FORD ESS-M11P24-A1-2013 ADHESIVE MALE THREADED FASTENER - FOR SERVICE TEMPERATURES BELOW 135 C TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Para. No. Revisions 2013 12 12 N Status No replacement named. L. Sinclair, NA 1983 06 17 Released Controlled document at www.MATS Page 1 of 5 ADHESIVE, MALE THREADED FASTENER - FOR SERVICE ESS-M11P24-A1 TEMPERATURES BELOW 13
2、5 C ADHESIVE, MALE THREADED FASTENER - FOR SERVICE ESS-M11P24-A2 TEMPERATURES BELOW 65 C NOT TO BE USED FOR NEW DESIGN 1. SCOPE These specifications define the performance requirements for adhesives which are pre-applied to the threads of any externally threaded fastener. The applied adhesive shall
3、be dry to the touch and become activated only when the coated fastener is inserted into a threaded hole or mating fastener where it then hardens to enhance resistance to loosening. No specific class or type of adhesive (anaerobic, epoxy, microencapsulated, etc.) is intended for exclusive use in this
4、 specification, but any composition which will meet the performance requirements below will be considered for approval. 2. APPLICATION These specifications were released originally for materials used for making fasteners more resistant to loosening. In all cases where ES-20007-S100 and ES-20010-S100
5、 are specified, ESS-M11P24-A1 and ESS-M11P24-A2 are their respective replacements and are technically equivalent. 3. REQUIREMENTS 3.1 ADHESIVE ELEMENT APPLIED TO THREADS 3.1.1 The length of adhesive material shall be a minimum of 1.5 times the nominal diameter of the threaded fastener, starting with
6、in two threads of the end of the fastener. The first thread of the fastener need not be clean of adhesive, but shall allow a finger effort start for a minimum of one revolution after first engagement. The adhesive coating process shall not degrade the specified corrosion protection. 3.1.2 The adhesi
7、ve element, when pre-applied on the threads, shall be dry to the touch and shall not cause the fasteners to bond together prior to application. It shall remain dormant until the shearing action of the mating thread activates the adhesive, which after proper curing time and temperature, shall harden
8、and form a bond between the mating threads. ENGINEERING MATERIAL SPECIFICATION ESS-M11P24-A1 ESS-M11P24-A2 Page 2 of 5 3.2 GENERAL 3.2.1 During the complete performance of the test, the nut shall be turned while the test bolt is restrained from turning. Test nuts shall be Ford Standard Nuts as liste
9、d in Tables I and II. Each test nut shall be gauged to assure conformance with dimensional requirements. Some of the terms used below are defined as follows: Prevailing “On“ Torque - the torque in the “on“ direction, when the nut is completely in engagement with the adhesive portion of the external
10、thread, as measured during the initial installation with the fastener in motion while bolt tension is zero. Prevailing “Off“ Torque - The torque in the “off“ direction measured during the first 360 of rotation after the nut has been broken from the hardened bond while bolt tension is zero. Adhesive
11、Break Torque - The torque in the “off“ direction which breaks the hardened adhesive between the mating threads while the bolt tension is zero. 3.2.2 First Application Room Temperature Test (30 Samples) The test nut shall be assembled with the adhesive coated bolt until one full adhesive coated threa
12、d protrudes through the nut. The maximum prevailing-on torque shall be measured and recorded during the next 360 nut rotation, while the nut is in constant motion. The speed of rotation shall be 10 - 20 rpm. The activated adhesive bolt-nut assembly shall be allowed to harden at 23 +/- 1 C ambient te
13、mperature. After 72 h curing time the maximum adhesive break torque and the maximum prevailing-off torque during the next 360 nut rotation shall be measured and recorded. ENGINEERING MATERIAL SPECIFICATION ESS-M11P24-A1 ESS-M11P24-A2 Page 3 of 5 3.2.3 Hot Strength Test (10 Samples) Test procedure is
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