AECMA PREN 2261-1994 Aerospace Series Silicone Rubber (VMQ) Hardness 70 IRHD Edition 1《航空航天系列硅胶(VMQ)硬度50 IRHD.第1版》.pdf

1、(EN PRENr22bL 94 3404589 0066330 63T Edition approved for publication 1994-07-25 AECMA STANDARD NORME AECMA AECMA NORM The equivalent versions in French and German languages can be supplied by B.N.A.E. - Technopolis 54 - 199. rue Jean-Jacques Rousseau 92138 ISSY - LES - MOULINEAUX CEDEX - FRANCE prE

2、N 2261 Edition 1 July 1994 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AkROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 47.36.98.76 UDC : 678.074 : 620.1 : 629.7 Descriptors : Aircraft industry, rubber, silicones, hardness ENG

3、LISH VERSION Arospace series Silicone rubber (VMQ) Hardness 70 IRHD Srie arospatiale lastomre silicone (VMQ) Duret 70 DIDC Luft- und Raumfahrt Silicon-Elastomer WMQ) Hrte 70 IRHD This “Aerospace series“ Standard has been drawn up under the responsibility of AECMA (Association Europenne des Construct

4、eurs de Matriel Arospatial. It is published on yellow paper in three equivalent versions (English, French, German). it will be submitted as a draft European Standard to CEN (European Committee for Standardization for formal vote. Copyright Association Europeene des Constructeurs de Materiel Aerospat

5、ial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CEN PRENx2261 Y m 3404589 0066131 576 Page 3 prEN 2261 : 1994 1 scope This standard specifies the properties of silicone rubber (VMQ) I), hardness 70 IRHD, for aerospace app

6、lications. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications, These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to

7、 or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 1629 Rubber and latices - Nomenclature IS0 181 7 Rubber, vulcanized - Determination

8、of the effect of liquids EN 3207 Aerospace series - Rubber compounds - Technical specification 2) 3 Application of the material The suitability of the material for a specific application shall be determined by complementary tests carried out on the finished product as the properties specified in thi

9、s standard are obtained from standard test specimens. 3.1 Typical use For application as ozone and weather resistant rubber with good thermal properties. NOTE : The ozone resistance test is not required. 3.2 Temperature range - Continuous service : from - 55 OC to + 200 OC - intermittent service : f

10、rom - 55 OC to + 260 OC 4 Properties See tables 1 and 2. For qualification, all tests shall be performed. For batch acceptance, the tests identified in tables 1 and 2 shall be performed. 5 Designation Description block I Identity block RUBBER I- l Number of this standard I 6 Technical specification

11、EN 3207 1) Symbol as per IS0 1629 2) In preparation at the date of publication of this standard Previous page is blank Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without licen

12、se from IHS-,-,-CEN PREN*2263 94 3404589 0066332 402 Density Page 4 prEN 2261 : 1994 Mglm3 1) *) Line Tensile strength Elongation at break E 15 M Pa 5 min. “1 % 150 min.“) 15.; Tear strength 17 I I Nlmm I 9 min. y 20 Resistance to low temperatures TR1 O Crystallization 1 20.1 OC - 40 max. Point I Co

13、mpression set after 70 h to 150 OC after - h to - OC Ozone resistance Ozone concentration : ( - I - 1 pphm Elongation of test piece : % Time h Temperature OC Corrosion and adhesion on metals in a dry atmosphere Time :-h Temperature : - OC Corrosion and adhesion on metals in a damp atmosphere Time :-

14、h Temperature : - OC Humidity : - Yo Time :-h Temperature : - OC Humidity : -% I 20.2 % 40 max. “1 28 Table 1 - Test methods 1 Properties Units I Requirements Hardness Modulus at - % strain I MPa I *) Test for batch acceptance. 1) The value determined for each batch shall not differ from that determ

15、ined at qualification by more than 0,02 Mg/m3. 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-,-,- CEN PRENM22bL 94 3404587 0066333 347 = Units 70 h/225 O

16、C Page 5 prEN 2261 : 1994 Table 2 - lests after exposure to test media 1 Column Line 51 4 Test media Oil No. 1, see IS0 1817 1 No. 101, see 70 h/l50 OC Conditions of exposure in test media 2 70 hl150 OC 3 Volume %I - +10 +I O 4 Mass %I - Permitted variation of the properties compared to the initial

17、value Tensile strength % 1 -25 max.- 5 6 - 20 max. Elongation at break % I -40max. - 15 max. O - 10 Hardness 7 a “1 Test for batch acceptance 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-,-,-