AECMA PREN 2342-1982 Heat and Crazing Resistant Acrylic Sheets for Aircraft Glazing Technical Specification Aerospace Series Edition 1《航空航天系列.飞机门窗玻璃用耐蚀丙稀酸的薄板 技术规范》.pdf

《AECMA PREN 2342-1982 Heat and Crazing Resistant Acrylic Sheets for Aircraft Glazing Technical Specification Aerospace Series Edition 1《航空航天系列.飞机门窗玻璃用耐蚀丙稀酸的薄板 技术规范》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2342-1982 Heat and Crazing Resistant Acrylic Sheets for Aircraft Glazing Technical Specification Aerospace Series Edition 1《航空航天系列.飞机门窗玻璃用耐蚀丙稀酸的薄板 技术规范》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、prEN2342 A. E.C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM Edition 1 January 1982 ENGLISH VERSION HEAT AND CRAZING RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING TECHNICAL SPECIFICATION AEROSPACE SERIES FEUILLES DACRYLIQUE RESISTANT LUFT- UND RAUMFAHRT A LA CHALEUR ET AU CRA2ING SPECIFICATION TEC

2、HNIQUE WRMEFORM- UND SPANNUNGSRISSBESTNDIGE ZUR VERGLASUNG VON LUFTFAHRZEUGEN POUR VITRAGES AERONAUTIQUES ACRY LGLASPLATTEN SCRIE AEROSPATIALE TECHNISCHE SPEZI FIKATION This industrial standard for the aerospace sector has been drawn up under the responsibility of AECMA (Association Europenne des Co

3、nstructem de Matriel Arospatial). It is published on yell0 w paper in three equivalent versions (English, French, German). It will be submitted to CEN (European Committee for Standardization) as a draft European Standard. I The equivalent venions in French and German languages COMITE DE NORMALISATIO

4、N can be supplied by B.N.A.E., 8, rue Moreau-Vauthier 92100 BOULOGNE-BILLANCOURT - FRANGE. I Approved by of A.E.C.M. A. 19881.01 -26 I l Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permi

5、tted without license from IHS-,-,-prEN2342 Page 2 AECMA PREN23Li2 82 m 2012312 0002984 1 m - =- QI, c ON TENTS 1 2 3 4 5 6 7 a 9 10 11 12 13 14 15 16 17 18 19 20 SCOPE AND FIELD OF APPLICATION REFERENCES MATERIAL CLASSIFICATION PHYSICAL PROPERTIES OPTICAL DEFECTS OPTICAL PROPERTIES RESISTANCE TO WEA

6、TIHERING THERMAL PROPERTIES MECHANICAL PROPERTIES SUSCEPTIBILITY TO SOLVENT CRAZING DIMENSIONS QUALIFICATION APPROVAL FORMULATION CHANGES SAMPLING AND INSPECTION ACCEPTANCE TESTS PROTECTION AND PACKAGING STORAGE CONDITIONS MARKING COMMENTS ON THE TABLE Copyright Association Europeene des Constructeu

7、rs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN23q2 82 m LO12311 O002985 3 m prEN2342 Page 3 A.E.C.M.A. STANDARD prEN2342 HEAT AND CRAZING RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING TE

8、CHNICAL SPECIFICATION 4 SCOPE AND FIELD OF APPLICATION This standard specifies the supply of heat and crazing resistant cast transparent acrylic sheets for aircraft glazing. REFERENCES EN2155, EN2.55-1 to EN2155-22, Test methods for transparent -. materials for aircraft glazing 1) . MATERIAL The she

9、ets shall be made from a modified acrylic polymer or Co-polymer mainly consisting of methyl methacrylate and shall be controlled under the conditions specified herein. CLASSIFICATION The material shall be available in four classifications as follow : Classe Oa CLasse Ob Classe Oc Classe d with optic

10、al deviation not greater than 130“ (0,00043 rad). Optical distortion not greater than that specified in clause 7.5 when the sheet is mounted at an optical incidence of 60“. with optical deviation not greater than 3 (0,00087 rad). Optical distortion not greater than that specified in clause 7.5 when

11、the sheet is mounted at an optical incidence of 60. _-_- with optical deviation not greater than 6 (0,00175 rad). Optical distortion not greater than that specified in clause 4.5 when the sheet is mounted at an optical incidence of 45O. with optical deviation not greater than 10 (O;0O291 rad). Optic

12、al distortion not greater than that; specified in cl.ause 7.9 when.the sheet is mounted at zero optical incidence. . 1) in preparatjon Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitt

13、ed without license from IHS-,-,-AECMA PREN2342 82 = LOL23LL 0002986 5 9 ,_ . _. prEN2342 Page 4 5 PHYSICAL PROPERTIES 5.1 Density Mass density of the material as determined in EN2155-1 shall be as stated in Gh.e table. 5.2 Water absorption The water absorption as determined in EN2155-2 l) shall not

