1、Designation: F1085 10An American National StandardStandard Specification forMattress and Box Springs for Use in Berths in MarineVessels1This standard is issued under the fixed designation F1085; the number immediately following the designation indicates the year oforiginal adoption or, in the case o
2、f revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification provides the requirements for mat-tresses and box springs that are for use
3、in berths for officers,crew, and passengers in marine vessels. This shall be consid-ered a minimum standard.1.2 The values stated in SI units are to be regarded as thestandard. The values given in parentheses, in inch-pound units,are for information only.1.3 This standard is used to measure and desc
4、ribe theresponse of materials, products, or assemblies to heat andflame under controlled conditions, but does not by itselfincorporate all factors required for fire-hazard or fire-riskassessment of the materials, products, or assemblies underactual fire conditions.1.4 This standard does not purport
5、to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2D123 Te
6、rminology Relating to TextilesD1424 Test Method for Tearing Strength of Fabrics byFalling-Pendulum (Elmendorf-Type) ApparatusD3574 Test Methods for Flexible Cellular MaterialsSlab,Bonded, and Molded Urethane FoamsD3951 Practice for Commercial PackagingD5034 Test Method for Breaking Strength and Elon
7、gationof Textile Fabrics (Grab Test)D6193 Practice for Stitches and SeamsD6413 Test Method for Flame Resistance of Textiles (Ver-tical Test)E162 Test Method for Surface Flammability of MaterialsUsing a Radiant Heat Energy SourceE176 Terminology of Fire StandardsE662 Test Method for Specific Optical
8、Density of SmokeGenerated by Solid MaterialsE1354 Test Method for Heat and Visible Smoke ReleaseRates for Materials and Products Using an Oxygen Con-sumption CalorimeterE1590 Test Method for Fire Testing of MattressesF1566 Test Methods for Evaluation of Innersprings, Box-springs, Mattresses or Mattr
9、ess Sets2.2 ANSI Standards:3ANSI Z357.1-1981 American National Standard for Bed-ding Products and ComponentsANSI/ASQC Z1.4 Sampling Procedures and Tables for In-spection by Attributes2.3 California Bureau of Home Furnishings and ThermalInsulation Standard:CATechnical Bulletin 129, (CATB 129) Flammab
10、ility TestProcedure for Mattresses for Use in Public BuildingsOctober 199242.4 Federal Standards:Code of Federal Regulations Title 16, Vol 2, Part 16325Purchase DescriptionMattressInnerspring, Flame-Resistant, ShipboardNAVSEA 05L PD 4-02 (May2002)61This specification is under the jurisdiction of AST
11、M Committee F25 on Shipsand Marine Technology and is the direct responsibility of Subcommittee F25.03 onOutfitting and Deck Machinery.Current edition approved Dec. 1, 2010. Published January 2011. Originallyapproved in 1988. Last previous edition approved in 2008 as F1085 - 08. DOI:10.1520/F1085-10.
12、2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.3Available from American National Standards Institute (ANSI),
13、 25 W. 43rd St.,4th Floor, New York, NY 10036, http:/www.ansi.org.4Available from California Bureau of Home Furnishings and Thermal Insula-tion, 3483 Orange Grove Ave., North Highlands, CA 95660.5Available from U.S. Government Printing Office Superintendent of Documents,732 N. Capitol St., NW, Mail
14、Stop: SDE, Washington, DC 20401, http:/www.access.gpo.gov.6Available from Naval Sea Systems Command (NAVSEA), 1333 Isaac HullAve., SE, Washington, DC 20376, http:/www.navsea.navy.mil.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.2.
15、5 NFPA Standard:NFPA 301 Code for Safety to Life from Fire on MerchantVessels73. Terminology3.1 DefinitionsFor definitions of terms used in this speci-fication associated with textiles, see Terminology D123. Fordefinitions of terms used in this specification associated withfire issues, see Terminolo
16、gy E176.3.2 Definitions of Terms Specific to This Standard:3.2.1 border, na material that forms the side panel thatsurrounds the perimeter of the mattress and defines its depth.3.2.2 box spring, na foundation for a mattress, consistingof wire spring elements mounted on a frame, generallyupholstered
17、and covered on the top and sides with ticking, andon the bottom with a dust cover.3.2.3 box spring assembly, nan interconnection of coilsprings, border wire, and top wire assembly contained within abox spring.3.2.4 flaming droplets, nflaming molten or flaming lique-fied droplets which fall from the
18、test specimen during the firetest and continue to burn.3.2.5 flange, nstrip of material secured to the perimeter ofan upholstery panel to secure to the innerspring core.3.2.6 innerspring unit, nan interconnection of wire springelements other than mounting on a frame that forms a singleunit that can
19、be incorporated into a mattress.3.2.7 insulator pad, none or more layers of a cushioningsystem between the upholstery and mattress core, whichconsist of foam or other cushioning or filling materials.3.2.8 mattress, nticking filled with a resilient materialused alone or in combination with other prod
20、ucts intended orpromoted for sleeping upon.3.2.9 mattress core, nthe main support system that maybe present in a mattress, such as springs, foam, or resilientfilling.3.2.10 mattress, innerspring, nany mattress containing aninnerspring unit.3.2.11 mattress, solid core, nany mattress containingpadding
21、, but not an innerspring unit.3.2.12 quilted, adjstitched with any thread or by fusionthrough the ticking and one or more layers of upholsterymaterial.3.2.13 tape edge, nseam or border edge of a mattress.3.2.14 ticking, nthe outermost layer of fabric or relatedmaterial that encloses the core and uph
22、olstery materials of amattress or mattress pad.4. Ordering Information4.1 Orders for items purchased under this specification shalldefine the following:4.1.1 MattressesQuantity, dimensional requirements, type(solid core or innerspring), and weight per each size.4.1.2 Box SpringsQuantity, dimensional
23、 requirements,and weight per each size.4.1.3 Upholstery material selections are to be offered aschoices by the manufacturer or distributor to the purchaser. Theselection shall be of good quality suitable for commercial useand for use aboard U.S. Navy vessels.4.1.4 When first article of inspection is
24、 required, it shall bespelled out in the paperwork.5. Materials and Manufacture5.1 Innerspring MattressThe essential components of aninnerspring mattress are: an innerspring core, cushioning,upholstery ticking (either quilted or with a smooth top, andpotentially including a flange), and a border. Op
25、tional compo-nents include various insulating layers or pads, flanges, andtapes. All materials used shall meet the mechanical propertyand fire performance requirements of Table 1. All materialsused shall comply with appropriate commercial bedding indus-try standards of manufacture and durability. An
26、y constructionof an innerspring mattress that is suitable for its intended useand that complies with the performance requirements shownherein shall be permitted to be used.5.1.1 Innerspring CoreThe innerspring core shall be con-structed from an all-wire carbon steel. The coils shall extendthe full l
27、ength and width of the mattress. The coils shall bepermanently secured to provide long-term structural stability.Various core designs shall be permitted. The support propertiesof the innerspring core, in terms of firmness rating, durability,resistance to impact, firmness retention, and surface defor
28、ma-tion, shall be assessed by Test Methods F1566. The coils, or thecomplete spring unit assembly, shall be given suitable thermaltreatment to relieve residual stresses caused by coiling.5.1.2 Cushioning and Insulator LayersAn insulator padshall be placed over each sleeping surface of the innerspring
29、core to insulate the upholstery from the core. The variouscushioning layers shall be constructed of materials that meetthe performance requirements of Table 1.5.1.3 Ticking and Cover AssemblyThe cover constructionshall be suitable for the type of mattress construction used.Upholstery ticking materia
30、ls shall be durable, per commonbedding industry practices. The ticking for each sleepingsurface shall be cut in one piece without fabric splices. Theticking for the mattress border shall be made of not more thantwo pieces of ticking, with the ends spliced and sewn togetherin a continuous manner leav
31、ing no gaps or voids in uniformityand finish. The border assembly shall be secured to the top andbottom sleeping surfaces of the mattress, by automatic sewing,per common bedding industry practices.5.1.4 BorderThe ticking for the mattress border shall bemade of not more than two pieces of ticking, wi
32、th the endsspliced and sewn together in a continuous manner leaving nogaps or voids in uniformity and finish. The border assemblyshall be secured to the top and bottom sleeping surfaces of themattress, by automatic sewing, per common bedding industrypractices.5.1.5 TapeA tape shall be permitted to b
