DLA A-A-59652 B-2011 BEARINGS ROLLER TAPERED SINGLE ROW STEEP ANGLE FLANGED CUP (TYPE TSSF).pdf

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1、Beneficial comments, recommendations, additions, deletions, clarifications, etc. and any data that may improve this document should be sent to: STDZNMGTdla.mil or DLA Aviation VEB, 8000 Jefferson Davis Highway, Richmond, VA 23297-5616. Since contact information can change, you may want to verify the

2、 currency of this address information using the ASSIST database at https:/assist.daps.dla.mil/. FSC 3110 INCH-POUND A-A-59652B 8 September 2011 SUPERSEDING A-A-59652A 22 May 2006 COMMERCIAL ITEM DESCRIPTION BEARINGS, ROLLER, TAPERED, SINGLE ROW, STEEP ANGLE, FLANGED CUP (TYPE TSSF) The General Servi

3、ces Administration has authorized the use of this commercial item description for all federal agencies. 1. SCOPE. This commercial item description (CID) covers government acquisition requirements for complete (cone with rollers and cup) single row, tapered, roller bearings with steep angle, flanged

4、cup (type TSSF) for general purpose use. These bearings are not intended for use in special precision applications such as on aircraft, precision ordnance, or submarine equipment. 2. CLASSIFICATION. The roller bearings shall be of one type (TSSF) and classified by the size codes listed in table I. T

5、he column headings in table I refer to bearing characteristics defined in figure 1. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59652B 2 FIGURE 1. Bearing characteristics. Provided by IHSNot for ResaleNo reproduction or networking permitted w

6、ithout license from IHS-,-,-TABLE I. Size codes and dimensions. 1Part numbers are for reference only. Part numbers reflect the cup and cone numbers used by industry and the ABMA. Some cones and cups may be used in multiple configurations and are not limited to one bearing assembly. 2These maximum fi

7、llet radii shall be cleared by the bearing corners. 3Minus value indicates load center inside cone backface. 3Size code Part number 1d D T T 1B C R 2D 1C 1d bd aD aK factorBasic dynamic load ratings (lb.) a 3Bore Outside diameter Bearing width StandoutCone width Cup width Shaft fillet radiusFlange B

8、acking shoulder diameters Effectiveload center Cone-cup Diameter Width Shaft Housing Radial001 21075 - 21212-B 0.7500 2.1250 0.8750 0.4062 0.8598 0.6250 0.06 2.2772 0.1562 1.24 1.04 2.05 0.99 7500 -0.23 002 23100 - 23256-B 1.0000 2.5625 0.8750 0.4063 0.8450 0.6250 0.06 2.7147 0.1563 1.54 1.36 2.48 0

9、.80 88100 -0.09 003 41126 - 41286-B 1.1250 2.8593 0.9688 0.5000 0.9550 0.6875 0.06 3.0741 0.2187 1.63 1.45 2.76 0.97 11200 -0.16 004 43125 - 43312-B 1.2500 3.1250 1.0000 0.5313 0.9478 0.6875 0.06 3.3390 0.2188 1.73 1.63 3.03 0.08 12500 -0.08 005 43131 - 43312-B 1.3125 3.1250 1.0000 0.5313 0.9478 0.6

10、875 0.14 3.3390 0.2188 2.01 1.65 3.03 0.08 12500 -0.08 006 43132 - 43312-B 1.3125 3.1250 1.0000 0.5313 0.9478 0.6875 0.08 3.3390 0.2188 1.89 1.66 3.03 0.08 12500 -0.08 007 44143 - 44348-B 1.4375 3.4843 1.0000 0.5312 0.9330 0.6875 0.09 3.6983 0.2187 2.13 1.97 3.39 0.09 13600 0.09 008 44162 - 44348-B

11、1.6250 3.4843 1.0000 0.5312 0.9330 0.6875 0.09 3.6983 0.2187 2.24 2.00 3.39 0.09 13600 0.09 009 53176 - 53387-B 1.7500 3.8750 1.2188 0.6563 1.1142 0.8125 0.05 4.1210 0.2500 2.32 2.08 3.62 0.79 16200 -0.01 010 55209C - 55437-B 2.0000 4.3750 1.1875 0.5938 1.0594 0.8125 0.14 4.5938 0.2188 2.80 2.54 4.2

12、1 0.03 20600 0.30 011 55206 - 55437-B 2.0625 4.3750 1.1875 0.5938 1.0594 0.8125 0.14 4.5938 0.2188 2.83 2.52 4.21 0.03 20600 0.28 012 55206C - 55437-B 2.0625 4.3750 1.1875 0.5938 1.0594 0.8125 0.14 4.5938 0.2188 2.83 2.54 4.21 0.03 20600 0.30 013 66225 - 66462-B 2.2500 4.6250 1.3125 0.6250 1.2500 0.

13、9375 0.14 4.8750 0.2500 2.99 2.71 4.45 0.93 24000 -0.01 014 HM911249 - HM911210-B 2.4375 5.1250 1.4375 0.7500 1.3125 0.9375 0.14 5.3750 0.2500 3.35 2.93 4.87 0.71 26900 0.21 015 9380 - 9321-B 3.0000 6.7500 1.9375 1.0000 1.8125 1.2500 0.14 7.0620 0.3125 4.13 3.87 6.46 0.76 49100 0.17 016 9386H - 9321

14、-B 3.3125 6.7500 1.9375 1.0000 1.8125 1.2500 0.14 7.0620 0.3125 4.37 3.87 6.46 0.76 49100 0.17 017 98400 - 98788-B 4.0000 7.8740 2.0772 1.0772 1.9375 1.3750 0.14 8.2500 0.3750 5.04 4.76 7.40 0.92 65200 0.05 018 37425 - 37625-B 4.2500 6.2500 0.9063 0.4688 0.8440 0.6250 0.14 6.4336 0.1875 4.80 4.53 6.

15、02 0.54 18900 0.54 019 37431 - 37625-B 4.3125 6.2500 0.9063 0.4688 0.8440 0.6250 0.14 6.4336 0.1875 4.84 4.57 6.02 0.54 18900 0.54 A-A-59652B Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59652B 4 3. SALIENT CHARACTERISTICS 3.1 Dimensions. Bear

16、ing dimensions (and dynamic load ratings, see 3.4) shall conform to the requirements specified in table I for each of the bearing part numbers. The listed dimensions conform to the requirements specified in American Bearing Manufacturers Association (ABMA) Standard 19.2, “Tapered Roller Bearings - R

17、adial Inch Design“. The bearing size shall be specified in the acquisition order (see 7.3(b). For any unlisted bearing size codes, the associated dimensional and dynamic load rating requirements should also be specified in the acquisition order. 3.2 Materials. 3.2.1 Cones (inner rings), cups (outer

18、rings), and rollers. The bearing cones, cups, and rollers shall be made of case carburized or through-hardened steel produced in accordance with the ASTM International (ASTM) A295/A295M, “Standard Specification for High-Carbon Anti-Friction Bearing Steel“, or ASTM A534, “Standard Specification for C

19、arburizing Steels for Anti-Friction Bearings“. The steel shall show a fine fracture grain size in accordance with ASTM E112, “Standard Test Methods for Determining Average Grain Size“. Material hardness shall be no less than Rockwell hardness number of 58 on Rockwell C scale (HRC) and no more than 6

20、4 HRC as defined in ASTM E18, “Standard Test Methods for Rockwell Hardness of Metallic Materials“. 3.2.2 Cage. The bearing cage material shall be impervious to deterioration from any lubricant, preservative, solvent, or other chemical substance expected to contact the bearing during normal use or st

21、orage. Similarly, the material shall not cause any chemical deterioration of any other bearing component. The cages shall be made from carbon steel (one piece stamped). Materials shall operate from -65 to 230 F (-53.9 to 110 C). 3.3 Tolerance class. The tolerance limits for bearings shall conform to

22、 tolerance class 4 as tabulated in ABMA Standard 19.2. Allowable tolerances for bearing components and assembled bearings are listed in tables II through VI. TABLE II. Cone bore tolerance. Cone bore (d) Size range B Tolerance Over Inclusive Plus Minus 0.0000 3.0000 5 0 3.0000 6.0000 10 0 Note: Allow

23、able tolerances are in 0.0001 inch. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59652B 5 TABLE III. Cup diameter tolerance. Cup diameter (D) Size range Tolerance Over Inclusive Plus Minus 0.0000 12.0000 10 0 12.0000 24.0000 20 0 Note: Allowab

24、le tolerances are in 0.0001 inch. TABLE IV. Standout tolerance. Standout (T1) Bore size range Tolerance Over Inclusive Plus Minus 0.0000 4.0000 80 0 4.0000 6.0000 140 100 Note: Allowable tolerances are in 0.0001 inch. TABLE V. Cup flange tolerance. Cup flange outside diameter (D1) Size range Toleran

25、ce Over Inclusive Plus Minus 0.0000 12.0000 20 0 Note: Allowable tolerances are in 0.0001 inch. TABLE VI. Assembled bearing tolerance. Assembled bearing maximum radial runout Cup outside diameter (D) Tolerance Over Inclusive 0.0000 24.0000 20 Note: Allowable tolerances are in 0.0001 inch. 3.4 Dynami

26、c load rating. The bearing dynamic load rating shall conform to the requirements specified in table I for each bearing size code. The listed ratings conform to the requirements specified in ABMA Standard 11, “Load Ratings and Fatigue Life for Roller Bearings“. 3.5 Effective load center. Dimension (a

27、) in figure 1 locates a point on the cone axis, which is the center of pressure of all resisting forces set up by the rollers. All moments should be calculated from this point when determining bearing loading and shaft stresses. A plus value of (a) indicates that the center is outside the cone backf

28、ace. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59652B 6 3.6 Lubrication. The bearings shall be furnished without lubrication. 3.7 Steep angle. A steep angle bearing has a contact angle between 22 and 31 degrees. The contact angle is the ang

29、le between the line of action of the roller load and a plane perpendicular to the bearing axis. 4. REGULATORY REQUIREMENTS 4.1 Recovered materials. The offeror/contractor is encouraged to use recovered materials to the maximum extent practicable, in accordance with paragraph 23.403 of the Federal Ac

30、quisition Regulation (FAR). 4.2 Foreign acquisition restrictions. Unless otherwise indicated in the solicitation and resulting contract, the foreign acquisition restrictions in Section 252.225, Clause 252.225.7016, of the Defense Federal Acquisition Regulation Supplement (DFARS) apply to products de

31、scribed by this CID. 5. PRODUCT CONFORMANCE PROVISIONS 5.1 Product conformance. The products provided shall meet the salient characteristics of this CID, conform to the producers own drawings, specifications, standards, and quality assurance practices, and be the same product offered for sale in the

32、 commercial marketplace. The government reserves the right to require proof of such conformance. 5.2 Market acceptability. The products offered must have been previously sold either to the government or on the commercial market. 6. PACKAGING 6.1 Preservation, packing, and marking. Unless otherwise s

33、pecified in the acquisition order, the bearings shall be preserved, packaged, and marked in accordance with MIL-DTL-197, “Packaging of Bearings, Associated Parts and Subassemblies“ (see 7.3(c). 7. NOTES 7.1 Part or identification number (PIN). The following PIN procedure is for government purposes a

34、nd does not constitute a requirement for the contractor. AA59652 - 003 Example of reference part number Size code (see table I) CID Number AA59652 - 003 indicates: Bearing bore 1.1250 inches; outside diameter 2.8593 inches; width 0.9688 inches. Provided by IHSNot for ResaleNo reproduction or network

35、ing permitted without license from IHS-,-,-A-A-59652B 7 7.2 Sources of documents. 7.2.1 DFARS and FAR. Copies of DFARS and FAR may be obtained from the Superintendent of Documents, P.O. Box 371954, Pittsburgh, PA 15250-7954. Electronic copies of DFARS may be obtained from http:/www.acq.osd.mil/dpap/

36、dars/dfarspgi/current/index.html. Electronic copies of FAR may be obtained from https:/www.acquisition.gov/far/. 7.2.2 Military specifications. Copies of military specifications may be obtained from Standardization Documents Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094. E

37、lectronic copies may be obtained from https:/assist.daps.dla.mil/. 7.2.3 ABMA standards. Copies of ABMA standards may be obtained from the American Bearing Manufacturers Association, 2025 M Street NW, Suite 800, Washington, DC 20036. Electronic copies may be obtained from http:/www.abma-dc.org/. 7.2

38、.4 ASTM standards. Copies of ASTM standards may be obtained from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959. Electronic copies may be obtained from http:/www.astm.org/. 7.3 Ordering data. The acquisition order should specify the following information:

39、a. CID document number, revision, and CID PIN. b. Bearing size (with dimension/load requirements if size is unlisted) (see 3.1). c. Preservation, packaging, and marking requirements (see 6.1). 7.4 Cross-reference information. Table VII relates the original specification slant sheets to the replaceme

40、nt CIDs. TABLE VII. Federal specification to CID cross-reference. FF-B-187B specification sheets Replacement CID numbers ABMA types 1 A-A-59649 TS 2 A-A-59650 TSF 3 A-A-59651 TSS 4 A-A-59652 TSSF 5 A-A-59653 TDI and TDIS 6 A-A-59654 TDO 7 A-A-59655 TDOS 8 A-A-59656 TNA (normal angle) 9 A-A-59657 TNA

41、S (steep angle) 10 A-A-59658 TNASW 11 A-A-59659 TNASWE Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59652B 8 7.5 Subject term (key word) listing. Bore Cone Cup Load Width MILITARY INTERESTS: CIVIL AGENCY COORDINATING ACTIVITY:Custodians: GSA -

42、 FAS Army - AR Navy - MC Air Force - 99 DLA - GS Review Activities: Navy - OS Air Force - 84 Preparing Activity: DLA - GS4 (Project 3110-2011-021) 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 database at https:/assist.daps.dla.mil/. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-