US2361383A - High temperature conduit - Google Patents
High temperature conduit Download PDFInfo
- Publication number
- US2361383A US2361383A US437897A US43789742A US2361383A US 2361383 A US2361383 A US 2361383A US 437897 A US437897 A US 437897A US 43789742 A US43789742 A US 43789742A US 2361383 A US2361383 A US 2361383A
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- Prior art keywords
- liner
- high temperature
- temperature
- pressure
- conduit
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/14—Arrangements for the insulation of pipes or pipe systems
- F16L59/147—Arrangements for the insulation of pipes or pipe systems the insulation being located inwardly of the outer surface of the pipe
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/14—Arrangements for the insulation of pipes or pipe systems
- F16L59/16—Arrangements specially adapted to local requirements at flanges, junctions, valves or the like
- F16L59/18—Arrangements specially adapted to local requirements at flanges, junctions, valves or the like adapted for joints
Definitions
- This invention relates to conduits and containers of composite form for utilization of gases or vapors under conditions of extreme high temperature.
- my invention consists of a. three-element structure comprised of (1) a thinwalled and unpressured inner conduit formed of a material resistant to corrosion or oxidation by extremely hot gases; (2) a concentric outer shell of ordinary structural material such as low-carbon steel, for example, which will satisfactorily bear the pressure stresses as long as the temperature of the shell is not excessive, and (3) a layer of suitable insulating material interposed between the two concentric shells to insure maintenance of the outer shell temperature below the allowable limit.
- the expensive corrosion-resistant alloy materials may be used sparingly with maximum benet.
- the -stressbearing portion of the structure is protected from both high temperatures and corrosive action, so that the less costly common 'steels can be used without undue sacrice with respect to strength, bulk or cost of the equipment to be fabricated.
- a further advantage is realized in that less heat is lost from the system per unit of time, with the dual eiect of conserving the heat energy and minimizing the discomfort to be inicted upon the operating personnel, as well.
- the required cooling is carried out in a/hea/.t exchanger in which the hot gaseous material is passed around a number of pipes containing water (steam) as a coolant.
- 'I'he gases to be cooled contain various hydrocarbon vapors, and often an appreciable quantity of sulphur, in which latter case the corrosive action is especially
- the indicated cost of the cooling unit and adjacent piping for a commercial applica-tion would be but a fraction of that which would be incurred in constructing the unit in conventional fashion, or if available commercial heat exchangers were to be modied. for the purpose.
- a principal object of my invention is to pro-l vide a relatively inexpensive structure for the handling of extremely hot gases and vapors.
- a more specific object is to make practical the use of ordinarycarbon steels for the stress-bearl lng members in an application where the conobtaining in the case of conventional structures l in .the same high-temperature service.
- Another object is to provide, in a unit of the nature to be described, full protection against corrosive attack with a minimum expenditure of special corrosion-resistant alloy.
- Figure 1 shows an apparatus for which my invention is particularly well adapted.
- Figure 2 is a detail of my improvement, and
- Figure 3 illustrates a convenient manner in Whic the insulating material may be applied.
- the numeral I refers generally to a cooling chamber whose outer walls are to vvbe formed in -accordance with my invention, which is described in greater detail hereinaiter.
- the conduit 2 is to contain the hot gases entering at 3 from a catalytic cracking chamber, not shown.
- the gases are passed in heat exchange relationship with tubes l, after which they exit through the outlet to recycle through the system, or other disposition.
- the tubes 4 contain a circulating cooling medium,
- I prefer to use water of condensate quality for the coolant in which case cooling of the gases is accompanied by the generation of steam inthe coolant tubes, producing usable by-product power for use in a turbine, for example.
- 'I'he gases enter the cooler at a temperature of approximately 1500 F., and exit at a temperature of approximately 850 F. A pressure of approximately 100 pounds per square inch is maintained in the conduit 2.
- the numeral I indicates a tubular liner which may be made of 17% chromium steel, for example, or oi' any other material which is suitably resistant to corrosion at the temperatures to be encountered in a specific application.
