US20060026743A1 - Gas distribution garment - Google Patents

Gas distribution garment Download PDF

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Publication number
US20060026743A1
US20060026743A1 US10/913,975 US91397504A US2006026743A1 US 20060026743 A1 US20060026743 A1 US 20060026743A1 US 91397504 A US91397504 A US 91397504A US 2006026743 A1 US2006026743 A1 US 2006026743A1
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United States
Prior art keywords
garment
substrate
gas
cavity
raised protrusions
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.)
Abandoned
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US10/913,975
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English (en)
Inventor
Brian Farnworth
Paul Dacey
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.)
WL Gore and Associates Inc
Original Assignee
Gore Enterprise Holdings Inc
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 Gore Enterprise Holdings Inc filed Critical Gore Enterprise Holdings Inc
Priority to US10/913,975 priority Critical patent/US20060026743A1/en
Assigned to GORE ENTERPRISE HOLDINGS, INC. reassignment GORE ENTERPRISE HOLDINGS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DACEY, PAUL, FARNWORTH, BRIAN
Priority to ES05857541T priority patent/ES2353218T3/es
Priority to CA2575757A priority patent/CA2575757C/en
Priority to DE602005024142T priority patent/DE602005024142D1/de
Priority to EP05857541A priority patent/EP1773143B1/en
Priority to PCT/US2005/025851 priority patent/WO2006085998A2/en
Priority to PL05857541T priority patent/PL1773143T3/pl
Priority to JP2007524832A priority patent/JP5198860B2/ja
Priority to AU2005327125A priority patent/AU2005327125B2/en
Priority to DK05857541.6T priority patent/DK1773143T3/da
Priority to AT05857541T priority patent/ATE484202T1/de
Priority to CN2005800313289A priority patent/CN101022741B/zh
Priority to US11/347,533 priority patent/US7716940B2/en
Publication of US20060026743A1 publication Critical patent/US20060026743A1/en
Priority to IL181064A priority patent/IL181064A0/en
Priority to HK07104605.2A priority patent/HK1097705A1/xx
Assigned to W. L. GORE & ASSOCIATES, INC. reassignment W. L. GORE & ASSOCIATES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GORE ENTERPRISE HOLDINGS, INC.
Abandoned legal-status Critical Current

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Classifications

    • A—HUMAN NECESSITIES
    • A41—WEARING APPAREL
    • A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
    • A41D13/00—Professional, industrial or sporting protective garments, e.g. surgeons' gowns or garments protecting against blows or punches
    • A41D13/002—Professional, industrial or sporting protective garments, e.g. surgeons' gowns or garments protecting against blows or punches with controlled internal environment
    • A41D13/005—Professional, industrial or sporting protective garments, e.g. surgeons' gowns or garments protecting against blows or punches with controlled internal environment with controlled temperature
    • A41D13/0053—Cooled garments
    • A—HUMAN NECESSITIES
    • A41—WEARING APPAREL
    • A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
    • A41D27/00—Details of garments or of their making
    • A41D27/28—Means for ventilation
    • A—HUMAN NECESSITIES
    • A41—WEARING APPAREL
    • A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
    • A41D31/00—Materials specially adapted for outerwear
    • A41D31/04—Materials specially adapted for outerwear characterised by special function or use
    • A41D31/14—Air permeable, i.e. capable of being penetrated by gases
    • A41D31/145—Air permeable, i.e. capable of being penetrated by gases using layered materials
    • A—HUMAN NECESSITIES
    • A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F7/00—Heating or cooling appliances for medical or therapeutic treatment of the human body
    • A61F2007/0059—Heating or cooling appliances for medical or therapeutic treatment of the human body with an open fluid circuit
    • A61F2007/0063—Heating or cooling appliances for medical or therapeutic treatment of the human body with an open fluid circuit for cooling

Definitions

  • the present invention relates to a personal gas distribution garment, preferably a ventilated cooling garment.
  • a ventilated cooling garment for use by a wearer who is clad in a sealed overall suit and breathing system which is designed to protect the wearer from harmful chemical, biological or other environmental hazards. It is also a function of the ventilated cooling garment of the present invention that it may be adapted to use filtered ambient air as the ventilating cooling medium. Further desirable attributes of the garment are high cooling power, low weight, low bulk, good flexibility, and high water vapour permeability, all of which contribute to the comfort of the wearer.
  • U.S. Pat. No. 5,564,124 to Elsherif et al. discloses a personal ventilation apparatus which comprises a garment incorporating areas of air permeable material, such as open cell foam, to direct air to selected areas of the body.
  • the system also comprises a battery powered blower unit which, optionally, includes thermoelectric heating or cooling devices or filters. Given the small areas over which the cooling air is vented relative to the total area of the torso, the cooling power of the garment disclosed in this reference is likely to be severely limited and not meet the cooling criteria previously defined.
  • U.S. Pat. No. 5,970,519 to Weber discloses a cooling garment for medical personnel which comprises a simple two ply construction of an air impermeable layer and an air permeable layer, each having minimal thickness, defining a cavity into which air is blown.
  • the cavity has no spacers, or intermediate material or structures except in the shoulder regions to prevent the collapse of the garment in that area when the garment is worn under a heavy apron such as a radiological shield.
  • One distinct shortcoming of such a system is the absence of any intermediate layer to control airflow within the cavity resulting in uneven air distribution.
  • a further shortcoming is the lack of a means for controlling air distribution between the inner air permeable layer and the body of the wearer. The absence of such mechanisms may cause excessive cooling of some areas of the wearer's body, especially next to the air inlet port, while not supplying sufficient cooling in other areas. It is an objective of the present invention to overcome the shortcomings of the systems described above.