14、be greater than the value stated in the table. 6 OPTICAL DEFECTS 6.1 The sheets viewed through the cast surfaces shall be colourless. 6.2 The sheets shall have a high polish and be free from scratches and grazes. 6.3 Sheets in classification Oa or Ob shall be examined for defects as in EN2155-6 and

15、shall satisfy the following clauses : 6.3;l There shall be no crazing or voids 6.3.2 Sheets shall not contain defects larger than those defined in EN2155-6 6.3.3 Sheets containing major and/or minor defects as defined in EN2155-6 shall be acceptable providing : 1) An area enclosed by a circle of rad

16、ius 150 mm with each major defect as centre contains no other major defect and not more than three minor defects, 2) An area enclosed by a circle of radius 150 mm and centre at any point on the sheet which does not contain a major defect, contains not more than five minor defects. 6.4 Sheets in clas

17、sification Oc or Od shall be examined for defects as in EN2155-6 to a standard agreed between manufacturer and purchaser. 7 OPTICAL PROPERTIES 7.1 Refractive index The refractive index as determined in .EN2155-3 l). shall be as stated in the table.- -, 1) in preparation b Copyright Association Europ

18、eene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I) I *- -AECMA PREN2342 82 Ri LOL23LL 0002987 7 =- prEN2342 Page 5 7.2 Ultra-violet light transmittance The ultra-violet transmitt

19、ance at any wavelength in the range 290 to 330 nm as determined in EN2155-4 shall not exceed the values shown in figure 1, 7.3 Visible light transmission The visible light transmission as determined in EN2155-5 1 shall not be less than the values stated in the table. 7.4 Optical deviation The optica

20、l deviation as examined in ENZ155-7 shall not be greater than the value quoted in clause 4. 7.5 Optical distortion The optical distortion as determined in EN2155-8 and examined under the viewing angle specified in clause 4 shall not, present : - A gradient exceeding 1 in 17 for classes Oa and Ob and

21、 1 in 12 for the other classes, - Discontinuities d exceeding 0,5 mm, 7.6 Haze As determined in EN2155-9 the average value shall not exceed that stated inthe tableand the maximum single value obtained shall not exceed the stated value by more than 1%. 8 RESISTANCE TO WEATHERING 8.1 Resistance to acc

22、elerated weathering Resistance to accelerated weathering will be determined by EN2155-10 ; requirements may be inserted at a later date. 8.2 Resistance to natural weathering The periods and conditions under which the material is to be exposed shall be decided by agreement between the manufacturer an

23、d purchaser and in accordance with EN2155-11 l. If changes Fire recordeci the acceptabi3ity of the material shall be discussed between manufacturer and purchaser. - I 1) in preparation Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMAN

24、ot for ResaleNo reproduction or networking permitted without license from IHS-,-,-l AECMA PREN2342 82 LOL23LL 0002988 3 W prEN2342 Page 6 9 THERMAL PROPERTIES 9.1 Coefficient of linear thermal expansion The coefficient of linear thermal expansion as determined in EN2155-12 shall not exceed the figur

25、e stated in the table. 9.2 Deformation temperature under load The deformation temperature as determined in EN2155-13 shall not be below that quoted in the tabbe. 9.3 1/10 Vicat softening temperature The softening point of the sheet as determined in EN2155-14 l) shall not be below the figure quoted i

26、n the table. L 1) in preparation 9.4 Thermal stability When tested as described in EN2155-15, the test shwt shall meet the requirements of clauses 6.3 and 6.4 in this standard. It shall show negligible deterioration in its ultraviolet and visible light transmission. 9.5 Flammabili-ty Flammability wi

27、ll be determined by EN2155-16 ; requirement may be inserted at a later date. 10 MECHANICAL PROPERTIES 10.1 Tensile strength and elongation at break When tested as described in EN2155-17 l) no individual value for these properties shall be less than those stated in the table . 10.2 Impact strength Wh

28、en tested as described in EN2155-18 ) the impact strength of test specimens shall not be less than the value stated in the table. 11 SUSCEPTIBILITY TO SOLVENT CRAZING 11.1 Craze resistance When the specimens to be tested are subjected to the conditions of EN2155-19 at a stress of 14 MPa they shall s

29、how no signs of crazing. I. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-12 13 14 15 prEN2342 Page 7 11.2 Retention of strength after crazing Specim

30、ens subjected to the conditions of EN2155-20 shall be acceptable under a stress of 10,4 MPa. Failure of more than one specimen shall entail rejection of the batch. If one specimen fails, a further sample of 10 specimens from a different sheet shall be selected from the same batch and tested under th

