DLA MIL-B-18 6 E-2011 BATTERY DRY BA-26.pdf

上传人:rimleave225 文档编号:689518 上传时间:2018-12-30 格式:PDF 页数:4 大小:47.15KB
下载 相关 举报
DLA MIL-B-18 6 E-2011 BATTERY DRY BA-26.pdf_第1页
第1页 / 共4页
DLA MIL-B-18 6 E-2011 BATTERY DRY BA-26.pdf_第2页
第2页 / 共4页
DLA MIL-B-18 6 E-2011 BATTERY DRY BA-26.pdf_第3页
第3页 / 共4页
DLA MIL-B-18 6 E-2011 BATTERY DRY BA-26.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 MIL-B-18/6E 1 March 2011 SUPERSEDING MIL-B-18/6D 21 May 1985 MILITARY SPECIFICATION SHEET BATTERY, DRY, BA-26 This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product described herein shall consist of this specif

2、ication sheet and MIL-B-18. FIGURE 1. Interface and physical dimensions. AMSC N/A FSC 6135 INACTIVE FOR NEW DESIGN AFTER 6 JULY 1998 INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-B-18/6E 2 Ltr Inches mm Min Max Min Max A .938 1.188 2

3、3.80 30.18 B 3.938 4.188 100.03 106.38 C 6.938 7.188 176.23 182.58 D 8.000 8.250 203.20 209.55 E 4.250 4.500 107.95 114.30 F .875 1.125 22.23 28.58 G - 7.938 - 201.63 H 7.125 7.375 180.98 187.33 NOTES: 1. All dimensions shown on figure 1 are in inches. 2. Metric equivalents specified in the table ar

4、e for general information only. 3. Voltage and polarity markings may be placed either on the top or front face of the battery 4. Unless otherwise specified, tolerance is .125 inch. FIGURE 1. Interface and physical dimensions - Continued. REQUIREMENTS: Interface and physical dimensions: See figure 1.

5、 Nominal voltage: 45 volts. Tapped at: 22.5 volts. Usual number and type of cells: 30 “F“ cells. Usual cell connection: Series. Terminals: Spring clip. Weight (maximum): 13 pounds, 12 ounces. Capacity tests: When the battery is tested in accordance with the methods of examination and test of this sp

6、ecification, the minimum capacity-test requirements shall be not less than the minimum time specified for SLD or SLT. First article inspection: Visual and mechanical (external). Battery voltage. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-B-1

7、8/6E 3 Vibration test. Mechanical-shock test in accordance with MIL-STD-202, method 213, test condition I. Insulation resistance test in accordance with MIL-STD-202, method 302, test condition letter B, tolerance 20 volts. Capacity, D (without storage). Jacket integrity test. Conformance inspection.

8、 Visual and mechanical (external) Battery voltage. Insulation-resistance test in accordance with MIL-STD-202, method 302, test condition letter B, tolerance 20 volts. Vibration test. Mechanical-shock test in accordance with MIL-STD-202, method 213, test condition I. Jacket integrity test. Electrode

9、leakage. Capacity, D and T. Methods of examination and test: Capacity tests: See requirements for capacity specified herein. Storage: Test Period D 12 months T 90 days Discharge: The battery shall be discharged through 2,000 ohms continuously to a test-end voltage of 34.0 volts. Closed circuit volta

10、ge: Use TS-183( )/U test per special marking or, with minimum permissible voltage as specified for TS-183 ( )/U, use a load resistant value of 1,923 ohms. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-B-18/6E 4 Special marking on each unit pack

11、age: Part or Identifying Number (PIN): BA-26, see 1.2 of MIL-B-18. Referenced documents. In addition to MIL-B-18, this document references MIL-STD-202. The margins of this specification are marked with vertical lines to indicate where changes from the previous issue were made. This was done as a con

12、venience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous issue

13、 Custodians: Preparing activity: Army - CR DLA - CC Navy - SH Air Force - 99 (Project 6135-2010-005) DLA - CC Review activities: Army - MI Navy - MC NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can chang

14、e, you should verify the currency of the information above using the ASSIST Online database at https:/assist.daps.dla.mil/. TO TEST THIS BATTERY WITH TS-183 ( )/U: USE JACK NO MINIMUM PERMISSIBLE VOLTAGE 16 42.0 Unless expressly authorized, this test information shall apply to Army and Air Force applications only. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4186-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Cross Unions Edition P 1《航空航天系列.导管接头8°30′钛合金球座四通活管接.P1版》.pdf AECMA PREN 4186-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Cross Unions Edition P 1《航空航天系列.导管接头8°30′钛合金球座四通活管接.P1版》.pdf
  • AECMA PREN 4187-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Elbows 90 Degrees Bulkhead Long Edition P 1《航空航天系列.钛合金管连接件8°30′闷头90°弯头》.pdf AECMA PREN 4187-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Elbows 90 Degrees Bulkhead Long Edition P 1《航空航天系列.钛合金管连接件8°30′闷头90°弯头》.pdf
  • AECMA PREN 4188-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Elbows 90 Degrees Bulkhead Long Welded Edition P 1《航空航天系列.钛合金管连接件8°30′闷头、焊接端头的90°弯头》.pdf AECMA PREN 4188-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Elbows 90 Degrees Bulkhead Long Welded Edition P 1《航空航天系列.钛合金管连接件8°30′闷头、焊接端头的90°弯头》.pdf
  • AECMA PREN 4189-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Bulkhead Branch Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管闷头分支》.pdf AECMA PREN 4189-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Bulkhead Branch Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管闷头分支》.pdf
  • AECMA PREN 4190-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced with Swivel Nut on Run Edition P 1《航空航天系列.钛合金管连接件8°30′带止推金属丝螺母的三通管分支》.pdf AECMA PREN 4190-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced with Swivel Nut on Run Edition P 1《航空航天系列.钛合金管连接件8°30′带止推金属丝螺母的三通管分支》.pdf
  • AECMA PREN 4191-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Branch Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf AECMA PREN 4191-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Branch Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf
  • AECMA PREN 4192-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Branch Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf AECMA PREN 4192-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Branch Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf
  • AECMA PREN 4193-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf AECMA PREN 4193-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Long Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf
  • AECMA PREN 4194-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf AECMA PREN 4194-1994 Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Tees Reduced Bulkhead Edition P 1《航空航天系列.钛合金管连接件8°30′三通管弯头分支》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1