invention may comprise a hydrophilic silica, a hydrophobized silica or at least one hydrophilic and at least one hydrophobic silica.


It has proven particularly useful to employ a hydrophobized silica. These are obtained from the reaction of hydrophilic silicas with a hydrophobizing agent. The hydroxyl groups present at the surface of the hydrophilic silica are partly or completely converted. The degree of hydrophobization may be determined by the methanol wettability.


Thus, the silica should have a methanol wettability of at least 20 vol % of methanol, preferably 20-80 vol % of methanol. Hydrophobic silicas may be rendered water-wettable by addition of methanol. This is effected by methanol/water mixtures of different concentrations. This makes it possible to reveal the degree of hydrophobization of the silicas.


The hydrophobized silica may preferably be obtained by reaction of a hydrophilic silica with an organosilane from the group consisting of Rn—Si—X4-n, R3Si—Y—SiR3, RnSinOn, (CH3)3—Si—(O—Si(CH3)2)n—OH, HO—Si(CH3)2—(O—Si(CH3)2)n—OH, where n=1-8; R=—H, —CH3, —C2H5; X=—Cl, —Br; —OCH3, —OC2H5, —OC3H8, Y═NH, O.


The hydrophobic properties thereof ensure that only very small amounts, if any, of adhering water are introduced into the cavity to be filled. Adhering water can result in an undesired reduction of the vacuum and thus in an increased thermal conductivity. It may therefore be advantageous to introduce the thermally insulating particulate material in a very largely water-free state. While this may be achieved by drying methods or a subsequent reduction in pressure, this can slow the filling procedure.


The compressed powder is preferably employed as a mixture of a silica and an IR opacifier. A proportion of 60-90% by weight of a silica and 10-40% by weight of an IR opacifier is particularly preferred. Suitable IR opacifiers are titanium oxides, zirconium oxides, ilmenites, iron titanates, iron oxides, zirconium silicates, silicon carbide, manganese oxides, graphites and/or carbon blacks. The particle size of the opacifiers is generally between 0.1 and 25 μm. In the case of silicon carbide and titanium oxides, the average particle diameter d50 is preferably 1 to 10 μm, particularly preferably 2 to 8 μm.

Claims
  • 1. A method for thermally insulating an evacuable container comprising an inner container, an outer container and a cavity disposed between the inner container and the outer container, wherein the cavity is provided to receive a thermally insulating particulate material; and wherein the method for providing the cavity with the thermally insulating particulate material comprises the steps of: evacuating the cavity; filling the cavity with the thermally insulating particulate material; compressing the thermally insulating particulate material in the cavity; evacuating the cavity; and sealing the cavity; wherein: a) a vacuum pump is used to reduce pressure in the cavity and after achieving a first value of the pressure, connection between the cavity and the vacuum pump is interrupted;b) subsequently making a connection from a reservoir container of the thermally insulating particulate material to a filling opening provided in the region of the cavity;c) setting the evacuable container into motion, wherein the thermally insulating particulate material flows into the cavity according to a) and the pressure in the cavity increases due to air introduced with the thermally insulating particulate material;d) terminating the filling at a second value of the pressure by interrupting the connection from the cavity to the reservoir container;e) repeating step a), wherein the output of the vacuum pump with which the cavity is deaerated is controlled such that the profile over time of the mass flow exiting from the cavity of air introduced with the thermally insulating particulate material is at a maximum;f) subsequently repeating steps b)-e) until desired degree of filling is reached; andg) as the final step sealing the evacuated cavity.
  • 2. The method of claim 1 wherein the reservoir container is set into motion.
  • 3. The method of claim 1, wherein the motion is a vibration or rotation.
  • 4. The method of claim 1, wherein the thermally insulating particulate material is a compressed silica-comprising powder having a tamped density of 50-150 g/l.
  • 5. The method of claim 4, wherein the silica is a hydrophobized silica.
  • 6. The method of claim 4, wherein the silica is a hydrophilic silica.
  • 7. The method of claim 4, wherein the silica comprises at least one hydrophilic and at least one hydrophobic silica.
  • 8. The method of claim 4, wherein the compressed powder is a mixture of a silica and an IR opacifier.
  • 9. The method of claim 8, wherein the proportion of the silica is 60-90% by weight and the proportion of the IR opacifier is 10-40% by weight.
  • 10. The method of claim 3, wherein the thermally insulating particulate material is a compressed silica-comprising powder having a tamped density of 50-150 g/l.
  • 11. The method of claim 10, wherein the silica is a hydrophobized silica.
  • 12. The method of claim 10, wherein the silica is a hydrophilic silica.
  • 13. The method of claim 10, wherein the silica comprises at least one hydrophilic and at least one hydrophobic silica.
  • 14. The method of claim 10, wherein the compressed powder is a mixture of a silic and an IR opacifier.
  • 15. The method of claim 14, wherein the proportion of the silica is 60-90% by weight and the proportion of the IR opacifier is 10-40% by weight.
  • 16. The method of claim 14, wherein the silica is a hydrophobized silica.
  • 17. The method of claim 14, wherein the silica is a hydrophilic silica.
  • 18. The method of claim 17, wherein the silica comprises at least one hydrophilic and at least one hydrophobic silica.
  • 19. The method of claim 18, wherein the proportion of the silica is 60-90% by weight and the proportion of the IR opacifier is 10-40% by weight.
Priority Claims (1)
Number Date Country Kind
10 2017 209 782.5 Jun 2017 DE national
PCT Information
Filing Document Filing Date Country Kind
PCT/EP2018/064248 5/30/2018 WO
Publishing Document Publishing Date Country Kind
WO2018/224377 12/13/2018 WO A
US Referenced Citations (82)
Number Name Date Kind
2595262 Hood May 1952 A
3532473 Biegler Oct 1970 A
3574027 Bonnet Apr 1971 A
4048290 Lee Sep 1977 A
4175159 Raleigh Nov 1979 A
4212925 Kratel et al. Jul 1980 A
4247708 Tsutsumi et al. Jan 1981 A
4276274 Heckel Jun 1981 A
4286990 Kleinschmidt et al. Sep 1981 A
4297143 Kleinschmidt et al. Oct 1981 A
5086031 Deller et al. Feb 1992 A
5183710 Gerbino Feb 1993 A
5362541 Sextl et al. Nov 1994 A
5458916 Kratel et al. Oct 1995 A
5556689 Kratel et al. Sep 1996 A
5565142 Deshpande et al. Oct 1996 A
5589245 Roell Dec 1996 A
5685932 Stohr et al. Nov 1997 A
5776240 Deller et al. Jul 1998 A
5851715 Barthel et al. Dec 1998 A
6099749 Boes et al. Aug 2000 A
6174926 Menon et al. Jan 2001 B1
6268423 Mayer et al. Jul 2001 B1
6303256 Kerner et al. Oct 2001 B1
6472067 Hsu et al. Oct 2002 B1
7241336 Scharfe et al. Jul 2007 B2
7562534 Jibb et al. Jul 2009 B2
7674476 Schwertfeger et al. Mar 2010 B1
7780937 Meyer et al. Aug 2010 B2
7842269 Schachtely et al. Nov 2010 B2
7855248 Stenzel et al. Dec 2010 B2
8333946 Gottschalk et al. Dec 2012 B2
8389617 Meyer et al. Mar 2013 B2
8512595 Meyer et al. Aug 2013 B2
8603353 Menzel et al. Dec 2013 B2
8962519 Heindl et al. Feb 2015 B2
9055748 Feucht et al. Jun 2015 B2
9233986 Kratel et al. Jan 2016 B2