- a layer of insulation material I is placed on the outward side of the corrosion resistant liner.
- the outer shell 1 is formed of ordinary carbon steel pipe or tubing of standard pipe size and weight.
- Conventional weld-type flanges 8 are provided at the termini of successive joints of pipe, and are fitted with frangible gaskets I'I of copper or soft iron which provide a pressure-tight joint.
- Spacer pins 9 of alloy steel are welded to the wall of the outer shell 1 and others are welded to the inner liner 5.
- 'I'he arrangement of these pins may be any of an almost infinite number of possible combinations. I preier to attach at least three of these pins to the outer shell at each end, spaced equally about the circumference and also at least three attached radially to the liner 5 at its longitudinal midpoint, It is understood that in no case will the liner be tied to the outer case by welding both ends of any pin. All pins attached to the liner are free from the outer case, and vice versa.
- seal ring I of similar material which'serves to provide an expansion joint for the liner.
- the seal ring has the form of a band, or short cylindrical section II which fits closely within the ends of the liners 5.
- a radial surface I2 which interposes between the abutting ends of the insulation layers.
- the cross-sectional shape of the seal ring is thus in T-iorm.
- Pressure-equalizationvents may be provided in the seal rings, as at I3, or in the alloy liners as at I4.
- the purpose of such vents is to assure equalization of pressure across the walls of the liner so that the liner will not be required to bear the stress which would otherwise be generated by pressure of the pipe content.
- These vents are not always absolutely necessary, due to the fact that the liner joints will leak suilciently to equalize the pressure.
- FIG. 3 Illustrated in Figure 3 is a convenient method of fabricating my improved pipe structure. Having at hand the carbon steel outer tubes with flanges attached, a wooden block I5 is turned on a lathe to the general shape shown in Figure 3 and is bolted to the flange at one end of the pipe as illustrated. The inner liner having been inserted from one end and brought to position, (determined by surface I6) the tube assembly is upended on the wooden form and insulation poured into vthe annular space between the tubes. After lling, another wood former may be placed on the remaining open end to form the insulation to like contour.
- insulating material While many different types-of insulating material are suitable for the purpose, I prefer to use one of the castable or moldable types which are placed in a wet condition and which upon drying or curing, attain a consistency at least rigid enough to retain a molded shape upon removal of the woodvforms.
- the insulating material when dried out, should have suiiicient porosity to allow leakage of pressure from the vents of the inner liner toward the outer shell 1. insulators can be used, however, by providing suitable ventpassages through the insulating layer. Such materials are commercially available, and no claim to the material per se is made herein. l
- the specific castable or moldable insulating materials that I have foundmost suitablein practicing this invention are "Panelag, Insulag and "Sil-O-Cell C-3. These are trade names. Quigley Co., 56 West 45th Street, New York city, states Panelag” is good for temperatures up to 1700 F. while “Insulag is good up to 2000 F., and that either one when mixedwith water forms a plastic cement material which hardens into an insulating block.
- Sil- O-Cell C-3 is a coarse granular form of calcined diatomaoeous silica, which mixed with water forms a plastic cement which hardens into a block good for temperatures up to 2000 F.
- the exact composition of Panelag, Insulag and "Sil-O-Cell C-3 are secrets, but they are sold by said companies in the open market with directions as to the amount of water to be added and the mixing procedure.
- the unit illustrated by Figure' 1 is connected to the discharge line from a thermal or a catalytic cracking furnace, for example. 'Ihe high temperature products enter the cooling unit at 3, and after passing in heat exchange relationship with the tubes exit from the cooler at a reduced temperature.
- the tubes 4 contain a Non-permeable particular benefit, other obvious applications can.
- coolant such as water (in which case steam is generated) or other suitable coolant.
- an inert material for the coolant such as CO2. for example, to reduce the oxidizing tendency on the interior of the cooler tubes 4.