  • a gas distribution garment system which can be used with sealed garments such as are used in hazardous or toxic environments, as well as in other applications where the subject is exposed to high heat stress situations such as fire-fighters, clean room operatives or hospital theatre operatives.
  • a gas distribution cooling garment system most conveniently comprises a vest which delivers cooling air only to the torso, but may also be a jacket with sleeves, a coverall with sleeves and legs, or any other form which delivers cooling air to specific areas of the body. For optimum comfort and cooling efficiency it is desirable that the garment conforms closely to the body shape of the wearer.
  • the cooling gas can be ambient air and that the air can be filtered to remove undesirable components from the cooling air.
  • the cooling gas may also be passed through a heat exchanger to lower the temperature of the gas or through a de-humidifier to further increase its cooling capability.
  • the most efficient cooling using air at an ambient temperature of about 35° C. is achieved by having an air flow of about 4 to 8 liters/second (l/s) over the subject and that the flow should be confined to layer no more than about 4 mm from the body of the subject.
  • Another object of the invention is to provide a high degree of cooling to the wearer, in addition to natural cooling experienced by the wearer, for an extended period of time.
  • more than 50 watts of additional cooling is provided over the torso for a period of at least about three hours; more preferably greater than about 80 watts of additional cooling, and further preferred greater than about 100 watts of additional cooling is provided over the torso of a wearer for a period of at least about three hours.
  • Yet a further object of the invention is that by the use of a gas distribution manifold and a plurality of discrete elements within the cavity defined by the substrates comprising the invention, substantially uniform cooling is achieved over the torso of the wearer.
  • One embodiment comprising the gas distribution garment of the present invention comprises a first and a second substrate sealed to define at least one cavity.
  • the first substrate is substantially gas-impermeable but water-vapour-permeable.
  • the second substrate is gas-permeable and preferably water-vapour-permeable.
  • the surface of one or both substrates which is orientated towards the inside of the cavity are provided with a plurality of raised protrusions in the form of discrete elements, and the cavity is adapted to contain a gas distribution manifold which is in fluid connection with a gas supply system.
  • the surface of the second substrate external to the cavity is also provided with a plurality of raised protrusions in the form of discrete elements.
  • the garment is in the form of a vest, and in use the second substrate will form the inside of the vest such that gas exiting the cavity through the gas-permeable second substrate will flow over the torso of the wearer.
  • the plurality of discrete elements on the surface of the second substrate external to the cavity provides a space between the substrate and either the body of the wearer or any other garment worn thereon.
  • the height of the discrete elements are chosen such that the space between the wearer's body, or any other clothing worn next to the wearer's body, and the gas permeable second substrate is sufficiently wide to allow uniform flow of cooling gas but not so wide that it reduces the cooling effect of the gas.
  • the in-plane spacing between the discrete elements is optimised to distribute the flow of gas exiting the cavity and give substantially uniform cooling of the torso.
  • the plurality of discrete elements on one or both surfaces of the substrates within the cavity provides a space between the surfaces thereby allowing optimal distribution of the cooling gas within the cavity, and therefore across the wearer's body.
  • a gas distribution garment system comprises protrusions external to the cavity that are disposed on an additional substrate that is interposed between the body of the wearer and the external surface of the second substrate forming the cavity.
  • the interposing substrate is preferably water-vapour-permeable and may be gas-permeable.
  • the interposing layer may be attached to the substrates forming the cavity or detached from the cavity substrates.
  • the plurality of discrete elements contributes to increased conformability of the garment of the present invention by allowing flexing between protrusions compared with prior art garments which utilise mesh or mesh-like spacers.
  • the flexibility of substrates suitable for use in the present invention, having a pattern or plurality of discrete elements thereon, is not substantially less than the flexibility of substrates without any discrete elements.
  • the three dimensional structures of the mesh or mesh-like spacers of the prior art lack flex points and they are generally bulky and stiff; therefore the use of these structures results in garments having poor flexibility and conformability.
  • the plurality of discrete elements also result in a garment construction having lower resistance to gas flow compared with garments of the prior art that utilise mesh or mesh like materials as spacers.
  • Mesh spacers are constructed with material that can interfere with the air flow, whereas materials of the present invention have no intervening material between the discrete elements to interfere with air flow.
  • the low resistance to gas flow afforded by the discrete elements facilitates the use of low power fans to supply cooling gas to the invention and obviates the need for the garment to be “tethered” to a power supply or a high pressure supply of cooling gas.
  • a preferred embodiment comprises a “portable” or “non-tethered” gas distribution garment system which, as used herein, refers to a system which is not tethered to a (stationary) power supply or a high pressure gas supply.
  • the cooling gas may be ambient air blown into the cavity by battery powered fans which may be optionally fitted with filter elements or other gas treatment systems to remove noxious or other undesirable contaminating components.
  • FIG. 1 represents an embodiment of the invention in the form of a vest and comprising a fan as a means to drive ambient air through a manifold into the cavity of the garment.
  • FIG. 2 is plan view of the body side of the vest illustrating the relative disposition of the discrete elements on the substrate and perforations in the said substrate.
  • FIG. 3 is an enlarged view of area “X” in FIG. 2 in which the discrete elements comprise round protrusions.
  • FIG. 4 is a representation of the cross-section of an embodiment of the invention wherein the discrete elements within the cavity are disposed on the gas-impermeable substrate.
  • FIG. 5 is a representation of a cross-section of an embodiment of the invention in the direction Y-Y′ of FIG. 2 wherein the discrete elements are disposed either side of the gas-permeable substrate.
  • FIG. 6 is a representation of a gas distribution manifold for use in an embodiment of the invention.