9540247 Stenzel et al. Jan 2017 B2
9593797 Kulprathipanja et al. Mar 2017 B2
9784402 Menzel Oct 2017 B2
9878911 Maisels et al. Jan 2018 B2
10179751 Geisler et al. Jan 2019 B2
10618815 Hindelang et al. Apr 2020 B2
10618849 Albinus et al. Apr 2020 B2
20030095905 Scharfe et al. May 2003 A1
20060027227 Everett et al. Feb 2006 A1
20070220904 Jibb et al. Sep 2007 A1
20080277617 Abdul-Kader et al. Nov 2008 A1
20090148342 Bromberg Jun 2009 A1
20100146992 Miller Jun 2010 A1
20100300132 Schultz Dec 2010 A1
20120064345 Gini Mar 2012 A1
20120286189 Barthel et al. Nov 2012 A1
20130071640 Szillat Mar 2013 A1
20140150242 Kratel et al. Jun 2014 A1
20140230698 Stepp et al. Aug 2014 A1
20150000259 Dietz Jan 2015 A1
20150183169 Ehsani Jul 2015 A1
20150183170 Ehsani Jul 2015 A1
20160082415 Drexel et al. Mar 2016 A1
20160084140 Dietz Mar 2016 A1
20160223124 Kulprathipanja et al. Aug 2016 A1
20160258153 Koebel et al. Sep 2016 A1
20160326003 Ishizuka et al. Nov 2016 A1
20170233297 Albinus et al. Aug 2017 A1
20170268221 Geisler et al. Sep 2017 A1
20180001576 Koebel et al. Jan 2018 A1
20180065892 Geisler et al. Mar 2018 A1
20180169931 Ehsani Jun 2018 A1
20190002356 Hebalkar et al. Jan 2019 A1
20190276358 Schultz et al. Sep 2019 A1
20190382952 Geisler et al. Dec 2019 A1
20200031720 Geisler et al. Jan 2020 A1
20200062661 Geisler et al. Feb 2020 A1
20210039954 Numrich et al. Feb 2021 A1
20210269359 Geisler et al. Sep 2021 A1
20210292233 Numrich et al. Sep 2021 A1
20210292238 Albinus et al. Sep 2021 A1
20220371261 Ehsani Nov 2022 A1
20230002627 Lazar et al. Jan 2023 A1
20230062574 Menzel et al. Mar 2023 A1
Foreign Referenced Citations (57)
Number Date Country
2 201 186 Sep 1997 CA
106830878 Jun 2017 CN
107814552 Mar 2018 CN
952 891 Nov 1956 DE
25 33 925 Feb 1977 DE
30 37 409 May 1982 DE
199 48 394 Feb 2001 DE
20 2007 013 074 Mar 2008 DE
10 2007 020 716 Nov 2008 DE
10 2007 031 635 Jan 2009 DE
10 2007 042 000 Mar 2009 DE
10 2007 051 830 May 2009 DE
10 2008 005 548 Jul 2009 DE
10 2008 036 430 Feb 2010 DE
10 2010 040 346 Mar 2012 DE
10 2013 016 705 Apr 2015 DE
10 2014 203 091 Aug 2015 DE
0 032 176 Jul 1981 EP
0 340 707 Nov 1989 EP
0 645 576 Mar 1995 EP
0 647 591 Apr 1995 EP
0 937 755 Aug 1999 EP
1 700 824 Sep 2006 EP
1 988 228 Nov 2008 EP
1988228 Nov 2008 EP
2 028 329 Feb 2009 EP
2 204 513 Jul 2010 EP
EP 2621873 Aug 2013 EP
2 910 724 Aug 2015 EP
3 403 818 Nov 2018 EP
2873677 Feb 2006 FR
919 018 Feb 1963 GB
20170112396 Oct 2017 KR
WO 9905447 Feb 1999 WO
WO 0112731 Feb 2001 WO
WO 03024705 Mar 2003 WO
WO 03064025 Aug 2003 WO
WO 2005028195 Mar 2005 WO
WO 2006097668 Sep 2006 WO
WO 2010126792 Nov 2010 WO
WO 2011066209 Jun 2011 WO
WO 2011076518 Jun 2011 WO
WO 2011083174 Jul 2011 WO
WO 2012041823 Apr 2012 WO
WO 2012044052 Apr 2012 WO
WO 2012049018 Apr 2012 WO
WO 2013053951 Apr 2013 WO
WO 2014090790 Jun 2014 WO
WO 2014095277 Jun 2014 WO
WO 2015007450 Jan 2015 WO
WO2016031637 Mar 2016 WO
WO 2016045777 Mar 2016 WO
WO-2016045777 Mar 2016 WO
WO 2016171558 Oct 2016 WO
WO 2017097768 Jun 2017 WO
WO 2017102819 Jun 2017 WO
WO 2018146137 Aug 2018 WO
Non-Patent Literature Citations (18)
Entry
U.S. Appl. No. 17/792,400, filed Jul. 31, 2022, Lazar.
U.S. Appl. No. 17/792,471, filed Jul. 13, 2022, Menzel.
Mathias, et al., “Basic characteristics and applications of aerosil: 30. The chemistry and physics of the aerosil surface,” Journal of Colloid and Interface Science 125:61-68 (1988).
Pajonk, et al., “Physical properties of silica gels and aerogels prepared with new polymeric precursors,” J. Non-Cryst. Solids 186(2):1-8 (Jun. 1995).
Somana, Chotangada Gautham, “Evaluation of Aerogel Composite Insulations by Characterization and Experimental Methods,” Thesis; B.Eng., R.V. College of Engineering, Banglore, India, (2012).
U.S. Appl. No. 16/978,164, filed Sep. 3, 2020, US-2021/0039954 A1, Feb. 11, 2021, Numrich.
U.S. Appl. No. 17/260,345, filed Jan. 14, 2021, Numrich.
U.S. Appl. No. 17/260,227, filed Jan. 14, 2021, Geisler.
U.S. Appl. No. 17/260,371, filed Jan. 14, 2021, Albinus.
English language translation of the International Search Report for PCT/EP2018/064248, (international counterpart of U.S. Appl. No. 16/620,481), filed May 30, 2018.
English language translation of the Written Opinion of the International Searching Authority for PCT/EP2018/064248, (international counterpart of U.S. Appl. No. 16/620,481 application), filed May 30, 2018.
English language translation of the International Preliminary Report on Patentability for for PCT/EP2018/064248, (international counterpart of U.S. Appl. No. 16/620,481 application), filed May 30, 2018.
Schreiner, et al., “Intercomparison of thermal conductivity measurements on an expanded glass granulate in a wide temperature range,” International Journal of thermal Sciences 95:99-105 (2015).
Ulmann's Encyclopedia of Industrial Chemistry, “Silica” chapter, published online on Apr. 15, 2008, DOI: 10.1002/14356007.a23_583.pub3.
U.S. Appl. No. 16/339,081, filed Apr. 3, 2019, US-2019/0276358 A1, Sep. 12, 2019, Schultz.
U.S. Appl. No. 16/484,368, filed Aug. 7, 2019, US-2019/0382952 A1, Dec. 9, 2019, Geisler.
U.S. Appl. No. 16/478,169, filed Jul. 16, 2019, Geisler.
U.S. Appl. No. 16/605,342, filed Oct. 15, 2019, Geisler.
Related Publications (1)
Number Date Country
20200124231 A1 Apr 2020 US