- the outer case 1 is protected against this extreme temperature by the insulation 6, thus maintaining the temperature in this locality low enough that the carbon steel will not be materially weakened;
- the thin alloy steel liner 5 is 0f a composition capable of withstanding the extreme internal temperature, and serves to protect the insulating material 6 from mechanical damage by the gas stream, which at times may have a high velocity.
- the inner and outer shells 5 and l are free to expand or contract independently of each other, and stresses in these members are thereby minimized. Continuity of the liner is maintained by the overlapping seal rings I 0. Pressure on the interior oi the liner E is equalized due to venting through the openings i3..so that no gas-stream pressure stresses are imposed on the liner.
- a conduit for high temperature fluids comprising an imperforate stress-bearing shell, a perforate temperature resisting liner contained therein, a moldable heat insulating material be.
- a conduit for high temperature uids comprising an imperforate stress-bearing shell, a perforate temperature resisting liner contained therein, a moldable heat insulating material between said outer member and the liner, spacer pins of the same material as the liner member welded to the outer member at the ends of they pipe, and further spacer pins intermediate the ends of the pipe welded to the inner liner. all of said spacer pins being imbedded in the moldable insulating layer.
Description
Oct'. 31, 1944. L COFFMAN 2,361,383
HIGH TEMPERATURE CONDUIT Filed April e, 1942 FVG.
vINVENTOR l, L. cof-FMAN k* BY Z z/ rf: d'1 1 l. ORNEY Patented oct. 3i, 1944 HIGH TEMPERATURE CONDUIT Irving Lee Coffman, Bartlesville, Okla., assignor,
to Phillips Petroleum Company, acorporation .of Delaware Application April 6, 1942, Serial No. 437,897
2 Claims.-
This invention relates to conduits and containers of composite form for utilization of gases or vapors under conditions of extreme high temperature.
More specically, my invention consists of a. three-element structure comprised of (1) a thinwalled and unpressured inner conduit formed of a material resistant to corrosion or oxidation by extremely hot gases; (2) a concentric outer shell of ordinary structural material such as low-carbon steel, for example, which will satisfactorily bear the pressure stresses as long as the temperature of the shell is not excessive, and (3) a layer of suitable insulating material interposed between the two concentric shells to insure maintenance of the outer shell temperature below the allowable limit.
In the past, many alloy steels have been developed for use in high temperature applications,
-such as in steam superheaters, petroleum cracking stills etc. 'Ihese alloys were developed to answer two specific problems. One problem is in the overcoming of rapid corrosion eect of high temperature steam and/or organic gases upon equipment constructed of the early common types of steel. The second advantage gained by the introduction of these special alloy steels was an improvement in tensile strength at elevated temperatures.
While the advantage of the special alloy steels is great in regard' to corrosion resistance, the improvement in strength characteristic as compared to ordinary steels is not proportionate to the increased cost of the alloy materials. The result is that equipment for high temperature applications (where high pressures are usually corollary) is designed to employ either the alloy materials at great money expense, or the ordinary steels at a lesser expense but a still considerable one and with the disadvantage of great bulk in the structure.
In my improved construction, the expensive corrosion-resistant alloy materials may be used sparingly with maximum benet. The -stressbearing portion of the structure is protected from both high temperatures and corrosive action, so that the less costly common 'steels can be used without undue sacrice with respect to strength, bulk or cost of the equipment to be fabricated. A further advantage is realized in that less heat is lost from the system per unit of time, with the dual eiect of conserving the heat energy and minimizing the discomfort to be inicted upon the operating personnel, as well.
A particular application for which my improvesevere.
ment has great utility is in a process for treating hydrocarbons, wherein it is necessary to cool the eilluent from a reaction vessel from i500 F. down to about 850 F., at a sustained pressure of approximately pounds per square inch.4
The required cooling is carried out in a/hea/.t exchanger in which the hot gaseous material is passed around a number of pipes containing water (steam) as a coolant. 'I'he gases to be cooled contain various hydrocarbon vapors, and often an appreciable quantity of sulphur, in which latter case the corrosive action is especially On the basis of results obtained in an experimental cooler incorporating my improved construction, the indicated cost of the cooling unit and adjacent piping for a commercial applica-tion would be but a fraction of that which would be incurred in constructing the unit in conventional fashion, or if available commercial heat exchangers were to be modied. for the purpose.
A principal object of my invention is to pro-l vide a relatively inexpensive structure for the handling of extremely hot gases and vapors.
t A more specific object is to make practical the use of ordinarycarbon steels for the stress-bearl lng members in an application where the conobtaining in the case of conventional structures l in .the same high-temperature service.
It is an object to reduce the amount of heat lost to the atmosphere in a system of the sort herein described, with a consequent increase in the amount of useful by-product heat recovered in the cooling system.
Another object is to provide, in a unit of the nature to be described, full protection against corrosive attack with a minimum expenditure of special corrosion-resistant alloy.
The advantages and true nature of my inverition will be readily lcomprehended by consideration of the following description and claims.
In the drawing, Figure 1 shows an apparatus for which my invention is particularly well adapted. Figure 2 is a detail of my improvement, and Figure 3 illustrates a convenient manner in Whic the insulating material may be applied. l
Referring to Figure 1, the numeral I refers generally to a cooling chamber whose outer walls are to vvbe formed in -accordance with my invention, which is described in greater detail hereinaiter. The conduit 2 is to contain the hot gases entering at 3 from a catalytic cracking chamber, not shown. The gases are passed in heat exchange relationship with tubes l, after which they exit through the outlet to recycle through the system, or other disposition. The tubes 4 contain a circulating cooling medium, In the specific application at hand, I prefer to use water of condensate quality for the coolant, in which case cooling of the gases is accompanied by the generation of steam inthe coolant tubes, producing usable by-product power for use in a turbine, for example. 'I'he gases enter the cooler at a temperature of approximately 1500 F., and exit at a temperature of approximately 850 F. A pressure of approximately 100 pounds per square inch is maintained in the conduit 2.
In Figure 2, which shows the detail about one wall of a flanged joint in the conduit 2, the numeral I indicates a tubular liner which may be made of 17% chromium steel, for example, or oi' any other material which is suitably resistant to corrosion at the temperatures to be encountered in a specific application. A layer of insulation material I is placed on the outward side of the corrosion resistant liner. The outer shell 1 is formed of ordinary carbon steel pipe or tubing of standard pipe size and weight. Conventional weld-type flanges 8 are provided at the termini of successive joints of pipe, and are fitted with frangible gaskets I'I of copper or soft iron which provide a pressure-tight joint.
Spacer pins 9 of alloy steel (same material as liner 5) are welded to the wall of the outer shell 1 and others are welded to the inner liner 5. 'I'he arrangement of these pins may be any of an almost infinite number of possible combinations. I preier to attach at least three of these pins to the outer shell at each end, spaced equally about the circumference and also at least three attached radially to the liner 5 at its longitudinal midpoint, It is understood that in no case will the liner be tied to the outer case by welding both ends of any pin. All pins attached to the liner are free from the outer case, and vice versa. The
result of this method of assembly is that the liner is spaced symmetrically within theouter shell and is well supported at the center and ends, yet the inner and outer tubes can expand and contract longitudinally in an independent manner.
At each joint in the inner lining 5 is provided a seal ring I of similar material which'serves to provide an expansion joint for the liner. The seal ring has the form of a band, or short cylindrical section II which fits closely within the ends of the liners 5. Appended to the band I I is a radial surface I2 which interposes between the abutting ends of the insulation layers. The cross-sectional shape of the seal ring is thus in T-iorm.
Pressure-equalizationvents may be provided in the seal rings, as at I3, or in the alloy liners as at I4. The purpose of such vents is to assure equalization of pressure across the walls of the liner so that the liner will not be required to bear the stress which would otherwise be generated by pressure of the pipe content. These vents are not always absolutely necessary, due to the fact that the liner joints will leak suilciently to equalize the pressure. However, if the pressure within the pipes were to rise suddenly, leakage at the liner joints could not be depended upon to relieve the resultant pressure stress adequately and rupture of the liner would be likely to occur. Therefore, it is preferable to provide the vents to take care of sudden rises in pressure which might occur.
