NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf

上传人:deputyduring120 文档编号:980326 上传时间:2019-03-12 格式:PDF 页数:6 大小:258.57KB
下载 相关 举报
NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf_第1页
第1页 / 共6页
NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf_第2页
第2页 / 共6页
NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf_第3页
第3页 / 共6页
NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf_第4页
第4页 / 共6页
NAVY MIL-M-22673-1960 MOUNTING PLENUMS MT-2243( ) ASQ-56 AND MT-3946( ) ASQ-56B《MT-2243( ) ASQ-56 和 MT-3946( ) ASQ-56B高压间装配》.pdf_第5页
第5页 / 共6页
点击查看更多>>
资源描述

1、MIL-M-22673 53 M 7797906 0103687 1 c, - CI-., M I L- M -2 2 6 7 3 C W LP I NOVEMBER 1960 MILITARY SPECIFICATION MOUNTING-PLENUM MT-2243(*)/ASQ- 56 This specification has been approved by the Bureau of Naval Weapons, Department of the Navy. 1. SCOPE 1.1 Scope - This specification covers the requireme

2、nts for the Mounting- Plenum MT-2243/A-6. When installed as part of Integrated Electronic Central AN/ASQ-56 this equipment shail provide the following: (i) Equipment mounting facilities (2) Vibration isolation (3) Facilities fgr electrical connections I .I d .Y * 1. 2 b (4) Distribution of cooling a

3、irto equipments Associated Equipments - The equipment shall be capable of operating . i with the follow-ig associated equipment which is not to be supplied as pal.t of this equipment. t - Item Type Designation Receiver-Transmitter, Radio RT- 54i/s Decoder, Puise KY- 309/ASQ Coder-Receiver- Transmitt

4、er KY- 308/ASQ Amplifier- Power Supply-Receiver AM- 231O/ASQ Receiver- Transmitter. Radio RT-542/ASQ 2. APPLICABLE DOCUMENTS 2.1 General - The following documents of the issue in effect on the date of invitation for bids form a part of this specification to the extent specified herein: SPECIFICATION

5、S Military MIL-C-172 MIL- T- 5422 Cases; Bases; Mounting; and Mounts, Vibration (for use with Electronic Equipment in Aircraft) Testing; Environmental, Aircraft Electronic Equipment Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-22673 (WEP) MI

6、L-1-22668 Integrated Electronic Centrals ANLAS number 8 hardware, 20 inch pounds. 1.2 shaii be silk screened on the bottom of the mounting-plenum as far forward as possible, and such that the Lettering is upright when the bottom of the mounting-plenum is viewed with the forward channel at the top. 3

7、3.1.12 Silk Screening - Nomenclature of associated equipment listed in paragraph 3 - o Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-, MIL-T-22673 NEP) v) W o r r w O 3 !I A Q I Q W J O O m 0.1 o1 I 3 4 5 6 789100 2 3 4 5 678910 2 FREQUENCY, cps 2

8、00 Figure 1 4 k Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-22673 53 m 7977706 0103691 3 m 4 MIL-T-22673 (WEP) 3.3.1.13 Specification MIL- C-172. Electrical Bonding - Electrical bonding shall be in accordance with 3.3.1.14 Vibration Isolato

9、rs - Mounting-Plenum MT-2243/ASQ-56 consists of a plenum and the following four isolators: Barry Controls Part Number 6375-2 Barry Controls Part Number 6375-1 Barry Controls Part Number 6376 Barry Controls Part Number 6777 (or approved equivalents) 4. QUALITY ASSURANCE PROVISIONS Right Front Assembl

10、y Left Front Assembly Right Rear Assembly Left Rear Assembly 4.1 General - Equipments shall be subjected to the test requirements of Specification MIL-Iwto determine compliance with all the applicable requirements. 5. PREPARATION FOR DELIVERY 5.1 General - All major units and parts of the equipment

11、shall be preserved, packaged, packed and-marlied for the level of shipment specified in the contract or order in accordance with Specification MIL-1-22668. 6. NOTES 6.1 Precedence - When the requirements of the contract, this specification, applicable subsidiary specifications are in conflict, the f