  • FIG. 7 is a representation of an alternative construction of a gas distribution manifold for use in an embodiment of the invention.
  • FIG. 8 shows graphical plots of heart rate (beats/minute) versus time (hours) for a human subject in evaluation trials of an embodiment of the invention.
  • FIG. 9 shows graphical plots of body core temperature for a human subject in evaluation trials of an embodiment of the invention.
  • the gas distribution cooling garment 1 comprises a substantially gas impermeable substrate 2 attached around it's periphery to a gas permeable substrate 3 to define a cavity, part of which is representationally shown by the cutaway section A.
  • Substrate 3 has on its surface, which is external to the cavity and which is proximate to the body of the wearer, a plurality raised protrusions 4 in the form of discrete elements.
  • Substrate 3 is rendered gas-permeable by perforating the substrate between said raised protrusions to give a plurality of holes 5 through which gas can vent from the cavity and pass over the body of the wearer.
  • the cooling gas is ambient air which is drawn by the fan 6 through optional filter 7 and fed through duct 8 to the air distribution manifold 9 and thence substantially uniformly throughout the volume of the cavity to exit via the perforations 5 .
  • the cooling garment is held in close contact to the body of the wearer by a fastening section 10 which may be fastened using “hook and loop” systems or other suitable methods known in the art.
  • FIG. 2 is a plan view of one embodiment of the present invention depicting the surface of the gas permeable substrate 3 that is worn proximate to the body of the wearer.
  • the distribution of the discrete elements 4 and the perforations 5 are more clearly represented and are shown in detail in FIG. 3 which is a pictorial enlargement of area “X” in FIG. 2 .
  • FIG. 3 shows the relative distribution (not to scale) of the discrete elements 4 and the perforations 5 on the surface of the substrate 3 .
  • the discrete elements are shown as having circular cross-section in plan view which is not to be seen as limiting the invention.
  • the raised protrusions may comprise other shapes such as cuboidal, conical, pyramidal, polyhedral, hemispherical or truncated hemispherical.
  • discrete elements it is meant a plurality of individual elements, that are substantially or essentially discontinuous or not connected.
  • the discrete elements 4 are preferably soft and resilient but with limited compressibility for optimum comfort and maintenance of air flow.
  • the discrete elements may comprise any material capable of maintaining space between substrate layers, or between a substrate and the body of a wearer, but preferably comprise a thermoplastic or thermosetting polymer selected from, for example, but not limited to silicone, polyester, polyurethane, polyalkene, polyamide, fluoropolymers or other similar materials known to one skilled in the art.
  • Raised protrusions 4 may be applied to substrate 2 by any convenient means such as extrusion or screen printing or other methods known, for example, to one skilled in the art of surface coatings.
  • the raised protrusions preferably cover 50% or less of the area of the surface of substrate 3 which is proximate to the body of the wearer, a preferred coverage is less than 30% of the surface area and a more preferred coverage is less than 20%. It has been discovered by the inventor that, surprisingly, optimal cooling is achieved in systems wherein the height of the raised protrusions, preferably in the form of discrete elements, 4 is in the range of about 1 mm to 20 mm, preferably in the range about 2 mm to 10 mm and more preferably in the range about 2 mm to 4 mm.
  • the raised protrusions 4 define a plurality of channels having a depth equivalent to the height of the protrusions, between the external surface of substrate 3 and the wearer.
  • the cooling gas which exits through perforations 5 flows through the aforesaid channels and is distributed substantially uniformly over the body of the wearer.
  • the perforations 5 shown as circular in cross section may also be of other cross-sections and are preferably uniformly distributed over the surface of substrate 3 to ensure uniform gas-flow over the body of the wearer.
  • the cross-sectional area of a single perforation is preferably equivalent to that of a circular perforation having a diameter of between about 1 mm and 2 mm.
  • the perforations should be sufficient in number for substrate 3 to have an air permeability preferably of between about 10 and 100 l m ⁇ 2 s ⁇ 1 at a pressure drop of about 100 Pa and more preferably of between about 60 and 70 l m ⁇ 2 s ⁇ 1 at a pressure drop of about 100 Pa.
  • FIG. 4 shows enlarged detail of a cross-sectional view in the direction of Y-Y′ of FIG. 2 of an embodiment of the invention.
  • Substrates 2 and 3 define cavity 11 into which the cooling gas is passed from the gas distribution manifold (not shown).
  • the raised protrusions 4 which comprise discrete elements having a hemispherical profile are provided on the external surface of substrate 3 , i.e. the surface which is external to cavity 11 . When the garment is worn the protrusions 4 are in contact with the body of the wearer or in contact with an article of clothing, such as underwear or t-shirt, worn by the wearer.
  • this embodiment comprises a plurality of raised protrusion integral with the surface of substrate 2 , disposed internal to cavity 11 .
  • These are in the form of hemispherical discrete elements 12 which are uniformly distributed over the surface of substrate 2 within cavity 11 .
  • Raised protrusions preferably in the form of discrete elements 12 cover preferably less than 50% of the area and, more preferably, less than 30% of the surface of substrate 2 which is internal to the cavity.
  • a function of the discrete elements 12 disposed within the cavity is to act as spacer members to prevent the collapse of cavity 11 , for example, when heavy articles of clothing or a self contained breathing apparatus is worn over the cooling garment of the invention.
  • a further function of the discrete elements 12 is to aid in the uniform distribution of the cooling gas throughout the cavity 11 .
  • the height of the discrete elements 12 within the cavity is preferably in the range of about 1 mm to 20 mm. To minimise the thickness of the vest, and maximise its conformability and flexibility, and to ensure uniform distribution of the cooling gas through the cavity 11 , a preferred height of the discrete elements may range from about 2 mm to 10 mm.
