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    ARMY A-A-52414 B-2012 BEARING ROLLER THRUST.pdf

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    ARMY A-A-52414 B-2012 BEARING ROLLER THRUST.pdf

    1、 Beneficial comments, recommendations, additions, deletions, clarifications, etc. and any data that may improve this document should be sent to usarmy.detroit.rdecom.mbx.tardec-standardizationmail.mil or U.S. Army RDECOM, Tank Automotive Research, Development and Engineering Center, ATTN: RDTA-EN/ST

    2、ND/TRANS MS #268, 6501 E. 11 Mile Road, Warren, MI 48397-5000. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https:/assist.dla.mil. AMSC N/A FSC 3110 DISTRIBUTION STATEMENT A. Approved for public release; dis

    3、tribution is unlimited. INCH-POUND A-A-52414B 28 August 2012 SUPERSEDING A-A-52414A 2 August 2005 COMMERCIAL ITEM DESCRIPTION BEARING, ROLLER, THRUST The General Services Administration has authorized the use of this commercial item description (CID) as a replacement for MIL-B-17380A and MS17103A wh

    4、ich are canceled. 1. SCOPE. This CID covers thrust roller bearings consisting of two flat thrust plates, cylindrical rollers, and a retainer (see figure 1). They are used where the shaft axis is parallel to the load. 2. SALIENT CHARACTERISTICS 2.1 Materials. Thrust plates and rollers shall be made o

    5、f vacuum degassed bearing quality steel and have a hardness of RC 58-60 for the thrust plates and RC 60-64 for the rollers. The retainer shall be made of cast bronze or brass and provided with a hardened steel band to resist the outward thrust of the rollers. The use of recovered materials made in c

    6、ompliance with regulatory requirements is acceptable providing that all requirements of this CID are met (see 3). 2.2 Design and construction. The general design and construction features of roller thrust bearings are shown in figure 1. The rollers shall be crowned and their lengths shall alternate

    7、from short to long in successive slots around the body of the retainer. The flat faces of each thrust plate shall be parallel within 1 mil. The roller diameters shall be uniform to within 0.25 mils. The difference in diameter between the rollers in any one bearing assembly shall not exceed 0.25 mils

    8、. The rollers shall remain in the retainer when the bearings are disassembled. Detailed and specific features and dimensions shall be specified in an engineering drawing (see 6.1). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-52414B 2 FIGURE 1

    9、. Bearing configuration. 2.2.1 Size. The size of the roller thrust bearings and tolerances shall be determined based on specific bearing application requirements and shall be given in the engineering drawing. Factors such as load, rpm, environmental conditions (e.g., temperature, humidity) are taken

    10、 into consideration. The basic empirical formula used for the dynamic load capacity is explained in 6.2. 2.2.2 Radius or chamfer. Bearings must clear the maximum fillet radius of the mating shaft or housing. A radius or chamfer (see figure 1), of 0.031 inch minimum, shall be used on the bore and out

    11、er diameter. 2.3 Surfaces. The surfaces labeled 15 and 30 in figure 1 shall have a maximum surface roughness of 15 and 30 microinches, respectively. Ground surfaces shall be free from tool marks, chatter waves, pits, rust or other injurious defects. All other surfaces shall have a smooth machine fin

    12、ish, free from scale. The bearings shall be supplied without lubrication, but with a coating of rust preventive film. 2.4 Identification and markings. The product shall be identified and marked in accordance with the engineering drawing to include, as a minimum, the military part number and the manu

    13、facturers CAGE code and part number (see 6.1). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-52414B 3 2.5 Workmanship. The product shall be free from dirt, oil, or other foreign material, except as required for preservation (see 5.0). Workmansh

    14、ip shall be of a quality which assures a product free from burrs, slivers, surface scratches, or sharp corners or edges. There shall be no paint runs, smears, corrosion or other defects which could adversely affect appearance, operation, or installation. 3. REGULATORY REQUIREMENTS. The offeror/contr

    15、actor is encouraged to use recovered materials to the maximum extent practicable, in accordance with paragraph 23.403 of the Federal Acquisition Regulation (FAR). 4. PRODUCT CONFORMANCE PROVISIONS. 4.1 Contractor certification. The contractor shall certify and maintain substantiating evidence that t

    16、he product offered meets the salient characteristics of this CID and that the product conforms to the producers own drawings, specifications, workmanship standards, and quality assurance practices. Items with known defects shall not be submitted for Government acceptance. The Government reserves the

    17、 right to require proof of such conformance prior to the first delivery and thereafter as may be otherwise provided for under the provisions of the contract or order. 5. PACKAGING. Preservation, packing, and marking shall be as specified in the contract or order (see 6.1). 6. NOTES (This section con

    18、tains information of a general or explanatory nature that may be helpful but is not mandatory.) 6.1 Ordering data. Acquisition documents should specify the following: a. Title, number, and date of this CID. b. If required, the specific issue of individual documents referenced. c. Number and date of

    19、the engineering drawing (see 2.2). d. Military part number and quantity required (see 2.4). e. Selection of applicable level and packaging requirements (see 5.0). 6.2 Basic design formula. The following formula may be used for design and selection. The determination of the operating conditions facto

    20、r (foc) is beyond the scope of this document but can be found according to Anti-Friction Bearing Manufacturers Association (AFBMA) standards. This factor makes an adjustment to the load capacity by considering parameters such as: Reliability, materials, lubrication, dimensions, and external environm

    21、ent. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-52414B 4 C = P (0.00006Ln)0.3/foc where, C = dynamic load capacity rating in pounds P = equivalent dynamic bearing load in pounds L = required or resultant rating life in hours n = operating sp

    22、eed in revolutions per minute fc = overall operating conditions factor (see 6.2) 6.3 Cross-reference. Bearings conforming to this CID are substitutable or interchangeable with bearings conforming to MIL-B-17380A dated 7 April 1954 and MS17103A dated 18 October 1966. 6.4 Metric product. a. Products m

    23、anufactured to metric dimensions will be considered on an equal basis with those manufactured using inch-pound units, provided they fall within specified tolerances using conversion tables contained in the latest revision of ASTM SI10, and all other requirements of this CID are met. b. If a product

    24、is manufactured to metric dimensions and those dimensions exceed the tolerances specified in the inch-pound units, a request should be made to the contracting officer to determine if the product is acceptable. c. The contracting officer has the option of accepting or rejecting the product. MILITARY

    25、INTERESTS: CIVIL AGENCY COORDINATING ACTIVITY: GSA - FAS Custodians: Army - AT PREPARING ACTIVITY: Navy - OS Army - AT Air Force - 99 (Project 3110-2012-001) Review activities: Army - AR Navy - MC, SH Air Force - 84 DLA - GS, IS NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https:/assist.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-


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