12、ollowing precedence shall apply: I 0) Contract - The contract shall have precedence over any specification. (2) System Specification - Integrated Electronic Centrals AN/ASQ- 56, AN/ASQ-57, AN/ASQ-58 Specification MIL-1-22668 shall have precedence over this specification, (3) This Specification - Thi

13、s specification shall have precedence over all applicable subsidiary specifications, Any deviation from this spec- ification, or from subsidiary specification where applicable, shall be approved in writing by the procuring activity, (4) Referenced Specifications - Any referenced specification shall

14、have precedence over all applicable specifications referenced therein. All referenced specifications shall apply to the extent specified. The parentheses ( * ), when used in the type designation, shall be replaced 6.2 by either a number or letter furnished by the procuring activity upon application

15、by the con- tractor for assignment of nomenclature in accordance with 3.2.10 of MIL-1-22668. The complete type number shall be used on nameplates, shipping records and instruction books, as applicable. 5 7. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS

16、1- - NIL-N-22673 53 = 9999906 0103692 5 MIL- T-22673(WEP) NOTICE - When government drawings, specifications, or other data are used for any purpose other than in connection with a definitely related government procurement operation, the United States Government thereby incurs no responsibility

17、nor any obligation whatsoever; and the fact that the government may have formulated, furnished or in any way supplied the said drawing, specifications or other data is not to be regarded by implication or otherwise as in any manner licensing the holder or any other person or corporation or conveying any rights or permission to manufacture, use or sell any patented invention that may in any way be related thereto. 6 Y o 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
  • NASA NACA-TR-1109-1952 Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities《在超音速下 钝后缘机翼基准压力的实验性研究》.pdf NASA NACA-TR-1109-1952 Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities《在超音速下 钝后缘机翼基准压力的实验性研究》.pdf
  • NASA NACA-TR-1130-1953 Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw《频率对垂直尾翼对偏航中飞机模型的振荡自由空气动力阻尼促进的一.pdf NASA NACA-TR-1130-1953 Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw《频率对垂直尾翼对偏航中飞机模型的振荡自由空气动力阻尼促进的一.pdf
  • NASA NACA-TR-1135-1953 Equations tables and charts for compressible flow《可压缩流的方程式 表格和图表》.pdf NASA NACA-TR-1135-1953 Equations tables and charts for compressible flow《可压缩流的方程式 表格和图表》.pdf
  • NASA NACA-TR-1146-1953 Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps《带有普通前缘和普通后缘襟翼的对称圆弧机翼上空气动力和荷载》.pdf NASA NACA-TR-1146-1953 Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps《带有普通前缘和普通后缘襟翼的对称圆弧机翼上空气动力和荷载》.pdf
  • NASA NACA-TR-1150-1953 Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow《风洞壁对二维亚音速可压缩流的振荡空气力量影响的考虑》.pdf NASA NACA-TR-1150-1953 Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow《风洞壁对二维亚音速可压缩流的振荡空气力量影响的考虑》.pdf
  • NASA NACA-TR-116-1923 Applications of modern hydrodynamics to aeronautics《现代化流体力学对航空学的应用》.pdf NASA NACA-TR-116-1923 Applications of modern hydrodynamics to aeronautics《现代化流体力学对航空学的应用》.pdf
  • NASA NACA-TR-1169-1954 Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data《测定瞬时飞行数据的飞机纵向稳定性导数的矩阵方法》.pdf NASA NACA-TR-1169-1954 Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data《测定瞬时飞行数据的飞机纵向稳定性导数的矩阵方法》.pdf
  • NASA NACA-TR-1170-1954 Behavior of materials under conditions of thermal stress《热应力条件下材料的表现》.pdf NASA NACA-TR-1170-1954 Behavior of materials under conditions of thermal stress《热应力条件下材料的表现》.pdf
  • NASA NACA-TR-1171-1954 Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip《水平尾翼翼展和垂直位置对侧滑中非掠尾翼组件空气动力特性的影.pdf NASA NACA-TR-1171-1954 Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip《水平尾翼翼展和垂直位置对侧滑中非掠尾翼组件空气动力特性的影.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