Illustrated in Figure 3 is a convenient method of fabricating my improved pipe structure. Having at hand the carbon steel outer tubes with flanges attached, a wooden block I5 is turned on a lathe to the general shape shown in Figure 3 and is bolted to the flange at one end of the pipe as illustrated. The inner liner having been inserted from one end and brought to position, (determined by surface I6) the tube assembly is upended on the wooden form and insulation poured into vthe annular space between the tubes. After lling, another wood former may be placed on the remaining open end to form the insulation to like contour.
While many different types-of insulating material are suitable for the purpose, I prefer to use one of the castable or moldable types which are placed in a wet condition and which upon drying or curing, attain a consistency at least rigid enough to retain a molded shape upon removal of the woodvforms. The insulating material, when dried out, should have suiiicient porosity to allow leakage of pressure from the vents of the inner liner toward the outer shell 1. insulators can be used, however, by providing suitable ventpassages through the insulating layer. Such materials are commercially available, and no claim to the material per se is made herein. l
The specific castable or moldable insulating materials that I have foundmost suitablein practicing this invention are "Panelag, Insulag and "Sil-O-Cell C-3. These are trade names. Quigley Co., 56 West 45th Street, New York city, states Panelag" is good for temperatures up to 1700 F. while "Insulag is good up to 2000 F., and that either one when mixedwith water forms a plastic cement material which hardens into an insulating block. J ohns-Manville Co., 292 Madison Ave., New York city states Sil- O-Cell C-3 is a coarse granular form of calcined diatomaoeous silica, which mixed with water forms a plastic cement which hardens into a block good for temperatures up to 2000 F. The exact composition of Panelag, Insulag and "Sil-O-Cell C-3 are secrets, but they are sold by said companies in the open market with directions as to the amount of water to be added and the mixing procedure.
The `Ftenery Catalog 1942, Gulf Publishing Company, Houston, Texas, lists suitable insulating cements on pages 96, 116, 239, 414, 449, 479, 508, 535 and elsewhere. A mixture of roughly 50% asbestos fibre and 50% Portland cement mixed with just enough water to make it plastic is also suitable, but is not preferred.
Having formed the insulation inthe above manner, the wood forms I5 are removed and the seal rings III are inserted. The completed composite pipes are now ready for installation and the iianges 8 are bolted in the conventional manner i for this purpose.
In operation, the unit illustrated by Figure' 1 is connected to the discharge line from a thermal or a catalytic cracking furnace, for example. 'Ihe high temperature products enter the cooling unit at 3, and after passing in heat exchange relationship with the tubes exit from the cooler at a reduced temperature. The tubes 4 contain a Non-permeable particular benefit, other obvious applications can.
circulating coolant such as water (in which case steam is generated) or other suitable coolant. In some cases it is desirable to use an inert material for the coolant, such as CO2. for example, to reduce the oxidizing tendency on the interior of the cooler tubes 4.
The temperature within the inner conduit 5.
may be as high as 1500-2000 F', at the inlet. The outer case 1 is protected against this extreme temperature by the insulation 6, thus maintaining the temperature in this locality low enough that the carbon steel will not be materially weakened; The thin alloy steel liner 5 is 0f a composition capable of withstanding the extreme internal temperature, and serves to protect the insulating material 6 from mechanical damage by the gas stream, which at times may have a high velocity.
The inner and outer shells 5 and l are free to expand or contract independently of each other, and stresses in these members are thereby minimized. Continuity of the liner is maintained by the overlapping seal rings I 0. Pressure on the interior oi the liner E is equalized due to venting through the openings i3..so that no gas-stream pressure stresses are imposed on the liner.
It is understood that while the drawings and descriptive matter of this specification illustrate a specific example wherein my invention is of be made. The scope of my invention is, therefore, subject only to the limitations of the appended claims.
