1、AECMA PREN2155 BO W LO12311 0002270 b -. Approved by COMITk DE NORMALISATION Of A.E.C.M.A. 79-07-31 A. E .C .M .A. STAN DARD NO RM E A.E .C.M .A, A.E,C.M.A. NORM The equivalent versions in French and German languages can be supplied by B.N.A.E., 8, rue Moreau-Vauthier 92100 BOULOGNE-BILLANCOURT - FR
2、ANCE. DRAFT prEN2155 Edition 1 March 1980 ENGL SH VERSION TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING AEROSPACE SERIES METHODES DESSAIS POUR MATERI AUX TRANSPARENTS POUR VITRAGES ACRONAUTIQUES SERIE AEROSPATIALE LUFT-UND RAUMFAHRT PR FVE R FAH REN FUR TRANSPARENTE WERKSTO FE ZUR VERG
3、LASUNG VON LUFTFAHRZEUGEN The text of this standad, whkh exists in three equivalent versions (English, French, German) has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial) and has been circulated to Official Services. An y reservations e
4、xpressed by Official Servkes and not resolved in this issue, have been incorporated in the history sheet which has accompanied this prEN to CEN. It is published on yellow paper as a draft European Standard intended to receive, under the same presentation and according to its own rules, the approval
5、of CEN (European Committee for Standardization). -, F -“ . prEN2155 AECMA PREN2155 80 3032313 0002273 A Page 2 CO NT E hTS 1 SCOPE AND FIELD OF APPLICATION 2 REFESENCES 3 EhVIROWNT FOX CONDITIONIXG Ah9 TESTING 4 METHODS !IF TEST . . AECNA PREN2155 80 W! 1012313 0002272 T M prEN2155 Page 3 DRAFT EURO
6、PEAN STANDARD AEROSPACE SERIES prEN2155 TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING 1 SCOPE AND FIELD OF APPLICATION This standard specifies 22 methods of test for determination of the properties, mechanical, physical, optical and thermal of transparent sheet for aircraft glazing mat
7、erials. 2 REFmENCES EN2155, Part 1 to Part 22, Test methods for transparent materials for aircraft glazing. 3 ENVIRONMENT FOR CONDITIONING AND TESTING If not otherwise stated, conditioning and test environment does not require close control. The test: conditions shall be within 23 k 5C and specimens
8、 shall be maintained within this range for not less than 4 hours prior to test. _- AECMA PREN2155 80 W LOLZ311 0002273 L W - prEN2155 Page 4 4 IIiETHODS OF TEST TABLE 1 Title _I_- - . I - - -_ _-l_ll TEST FTHODS FOR TRAKSPARENT MATERIALS FOR AIRCRAET GLAZING. .PART 1 DETERMIXATION OF DEIS ITY AND RE
9、LATIVE DENSITY TEST NETHODS FOR TRANSPARENT NATERIALS FOR AIRCRAFT GLAZING. PUT 2 DETERMINATXOH OF WATER ABSORPTION - - I - TEST EWH9DS FOR TRANSPAREIIT MTERIALS FOR AIRCRAFT GLAZING. PART 3 DETSRI.IINATIO# OF REFRACTIVE INDEX TEST KETHGDS FOR TRANSPARENT MTERIALS FOR AIRCRAFT GLAZING. PAXT 4 _I_ -.
10、_ - _ -. - . I-=- .- - DETERMINATIOH OF ULTRA-VIOLET RADIATIOR TRAPISMISSION AT 290 TO 330 PA TEST NETHODS FOR TRANSPAREhT MATERIALS FOR AIRCRAFT GLAZING. PUT 5 DETERMIKATION OF VISIBLE LIGhT TRANSMISSION TEST BTHCDS FOR TRANSPAREFT !-IATERIAM FOR AIRCRAFT GLAZING. PART 6 DETERMINATION OF OPTICAL DE
11、FECTS TEST YlTKCDS FOR TPANSPARENT IATERIALS FOR AIRCRAFT GLAZING. PART 7 -I -I_- I-_- _. DETERIIJAflTIOB OF OPTICAL DEVIATION -_-_I._- . _-_ -_ TEST !*ETHODS FOR TRANSPAREIGT FATERIALS FOR AIRCRAFT GLAZING. PART 8 DETERMINATION OF OPTICAL DISTORTION TEST IETHODS FOR TRAXSPARENT MATERIALS FOR ARCRAF
12、T GLAZING. PART 9 DETER13INATION OF HAZE TEST I.IETIiODS ?OR TRANSPARENT KATERIALS FOR AIRCRAFT GLAZIHG. PART 10 DETERIE3!AATION OF RES ISTAhTCE TO ACCELEFATED WEATHERING TEST KETHODS FOR TRANSPARENT MATERIALS FOR AIRCRU? GLAZING. PART 11 DETERMINAA-IOW OF RESISTANCE TO NATURAL WEATEFERING _ _-.“_-I
13、-.- I_ -. _. -._I. -. . _._-_-I_._ _- _l_,_,_ . - - -_I- _ ., - . _ I -. -._- _._II_- -.lll- _I_-. TEST METHODS FOR TRANSPARENT MTERIALS FOR AIRCRAFT GL4ZXNG. PAIT 12 DETERMINATIOW OF LIXAR THERNAL EXPANSIOIT TEST KXTHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZIRG. PART 13 DETERKINAFION OF TENPE
14、RATURE OF DEFLECT ION UKJIER LOAD _l_l_._I_._ l.-l_._II - -I - _._I_ . - . TEST IETHODS FOR TRANSPAREhT MATERIALS FOR AIRCRAFT GL4ZIITG. PART 14 DETERMINATIOE OF THE 1/10 VICAT SOFTENING TEGERATURE - _ . _ - _I- - .- . .- - . -. - .- -. TEST IBODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING, PART
15、 15 . . . . DETERt*IIJATION OF THERMAL STABILITY TEST IETHODS FOR TRANSPAREhT MATERIALS FOR AIRCRAFT GLAZING. PART 16 DETERMINATION OF FLAE!Ki3ILITY _ _-I-I._ ._-_ . - _ - -_ - : . .- _-. - - . -. . . ,. . . _. . - ._ - . . . TEST KETEODS FOR TRANSPAREhT NATERIALS F3R AIRCRAFT GLAZING. PART i7 DETER
16、KINATION OF TENSILE PROPERTIES TEST NETHODS FOR TRANSPARENT KATERIALS FOR AIRCRAFT GLAZIKG. PART 18 DETERMINATION OF CHARPY II.1PACT RES ISTARGE TEST ElETHODS FOR TRANSPAfiEXT MATERIALS FOR AIRCRAFT GLAZIXG. PART 19 DETERMINATION OF CRAZE RESISTANCE - I_II I_ . , . _ . . . - - -. - -. - - .- 1 - -_-
17、, . . ._ . . . .- _-._ r - . . . . . - . -. - .II- , . _- _CI._- -II_ TEST IGDHODS FOR TMNSPAREh MATERIALS FOR AIRCRAFT GLAZING. PART 20 DETERKCNATION OF RETENTION OF STRENGTH AFTER GRAZ IWG TEST KETHODS FGR TRANSPAREKT NATERIALS FOR AIRCWF“ GLPiZ1l:G. FART 21 DETERIZXAZICB OF PIESISTANCE TO CRACK PROPAGATION (K factor) EK2 15 5 - 6 EN2 155-7 EN2155-8 EN2155-9 EN2155-lO1) EN2 15 5 - 11 EN21 j5-12 - EN2155-13