31、e same conditions. No specimen shall fail on re-test. DIMENSIONS 12.1 The sheet size and thickness shall be as specified in the contxact or order. 12.2 The thickness of a sheet at; any point. shall riot differ from the nominal thickness by more than & the value given in figure 2 for the particular s

32、ize range. QIJAALIFICATION APPROVAL Before any particular manufacturers materials are supplied as complying with this standard the manufacturer shall obtain qualification approval. Application for approval shall be submitted to the appropriate inspecting authority together with : 13.1 Evidence that

33、the materials comply with all the reqiiirernents specified herein, 13.2 Sufficient material for which approval is sought to meet the test requirements of this standard, 13.3 Details of composition supplied in confidence to the inspecting authority if national. practice requires, 13.4 Recommended for

34、ming and fabrication instructions, 13.5 Details of sheet thicknesses and maximum sizes available. FORMULATION CHANGES Any proposed change by the manufacturer in the formulation and/or the production process shall be notified to the approving authority. If significant the material shall be designated

35、 a new material requiring specific and separate approval. If approved the changed material shall be given a new name or trade symbol. SAMPLING AND INSPECTION 15.1 For a periodic test or batch test a single sheet of material shall be taken at random. The sheet shall be divtded into two equal parts, o

36、ne part shall be tested for compliance with clause 16 of this standard and the other retained for retest in the case of dispute within 3 months. 1) in preparation Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reprod

37、uction or networking permitted without license from IHS-,-,-AECMA PREN2342 82 LOL23LL 0002790 7 prEN2342 Page 8 The term “batch“ refers to any number of sheets of the same casting mix. The term “periodic“ implies that the material shall be tested every three months or at periods agreed between manuf

38、acturer and inspection authority. The storage conditions of specimen shall be those recommended by the manufacturer. 15.2 At hhe discretion of the inspector anybatch of material-may be . tested to the full requirements of this standard, 16 ACCEPTANCE TESTS Any manufacturers material granted qualific

39、ation approval under this standard shall be subject to the following acceptance tests : 16.1 Each sheet - Optical defects according to clause 6.3 for classes Oa and Ob and according to clause 6.4 for classes Oc and d - Optical deviation according to clause 7.4 - Dimensions according to clause 12. 16

40、.2 Each batch - Deformation temperature under load according to clause 9.2 for - 1/10 Vicat softening temperature according to clause 9.3 for - Craze resistance according to clause 11.1. material 6 mm and more in thickness material less than 6 mm in thickness 16.3 Periodic - Ultra-violet light trans

41、mission according to clause 7.2 - Visible light transmission according to clause 7.3 - Haze according to clause 7.6 - Thermal stability according to clause 9.4 - Tensile strength and elongation at break according to clause 10.1 - Retention of strength after crazing according to clause 11.2. 17 PROTE

42、CTION AND PACKAGING I 17.1 Individual sheets shall be protected on both surfaces by a paper or opaque plastic film adhered with a compatible adhesive which can readily be removed without injury to the surfaces. The film shall adequately-protect the surfaces from damage during delivery, storage, hand

43、ling and cutting operations. 17.2 Unless otherwise specified by the purchaser all sheets shall be segregated by thickness and size packed for domestic delivery, The container shall be suitable for maintaining the material in its original. condition and the sheets shall be supported to avoid damage,

44、- - I i _ - Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-i AECMA PREN2342 82 10123L3 0002993 9 psEN2342 Page 9 18 STORAGE CONDITIONS Sheets shall be

45、 stored, protected on both surfaces as defined in clause 17 and stacked in vertical racks with padded separators. The storage area shall be protected from extremes of temperature and humidity 19 MARKING Each sheet of niaterial shall be clearly marked on the protective backing with : . 19.1 The stand

46、ard number 19.2 The name or trade symbol of the manufacturer as designated in the asproval 19.3 The manufacturers batch number or reference 19,4 The sheet thickness. NOTE : The marking called for in clauses 19.1 and 19.2 shall be spaced at approximately 60 cm intervals over the backing material. 20

47、COMrIMENTS ON THE TABLE While a number of the properties included in the table are specific to heat and craze resistant acrylics and are not subject to variation, others do vary. Iri these instances a base minimum value, below which material would not be acceptable to the purchaser, is required. The

48、refore the value quoted intheMleis such a minimum figure (not a minimum average). No specimen as tested according to the standard shall fall below the quoted value. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo repr

49、oduction or networking permitted without license from IHS-,-,-b AECMA PREN2342 82 10123LL 0002792 O prEN2342 Page 10 TABLE . - Properties of craze and heat resistant transparent acrylic sheets 1) in preparation - Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking