AECMA PREN 2799-1995 Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 90 IRHD Edition P 1《航空和航天系列氟烃树脂涂料(FPM) 低压缩形变硬度50 IRHD》.pdf

《AECMA PREN 2799-1995 Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 90 IRHD Edition P 1《航空和航天系列氟烃树脂涂料(FPM) 低压缩形变硬度50 IRHD》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2799-1995 Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 90 IRHD Edition P 1《航空和航天系列氟烃树脂涂料(FPM) 低压缩形变硬度50 IRHD》.pdf（4页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA PREN*2799 95 I LOL23bl 0008392 280 AECMA STANDARD NORME AECMA AECMA NORM prEN 2799 Edition P 1 April 1995 DIT PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopoiis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1 ) 47.36.98.76 ICs : Descrip

2、tors : ENGLISH VERSION Aerospace series Fluorocarbon rubber (FPM) Low compression set Hardness 90 IRHD Srie arospatiale lastomre fluor (FPMI Faible dformation rmanente aprs compression Duret 90 DIDC Luft- und Raumfahrt Fluorocarbon-Elastomer (FPM) niedriger Druckverformungsrest Hrte 90 IRHD This “Ae

3、rospace Series Prestandard has been drawn up under the responsibility of AECMA IAssociation Europenne des Constructeurs de Matriel Arospatiall. It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee followin

4、g comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-ideniification of the standard. After examination and signature of the AECMA Stand

5、ard Checking Centre (NPS) and formal agreement of the Officiai Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199. rue Jean-Jacques

6、Rousseau - 921 38 ISSY-LESMOUUNEAUX CEDEX Comments should be sent within six months after the date of publication to I Edition approved for publication 1995-04-28 AECMA Technopolis - 175, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex - FRANCE C 7 Chairman M. Wright Copyright Association

7、 Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN*2799 95 1012311 0008393 117 H Page 3 prEN 2799 : 1995 1 Scope This standard specifies the properties of fluorocar

8、bon rubber (FPMI), low compression set, hardness 90 IRHD, for aerospace applications. f. 2 Normative references IS0 1629 Rubber and latices - Nomenclature IS0 1817 Rubber, vulcanized - Determination of the effect of liquids EN 3207 Aerospace series - Rubber compounds - Technical specification *I 3 A

9、pplication 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 this standard are obtained from standard test specimens. 3.1 Typical use Application requiring a resista

10、nce to air, hydrocarbon and synthetic oils, fuels at elevated temperature and low compression set properties. 3.2 Temperature range - Continuous service : from - 20 OC to + 225 OC - Intermittent service : from - 20 OC to + 250 OC 4 Properties See tables 1 and 2. For qualification, all tests shall be

11、 performed. For batch acceptance, the tests identified in tables 1 and 2 shall be performed. 5 Designation Description block RUBBER Identity block EN2799 I Number of this standard I 6 Technical specification EN 3207 1) Symbol as per IS0 1629 2) In preparation at the date of publication of this stand

12、ard 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 license from IHS-,-,-Properties Hardness Units IRHD Tear strength N/mm Crystallization zompressio

13、n set after 70 h to 200 OC Point % Page 4 prEN 2799 : 1995 Table 1 - Test methods 1 2 3 Line , Reauirements g0+5 *I -4 1 2 3 4 I Densitv I Mdm3 11 * I Tensile strenath 1 MPa 5 11 min. *I 6 7 Elongation at break 1 % 120 min. *) 8 9 10 I Modulus at - % strain I M Pa 11 12 13 Resistance to low temperat

14、ures TRI O I OC - 12 max. 14 15 15.1 30 max. “1 15.2 after - h to - OC I 16 Ozone resistance 3zone concentration : ( - - + - ) pphm Elongation of test piece : % rime h Temperature OC Eorrosion and adhesion on metals in a dry atmosphere Time :-h Temperature : - OC Corrosion and adhesion on metals in

15、a damp atmosphere Time -h Temperature : - oc Humidity : - Yo Test fluid 17 18 19 20 20.1 Time -h Temperature : - OC Humidity :-% Test fluid *- 20.2 21 22 23 24 25 26 27 I _, 28 29 “1 Test for batch acceptance. 1) The value determined for each batch shall not differ from that determined at qualificat

16、ion by more than OD3 Mg/rn3. 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-,-,-Page 5 prEN 2799 : 1995 2 Table 2 - Tests after exposure to test media Con

17、ditions of exposure in test media 1 I Test media I t 3 t-7 Permitted variation of the properties compared to the initial value 171 Volume Mass Tensile strength Elongation at break Hardness 2 Units , % % % % IRHD Liquid B Fluid 101 1 ISl7 I ISl7 Air 70 hi250 OC 70 hi23 OC 70 hi200 OC q I- - 20 max. I I- - 20 max. O -15 +5 k 5 “1 *) Test for batch acceptance. 4&# 1 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-,-,-