33、e used to concealthe seams formed between the border, if present, and anupholstery panel. The tape shall be continuously stitched alongthe total length of each seam, with no gaps or voids betweenthe upholstery panel and border surfaces.7Available from National Fire Protection Association (NFPA), 1 B
34、atterymarchPark, Quincy, MA 02169-7471, http:/www.nfpa.org.F1085 1025.1.6 Seam and StitchingThe seam and stitch types shallbe in accordance with Practice D6193. All seams shall besecurely stitched. Seams shall not slip or pull out.5.1.7 MattressAll mattress components shall meet therequirements of T
35、able 1, as appropriate. The overall mattressshall meet the performance requirements of Table 2,asTABLE 1 Mattress Component RequirementsComponent Characteristic Requirement Test MethodUpholstery Ticking(and Flange, Tape, and Pocketing Materials, if used)(Notes 1 and 2)Initial FlammabilityChar Length
36、 #127 mm (5.0 in.) Test Method D6413After Flame #2.0 s Test Method D6413No Flaming Droplets Test Method D6413Flammability after 15 LaunderingsChar Length #127 mm (5.0 in.) Test Method D6413After Flame #2.0 s Test Method D6413No Flaming Droplets Test Method D6413Other PropertiesTear Strength (Note 3)
37、 Warp: 1.6 kg (3.5 lb) min;Filling: 1.6 kg (3.5 lb) minTest Method D1424Breaking Strength (Note 3) Warp: 42.6 kg (94 lb) min;Filling: 26.3 kg (58 lb) minTest Method D5034Border Ticking FlammabilityChar Length #38 mm (1.5 in.) Test Method D6413After Flame #2.0 s Test Method D6413No Flaming Droplets T
38、est Method D6413DMAX50 Test Method E662DMAXNo Flaming Droplets Test Method E662Other PropertiesTear Strength Warp: 1.8 kg (4 lb) min;Filling: 1.8 kg (4 lb) minTest Method D1424Breaking Strength Warp: 42.6 kg (94 lb) min;Filling: 22.7 kg (50 lb) minTest Method D5034Cushioning and Insulator Layers Fla
39、mmabilityChar Length #127 mm (5.0 in.) Test Method D6413After Flame #2.0 s Test Method D6413No Flaming Droplets Test Method D6413Flame Spread (Is)(Note 4 10 Test Method E162DMAX(Note 4) 200 Test Method E662DMAX(Note 4) No Flaming Droplets Test Method E662Other PropertiesDry Heat Aging /Compression F
40、orce DeflectionNo more than 20 % change incompression force deflectionTest Method D3574,Methods C and KNOTE 1Only Molten and/or Flaming Droplets requirement applies to Tape.NOTE 2Only Initial Flammability requirements apply to Pocketing Material.NOTE 3Tear Strength and Breaking Strength apply only t
41、o Upholstery Ticking.NOTE 4When materials are not identical on both sides, each side shall be tested as a different specimen.TABLE 2 Full Mattress RequirementsCharacteristics Requirement Test MethodFire Performance CharacteristicsMinimum a. Maximum Rate of Heat Release #100 kW Test Method E1590b. Ma
42、ximum Total Heat Release in first 10 min of test #25 MJ Test Method E1590c. Maximum Mass Loss in the first 10 min of test #1.4 kg (3 lb) Test Method E1590d. Class A Pass 16 CFR 1632Optional (US Navy Requirement) a. Maximum Rate of Heat Release #150 kW Annex A1b. Maximum Average Specific Extinction A
43、rea 300 m2/kg Annex A1c. No Flaming Droplets Annex A1Optional Screening Test Mass loss #15 % (based on initial mass) Annex A3Physical CharacteristicsDurability (Rollator Test) a. Firmness Rating of 330 N (75 lbf) 6 10 %, after 100 000 cycles Test Method F1566, Section 7b. Permanent Deformation #20 %
44、 of depth Test Method F1566, Section 7c. No Damage Test Method F1566, Section 7Firmness Retention and Surface Deformation (Cornell Test) a. Accumulated Dimple #44.5 mm (1.75 in.) Test Method F1566, Section 9b. Support Firmness Change #(+ 40 %) - (-15 %) Test Method F1566, Section 9Dimensions See Sec
45、tion 6Weight See Section 6Visual CharacteristicsVisual Defects See section 6.5 ANSI/ASQC Z1.4F1085 103discussed in Section 6. For dimensional requirements, see 6.6.5.1.7.1 Upholstery ticking, as well as any flange, tape, andpocketing materials used, shall exhibit a char length notexceeding 127 mm (5
46、.0 in.), an after flame period not exceed-ing 2.0 s, and shall not exhibit any molten or flaming droplets,or both, when tested in accordance with Test Method D6413.The char length and after flame requirements shall not apply totape.5.1.7.2 Upholstery ticking, as well as any flange, tape, andpocketin
47、g materials used, shall exhibit a char length notexceeding 127 mm (5.0 in.), an after flame period not exceed-ing 2.0 s, and shall not exhibit any molten or flaming droplets,or both, when tested in accordance with Test Method D6413,after having been subjected to 15 launderings. The char lengthand af
48、ter flame requirements shall not apply to tape.5.1.7.3 Border ticking materials shall exhibit a char lengthnot exceeding 38 mm (1.5 in.), an after flame period notexceeding 2.0 s, and shall not exhibit any molten or flamingdroplets, or both, when tested in accordance with Test MethodD6413. Border ti
49、cking materials shall also exhibit a maximumspecific optical density (DMAX) not exceeding 50, and shall notexhibit any molten or flaming droplets, or both, when tested inaccordance with Test Method E662.5.1.7.4 Cushioning and insulator layer materials shall ex-hibit a char length not exceeding 127 mm (5.0 in.), an afterflame period not exceeding 2.0 s, and shall not exhibit anymolten or flaming droplets, or both, when tested in accordancewith Test Method D6413. Cushioning and insulator layermaterials shall also exhibit a radiant panel index (Is)