  • the discrete elements 12 located within the cavity may comprise any suitable material but preferred materials are soft, resilient polymers having limited compressibility.
  • the polymers may be thermosetting or thermoplastic and may be selected from a range of polymers such as silicones, polyurethanes, polyesters, polyamides, polyalkenes fluoropolymers or other polymers deemed suitable by one skilled in the art, and may be applied to the supporting substrate by extrusion, screen printing or any suitable method known to one skilled in the art.
  • FIG. 5 is a cross-section of a garment having an alternative arrangement of raised protrusions in the form of discrete elements 12 within the cavity 11 .
  • the discrete elements 12 are located on the internal surface of substrate 3 and are positioned so as to be off-set from the protrusions 4 which are situated on the opposite surface of substrate 3 .
  • the discrete elements 12 on the internal surface of substrate 3 may be in alignment with the position of protrusions 4 on the external surface of the substrate, while maintaining airflow through the perforations 5 .
  • Substrate 2 is preferably substantially gas impermeable; by “substantially gas impermeable” is meant a substrate having less than about 10% of the gas permeability of the gas permeable second substrate. Preferred substrates have an air permeability of less that 10 lm ⁇ 2 s ⁇ 1 at pressure of 100 Pa. Preferably, substrate 2 is also water vapour permeable.
  • Substrate 3 may be a gas impermeable layer which has been perforated, or may be an intrinsically air permeable layer such as a laminate of microporous PTFE, a tightly woven textile, or a dense non-woven textile, with preferred constructions comprising an air permeability in the range of between about 10 and 100 l m ⁇ 2 s ⁇ 1 as previously taught herein. Where perforated, substrate 3 may be rendered somewhat water-vapour-permeable by the perforations 5 but it is preferred that the material of construction of substrate 3 is inherently water-vapour permeable.
  • Substrates 2 and 3 may comprise single monolithic constructions or may comprise a plurality of layers of different materials chosen to impart the desired features to the substrates, such as air permeability and water vapour permeability.
  • a preferred construction is a laminate of knitted or woven textile and an expanded polytetrafluoroethylene membrane coated with a water vapour permeable polymer. Such laminates are sold under the GORE-TEX® trade name by W.L.Gore and Associates Inc. Newark Del.
  • Preferred water vapour permeable materials for use in the substrates of the present invention including both the gas impermeable substrate and the gas permeable substrate may be comprised of a layer of a water-vapour permeable polymer such as polyurethane, polyester or microporous polyurethane or may comprise such polymers coated on or laminated to a textile construction.
  • Preferred materials are those having water vapor evaporative resistance (Ret) values less than about 20 m 2 Pa W ⁇ 1 as measured according to ISO 11092. More preferred materials are those having Ret values less than about 15 m 2 Pa W ⁇ 1 as measured according to ISO 11092.
  • Substrate 3 may comprise a monolithic single layer construction or a plurality of layers or a laminate comprising the same or different material that is chosen for substrate 2 .
  • a gas distribution garment system is formed wherein the plurality of raised protrusions external to the cavity are not disposed directly on the external cavity surface.
  • the raised protrusions external to the cavity surface are disposed on an additional substrate that is interposed between the body of the wearer and the external surface of the cavity.
  • the plurality of raised protrusions external to the cavity surface are disposed on an additional substrate located between the external cavity substrate and the skin of the wearer, and the raised protrusions are predominantly oriented towards the skin.
  • the additional substrate may be any suitable woven, non-woven or knitted fabric which is air permeable.
  • a knitted undergarment worn separately from the gas distribution garment may comprise a plurality of raised protrusions disposed on the inside of the undergarment directed toward the skin of the wearer.
  • the additional substrate comprising the raised protrusions is air permeable to enable the flow of air from the air permeable cavity substrate to flow through the additional substrate into close proximity with the wearer's skin.
  • the additional substrate comprising the plurality of raised external to the cavity is also located between the body of the wearer and the external surface of the cavity.
  • the plurality of raised protrusions are predominantly disposed on the additional substrate in an orientation that is away from the skin.
  • the additional substrate may be any suitable woven, non-woven or knitted fabric which is water vapor permeable such as, for example, a knitted undergarment such as a T-shirt.
  • the additional substrate is water vapor permeable to permit the evaporation of water from the skin into the stream of air which is formed external to the cavity between the air permeable cavity substrate and the additional substrate comprising the raised protrusions.
  • the additional substrate is optionally air permeable.
  • the additional substrate may be permanently affixed to one or both of the substrates that form the cavity, or the additional substrate may be detachably affixed to the substrates, or the additional substrate may be separate from the substrates that form the cavity.
  • the cavity formed by the substrates is adapted for connection with a gas supply so that gas flows into the cavity and exits the cavity through the gas permeable substrate.
  • a preferred means for such adaptation comprises a gas distribution manifold, substantially hollow in cross section, which is in fluid connection with the gas supply and comprises a series of perforations to allow gas to be distributed within at least part of the cavity.
  • FIG. 6 is a representation of the construction of a gas distribution manifold for use in an embodiment of the invention. The manifold of FIG.
  • Hollow member 13 which is substantially rectangular in cross-section, though it should be understood that other cross-sectional shapes are suitable for use in the present invention
  • Hollow member 13 is provided with a series of perforations 14 along the sides 15 and 16 and a gas feed duct 17 .
  • hollow member 13 is placed in the cavity of the garment with the duct 17 external to the cavity.
  • the cooling gas is fed through the lumen 18 of duct 17 and is distributed into the cavity of the garment through perforations 14 .
  • FIG. 7 is a representation of an alternative and preferred construction of a gas distribution manifold for use in the garment of the invention and corresponds to item 9 in FIG. 1 .
  • the construction comprises two hollow elongate members 19 and 20 which are substantially cylindrical in cross-section and have a series of perforations 21 along edges 22 , 23 , 24 , and 25 .
  • Hollow members 19 and 20 are connected to gas feed duct 26 by union piece 27 and the ends members 19 and 20 remote from union piece 27 are closed off by blanking pieces 28 and 29 .
  • members 19 and 20 are preferably placed in the cavity of the garment such that one member is in the area of the garment which covers the front of the torso of the wearer and the other member is in the back area of the garment.
  • Gas feed duct 26 is the representative embodiment is external to the cavity of the garment. Cooling gas fed into duct 26 is fed into both members 19 and 20 and is distributed into the cavity through perforations 21 .
  • the members 19 and 20 maybe constructed of any suitable material known to one skilled in the art but for optimal comfort for the wearer the material should be soft and flexible and preferably resilient with only a slight degree of compressibility. Suitable materials include elastomeric materials such as polyurethane, polyester, or synthetic rubbers such as EPDM or SBR. It is preferable for the material to have a hardness in the range of 55-65 Shore A.
  • the first and second substrates comprised a laminate of Basofil® spun bonded non-woven textile and expanded polytetrafluoroethylene having an air-impermeable water vapour permeable coating with a plurality of foamed silicone rubber protrusions uniformly distributed on the Basofil® surface.
  • the laminate is available from W.L.Gore and Associates GmbH, Putzbrunn, Germany under the trade name Airlock® Part No. AIRL 002000.
  • the silicone rubber protrusions are approximately 3 mm in height and cover an area of approximately 13% of the surface of the laminate.
  • Airlock® AIRL 002000 laminate Two pieces of Airlock® AIRL 002000 laminate were cut and sized according to FIG. 2 to give a body coverage of about 0.45 m 2 .
  • the laminate corresponding to the second substrate of the invention was perforated with a 1.34 mm diameter needle to give a grid pattern of holes on an approximately 6 mm by 10 mm spacing.
  • the air permeability of the laminate resulting from the perforations was about 60 l.m ⁇ 2 s ⁇ 1 at a pressure drop of about 100 Pa.
  • a gas distribution manifold of the general arrangement of FIG. 7 was formed from two lengths of 25 mm inside diameter cylindrical cable duct (Part No. 364-3458 from RS Components Ltd. Corby, Northants, England) corresponding to members 19 and 20 of FIG. 7 .
  • the length of each member was about 460 mm.
  • a uniform series of approximately 4 mm diameter holes were drilled in the surfaces of the duct corresponding to surfaces 22 , 23 , 24 and 25 of FIG. 7 to give 92 holes per member.
  • the ends of the duct within the cavity were sealed with blanking pieces and the other ends terminated in a union piece and gas entry duct corresponding to 27 and 26 respectively of FIG. 7 .
  • An electrically powered fan (Part No. U97EM-012KK-3 from Acal Radiatron, Egham, Surrey, England) was connected to the gas duct to complete the assembly.
  • the fan was powered from a bench mounted power supply unit adjusted to provide about 15 Volts dc to the fan. With this set up the airflow from the fan was calculated by measuring the pressure drop across the fan and comparing this with the pressure drop versus flow from the manufacturers data sheet for the fan. The flow was ascertained to be about 10 litres/sec.
  • Example 2 For the evaluation trials the subject was clad in the following manner. The subject was dressed in a cotton T-shirt and cotton briefs next to the skin. The cooling garment of Example 1 was provided over the T-shirt. Over the cooling garment, a British Army Mk IV protective suit was provided. Finally, on top of the protective suit, a British Army MK I Fragmentation vest was provided. The feet were covered in socks and heavy boots, and the hands were covered with lightweight cotton gloves under rubber gloves. A respiration mask was placed on the face of the subject.
  • the subject was tasked to walk on a tread-mill set at a linear speed of about 4.5 km/hr and the subject's body core temperature and heart rate monitored and recorded.
  • the duration of each trial consisted of periods of about 100 minutes of walking followed by rest periods of about 30 minutes.
  • the evaluation trials were carried out in an environmentally conditioned room at an ambient temperature of approximately 35° C. and a relative humidity of 50%.
  • FIGS. 8 and 9 The plot of heart rate versus time and the plot of body core temperature versus time for all three trials are shown respectively in FIGS. 8 and 9 .
  • FIG. 8 the plot of heart rate (beats/minute) versus time (hours), shows the highly significant cooling effect of the garment of the invention.
  • the regular peaks in the plot correspond to the exercise periods but, with the cooling in operation, the rate drops back to substantially the base level during the rest periods.
  • the heart rate plots for the “no cooling” and the “no vest” modes (Trials 2 and 3) result in regular rise in heart rate throughout the trials from approximately 80 beats per minute to highly undesirable rates of 160 beats per minute.
  • the body core temperature plots in FIG. 9 further confirms the effectiveness of the cooling garment of the invention.
  • the “cooling” plot shows the very small rise (less than about 0.5° C.) in the subject's body core temperature.
  • the “no cooling” and “no vest” plots corresponding to Trials 2 and 3 show highly undesirable increases of almost 2° C.
  • the body core temperature plots demonstrate the negligible thermo-physiological loading characteristics of the garment when worn without the cooling in operation.
  • the objectives of the invention are also clearly achieved by the garment of the above example.
  • the fan was powered by a bench mounted power supply unit it has been shown that a battery powered fan could be used and the same air flow rates achieved.
  • the fan of the example was replaced by a fan requiring only a 5 Volt dc supply (Part no.U97LM-005K1 from Acal Radiatron, Egham, Surrey, England) and the replacement fan powered by a nominally rated 6.4 Volt battery with an under-load voltage of 5.0 Volts (Part no. U3356H/2/7, from Ultralife Batteries Ltd. Abingdon, Oxfordshire, England.)
  • the fan gave an output of about 6 litres/sec for over 9 hours.
  • the garment of the example with the fan and battery attached weighed approximately 2.1 kg, which is considerably less than the 3 kg target for a lightweight system.
  • Example 1 To evaluate the cooling power of the cooling garment prepared substantially according to Example 1, it was subject to Thermally Instrumented Manikin testing by The Cord Group Ltd., Dartmouth, Nova Scotia, Canada.
  • the cooling garment was tested in combination with a standard British Army Mk IV protective suit as used in the foregoing Example 1 and under the various conditions as detailed in the following Table 1. Testing was carried out in a temperature and humidity controlled room with an ambient temperature set at 35° C. and relative humidity set 50%. Details of the test methodology are as follows.
  • cooling vest prototypes using UK standard suit ensemble were evaluated using a Thermal Instrumented Manikin Test System. During the testing, environment temperature, skin temperature and power consumption were recorded.
  • the Thermal Manikin Test System consists of a hollow aluminum manikin equipped with temperature sensors and electric heaters connected to a computer system.
  • the manikin was dressed in the human-use apparel to be tested and placed in an appropriate environment.
  • the computing equipment controlled the heaters to maintain the skin of the manikin at a set temperature and measured the electrical power required to do so. This power is equivalent to the heat that escaped through the clothing due to the temperature difference across it.
  • the power and the temperature difference were then used, along with the known surface area of the manikin to calculate the thermal resistance offered by the apparel.
  • the thermal performance of a garment was evaluated by unmanned tests on the whole garment under conditions identical or similar to actual operating conditions.
  • the system employed a life-sized watertight manikin capable of being heated to and maintained at a selected temperature.
  • the system comprised a Thermally Instrumented Manikin (TIM), a control module, a computer, environmental temperature sensors and cables connecting these components.
  • TIM Thermally Instrumented Manikin
  • the manikin was in a shape of human proportions to fit inside the test garment.
  • the combinations of the aluminum shell of the manikin and the output of heaters inside it provided for an approximately uniform temperature over the manikin surface. This temperature is sensed by sensors embedded in the manikin's shell and is then passed to the control module.
  • the control module housed the programmed data acquisition system, the heater relays and other circuit components.
  • the data acquisition system received data from the temperature sensors on the manikin and controlled the heater relays so that the manikin surface temperature remains constant. It also measured the environment temperature and the power applied to the manikin and was programmed with the surface area of the manikin. With this temperature, power and area data, it calculated the insulation value of the garment and passed this, along with other pertinent data to the computer.
  • the computer acted as a control and display terminal and post-processor.
  • the following clothing combination was used for testing.
  • the manikin was first covered in a shirt with long sleeves and trousers assembled into a coverall (skin) made of an interlock knit (high stretch), white 100% cotton textile. Tubes for the distribution of water were sewn into the garment.
  • coverall skin
  • Tubes for the distribution of water were sewn into the garment.
  • Table 1 cooling garments prepared according to Example 1 two styles were selected and optionally provided over the coverall.
  • One style of cooling garment comprised a single entry port manifold ( FIG. 6 ), and a second style of cooling garment was provided with a split manifold ( FIG. 7 ).
  • An outer layer comprising a UK Standard protective suit ensemble top and bottom, and a Mk I ballistic vest, was provided over the cooling garment, or depending on test conditions, directly over the coverall (skin).
  • Garment openings were secured as follows. Arm cuffs were tucked and secured with elastic straps; front zippers were secured to the top; and bottom of legs were secured with elastic straps. Tensioning straps on the ballistic vest were secured.
  • the manikin was lifted into a vertical position and suspended in the test chamber hanging from a head bolt with feet lightly touching the floor.
  • Environmental sensors were suspended around the manikin to detect the environment temperature.
  • the manikin temperature was set at about 35.0° C.
  • the ambient temperature of the chamber was set at about 35° C. and actual temperature was measured at about 34.16-34.31° C.
  • the ambient relative humidity of the chamber was set at about 50% about and measured at about 48.5-56.0%.
  • a warm-up period was provided to allow the manikin to reach the set temperature and go into test period. The long-term power was monitored for all calculated sections until steady state condition was reached, and the test was restarted.
  • Table 1 illustrates the significant overall cooling power of the cooling garment of the present invention when energised in cooling mode. Furthermore, a comparison of the results of Manikin Set Ups A and B demonstrates the minimal additional thermal stress added to the Thermally Instrumented Manikin by the cooling garment system of the invention when the garment is not energised for cooling.
  • Conformability of the garment of the present invention was tested and compared with a mesh spacer material representative of those used by garments of the prior art.
  • a sample comprising Airlock® Laminate AIRL 02000 was prepared according to the air permeable second substrate of Example 1 having a plurality of protrusions and perforations, and was tested and compared with spacer material from Mueller Textile Germany, Mueller Part no. 5911.
  • test method used was performed substantially as described in ASTM D 4032-94 (as re-approved in 2001)—Standard Test Method for Stiffness of Fabric by the Circular Bend Procedure, with the following modifications.
  • the size of the test sample was 4 inches by 4 inches (100 mm by 100 mm) an Instron Model 1011 tensile/compression tester operating with Instron Series 9 software replaced the force measurement gauge; and the plunger speed was set at 500 mm/min.
  • Airlock® laminate was tested in three different modes, as follows:
  • preferred embodiments of the present invention comprise a conformability peak force value of preferably less than or equal to 0.03 kg, more preferably less than or equal to 0.02 kg, and further preferred, less than or equal to 0.01 kg, for a substrate comprising a plurality of raised protrusions on a substrate surface, when tested according to the method provided herein.

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Environmental & Geological Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Materials For Medical Uses (AREA)
  • Woven Fabrics (AREA)
  • Details Of Garments (AREA)
US10/913,975 2004-08-06 2004-08-06 Gas distribution garment Abandoned US20060026743A1 (en)

Priority Applications (15)

Application Number Priority Date Filing Date Title
US10/913,975 US20060026743A1 (en) 2004-08-06 2004-08-06 Gas distribution garment
CN2005800313289A CN101022741B (zh) 2004-08-06 2005-07-20 气体分配服
AU2005327125A AU2005327125B2 (en) 2004-08-06 2005-07-20 Gas distribution garment
AT05857541T ATE484202T1 (de) 2004-08-06 2005-07-20 Gasverteilungkleidung
DE602005024142T DE602005024142D1 (de) 2004-08-06 2005-07-20 Gasverteilungkleidung
EP05857541A EP1773143B1 (en) 2004-08-06 2005-07-20 Gas distribution garment
PCT/US2005/025851 WO2006085998A2 (en) 2004-08-06 2005-07-20 Gas distribution garment
PL05857541T PL1773143T3 (pl) 2004-08-06 2005-07-20 Ubranie do rozprowadzania gazu
JP2007524832A JP5198860B2 (ja) 2004-08-06 2005-07-20 気体分配衣服
ES05857541T ES2353218T3 (es) 2004-08-06 2005-07-20 Traje de distribuciã“n de gas.
DK05857541.6T DK1773143T3 (da) 2004-08-06 2005-07-20 Klædningsstykke med gasfordeling
CA2575757A CA2575757C (en) 2004-08-06 2005-07-20 Gas distribution garment
US11/347,533 US7716940B2 (en) 2004-08-06 2006-02-03 Gas distribution garment having a spacer element
IL181064A IL181064A0 (en) 2004-08-06 2007-01-30 Gas distribution garment
HK07104605.2A HK1097705A1 (en) 2004-08-06 2007-04-30 Gas distribution garment

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US10/913,975 US20060026743A1 (en) 2004-08-06 2004-08-06 Gas distribution garment

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DE (1) DE602005024142D1 (ja)
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US20070093885A1 (en) * 2005-10-20 2007-04-26 Arizant Healthcare Inc. Multifunction warming device with an upper body convective apparatus
US20070095088A1 (en) * 2005-10-20 2007-05-03 Tiax Llc Body ventilation system and method
US20070118956A1 (en) * 2005-06-29 2007-05-31 Jack Sawicki Personal ventilating garment apparatus
US20090158496A1 (en) * 2006-04-24 2009-06-25 Stefan Roeckl Glove with inflatable air
US20100125928A1 (en) * 2004-07-01 2010-05-27 Michael Smith Pneumatic Cooling Apparel System
EP2474243A1 (en) * 2011-01-05 2012-07-11 Hill-Rom Services, Inc. Cooling system for an occupant of an occupant support and a cooling garment
US20120246788A1 (en) * 2011-03-28 2012-10-04 Harrell Jeremy L Multipurpose Cooling and Trauma Attenuating Devices and Associated Methods
NL2007462C2 (en) * 2011-09-23 2013-03-26 Bartholomeus Theodorus Maria Crasbeek Method and thermal device for controlling the temperature of a patient.
WO2014076479A1 (en) * 2012-11-14 2014-05-22 Benedetti International Limited Vasodilation assembly
US20140201891A1 (en) * 2013-01-23 2014-07-24 Nike, Inc. Ventilated And Protective Articles Of Apparel
USD731122S1 (en) 2013-01-14 2015-06-02 Jeremy L. Harrell Inflatable pad
US20150231420A1 (en) * 2014-02-20 2015-08-20 Draeger Safety Uk Limited Garment
US20150231419A1 (en) * 2014-02-20 2015-08-20 Draeger Safety Uk Limited Garment
USD738577S1 (en) 2013-01-14 2015-09-08 Jeremy L. Harrell Inflatable pad pattern
USD738576S1 (en) 2013-01-14 2015-09-08 Jeremy L. Harrell Inflatable pad pattern
USD743633S1 (en) 2013-01-14 2015-11-17 Jeremy L. Harrell Inflatable pad pattern
WO2016083638A1 (es) 2014-11-25 2016-06-02 Mat Global Solutions, S.L. Prenda transpirable
US20160270457A1 (en) * 2015-03-20 2016-09-22 Chien-Chou Chen Clothes structure with temperature falling device
US10765158B2 (en) 2016-03-25 2020-09-08 Nike, Inc. Foam nodes for creating stand off on apparel items
US20220273906A1 (en) * 2021-03-01 2022-09-01 The Johns Hopkins University Regenerable Carbon Dioxide Scrubber
US11432597B2 (en) 2019-07-03 2022-09-06 Kwaku TEMENG Pump-conditioned garment and apparatus therefor
US20220386712A1 (en) * 2019-10-31 2022-12-08 Sft Laboratory Co., Ltd. Garment body of fan-equipped garment and fan-equipped garment