I claim:
1. A conduit for high temperature fluids comprising an imperforate stress-bearing shell, a perforate temperature resisting liner contained therein, a moldable heat insulating material be.
tween said outer member and the liner, spacer means welded to the outer member at the ends of the pipe, and further spacer means intermediate the ends of the pipe Welded to the inner liner, all of said spacer means being imbedded in the moldable insulating layer.
2. A conduit for high temperature uids comprising an imperforate stress-bearing shell, a perforate temperature resisting liner contained therein, a moldable heat insulating material between said outer member and the liner, spacer pins of the same material as the liner member welded to the outer member at the ends of they pipe, and further spacer pins intermediate the ends of the pipe welded to the inner liner. all of said spacer pins being imbedded in the moldable insulating layer.
IRVING LEE COFFMAN,
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US437897A US2361383A (en) | 1942-04-06 | 1942-04-06 | High temperature conduit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US437897A US2361383A (en) | 1942-04-06 | 1942-04-06 | High temperature conduit |
Publications (1)
Publication Number | Publication Date |
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US2361383A true US2361383A (en) | 1944-10-31 |
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US437897A Expired - Lifetime US2361383A (en) | 1942-04-06 | 1942-04-06 | High temperature conduit |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423213A (en) * | 1944-11-13 | 1947-07-01 | Phillips Petroleum Co | High-temperature conduit |
US2650111A (en) * | 1948-10-29 | 1953-08-25 | Edward W Kaiser | Expansion joint enclosure |
US3155117A (en) * | 1959-11-27 | 1964-11-03 | Escher Wyss Ag | Double-walled hollow body for the reception of a hot gaseous medium under pressure |
US3693665A (en) * | 1970-01-28 | 1972-09-26 | Shell Oil Co | Pipeline for the transport of cold liquids |
US4063344A (en) * | 1976-12-27 | 1977-12-20 | Texaco Inc. | Methods for forming a high temperature and shock resistant insulated pipe |
WO2011011208A1 (en) | 2009-07-24 | 2011-01-27 | Mogas Industries, Inc. | Tubular member with thermal sleeve liner |
US20150325988A1 (en) * | 2014-05-12 | 2015-11-12 | SYNCRUDE CANADA LTD. in trust for the owners of the Syncrude Project, as such owners exist now and | Sectioned continuity wire system in conduits |
US11940084B2 (en) | 2019-03-25 | 2024-03-26 | Velan Inc. | Thermal insulating sleeve liner for fluid flow device and fluid flow device incorporating such liner |
-
1942
- 1942-04-06 US US437897A patent/US2361383A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423213A (en) * | 1944-11-13 | 1947-07-01 | Phillips Petroleum Co | High-temperature conduit |
US2650111A (en) * | 1948-10-29 | 1953-08-25 | Edward W Kaiser | Expansion joint enclosure |
US3155117A (en) * | 1959-11-27 | 1964-11-03 | Escher Wyss Ag | Double-walled hollow body for the reception of a hot gaseous medium under pressure |
US3693665A (en) * | 1970-01-28 | 1972-09-26 | Shell Oil Co | Pipeline for the transport of cold liquids |
US4063344A (en) * | 1976-12-27 | 1977-12-20 | Texaco Inc. | Methods for forming a high temperature and shock resistant insulated pipe |
WO2011011208A1 (en) | 2009-07-24 | 2011-01-27 | Mogas Industries, Inc. | Tubular member with thermal sleeve liner |
EP2457005A1 (en) * | 2009-07-24 | 2012-05-30 | Mogas Industries Incorporated | Tubular member with thermal sleeve liner |
EP2457005A4 (en) * | 2009-07-24 | 2013-01-16 | Mogas Ind Inc | Tubular member with thermal sleeve liner |
US20150325988A1 (en) * | 2014-05-12 | 2015-11-12 | SYNCRUDE CANADA LTD. in trust for the owners of the Syncrude Project, as such owners exist now and | Sectioned continuity wire system in conduits |
US11940084B2 (en) | 2019-03-25 | 2024-03-26 | Velan Inc. | Thermal insulating sleeve liner for fluid flow device and fluid flow device incorporating such liner |
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