US11707095B2 (en) * 2018-01-25 2023-07-25 Teijin Limited Garment
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JP6731335B2 (ja) * 2016-12-28 2020-07-29 東田商工株式会社 携帯式衣服内送風機
JP6656630B1 (ja) * 2019-05-30 2020-03-04 株式会社大谷機械製作所 作業衣
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US20060150305A1 (en) * 2003-07-10 2006-07-13 Plut William J Protective apparel breathing assistance
US7636955B2 (en) * 2003-07-10 2009-12-29 Cylena Medical Technologies Inc. Protective apparel breathing assistance
US20100125928A1 (en) * 2004-07-01 2010-05-27 Michael Smith Pneumatic Cooling Apparel System
US20060003688A1 (en) * 2004-07-01 2006-01-05 David Turner Air delivery apparatus and method
US8602855B2 (en) 2004-07-01 2013-12-10 Nike, Inc. Air delivery apparatus and method
US8465351B2 (en) * 2004-07-01 2013-06-18 Nike, Inc. Pneumatic cooling apparel system
US20070118956A1 (en) * 2005-06-29 2007-05-31 Jack Sawicki Personal ventilating garment apparatus
US20070095088A1 (en) * 2005-10-20 2007-05-03 Tiax Llc Body ventilation system and method
US7857841B2 (en) * 2005-10-20 2010-12-28 Arizant Healthcare Inc. Multifunction warming device with an upper body convective apparatus
US20070093885A1 (en) * 2005-10-20 2007-04-26 Arizant Healthcare Inc. Multifunction warming device with an upper body convective apparatus
US20090158496A1 (en) * 2006-04-24 2009-06-25 Stefan Roeckl Glove with inflatable air
EP2474243A1 (en) * 2011-01-05 2012-07-11 Hill-Rom Services, Inc. Cooling system for an occupant of an occupant support and a cooling garment
US10010446B2 (en) 2011-01-05 2018-07-03 Hill-Rom Services, Inc. Cooling system for an occupant of an occupant support and a cooling garment
US20120246788A1 (en) * 2011-03-28 2012-10-04 Harrell Jeremy L Multipurpose Cooling and Trauma Attenuating Devices and Associated Methods
NL2007462C2 (en) * 2011-09-23 2013-03-26 Bartholomeus Theodorus Maria Crasbeek Method and thermal device for controlling the temperature of a patient.
US10575982B2 (en) 2012-11-14 2020-03-03 Benedetti International Limited Vasodilation assembly
CN104797218A (zh) * 2012-11-14 2015-07-22 贝内德蒂国际有限公司 血管舒张组件
WO2014076479A1 (en) * 2012-11-14 2014-05-22 Benedetti International Limited Vasodilation assembly
USD731122S1 (en) 2013-01-14 2015-06-02 Jeremy L. Harrell Inflatable pad
USD738577S1 (en) 2013-01-14 2015-09-08 Jeremy L. Harrell Inflatable pad pattern
USD738576S1 (en) 2013-01-14 2015-09-08 Jeremy L. Harrell Inflatable pad pattern
USD743633S1 (en) 2013-01-14 2015-11-17 Jeremy L. Harrell Inflatable pad pattern
US20140201891A1 (en) * 2013-01-23 2014-07-24 Nike, Inc. Ventilated And Protective Articles Of Apparel
US10195468B2 (en) * 2014-02-20 2019-02-05 Draeger Safety Uk Limited Garment
US20150231419A1 (en) * 2014-02-20 2015-08-20 Draeger Safety Uk Limited Garment
US20150231420A1 (en) * 2014-02-20 2015-08-20 Draeger Safety Uk Limited Garment
WO2016083638A1 (es) 2014-11-25 2016-06-02 Mat Global Solutions, S.L. Prenda transpirable
US20160270457A1 (en) * 2015-03-20 2016-09-22 Chien-Chou Chen Clothes structure with temperature falling device
US10765158B2 (en) 2016-03-25 2020-09-08 Nike, Inc. Foam nodes for creating stand off on apparel items
EP3708015A1 (en) * 2016-03-25 2020-09-16 Nike Innovate C.V. Apparel item with foam ink nodes for creating stand off on apparel items
US11707095B2 (en) * 2018-01-25 2023-07-25 Teijin Limited Garment
US11432597B2 (en) 2019-07-03 2022-09-06 Kwaku TEMENG Pump-conditioned garment and apparatus therefor
US12029263B2 (en) 2019-07-03 2024-07-09 Kwaku TEMENG Pump-conditioned garment and apparatus therefor
US20220386712A1 (en) * 2019-10-31 2022-12-08 Sft Laboratory Co., Ltd. Garment body of fan-equipped garment and fan-equipped garment
US12108814B2 (en) * 2019-10-31 2024-10-08 Sft Laboratory Co., Ltd. Garment body of fan-equipped garment and fan-equipped garment
US20220273906A1 (en) * 2021-03-01 2022-09-01 The Johns Hopkins University Regenerable Carbon Dioxide Scrubber

Also Published As

Publication number Publication date
EP1773143B1 (en) 2010-10-13
ES2353218T3 (es) 2011-02-28
CA2575757C (en) 2010-09-28
CN101022741B (zh) 2011-02-16
CA2575757A1 (en) 2006-08-17
HK1097705A1 (en) 2007-07-06
IL181064A0 (en) 2007-07-04
JP5198860B2 (ja) 2013-05-15
DE602005024142D1 (de) 2010-11-25
PL1773143T3 (pl) 2011-04-29
AU2005327125A1 (en) 2006-08-17
WO2006085998A3 (en) 2006-12-14
EP1773143A2 (en) 2007-04-18
JP2008509291A (ja) 2008-03-27
AU2005327125B2 (en) 2009-05-28
ATE484202T1 (de) 2010-10-15
WO2006085998A2 (en) 2006-08-17
DK1773143T3 (da) 2011-01-31
CN101022741A (zh) 2007-08-22

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