V39 燃油系统及其附件 标准查询与下载

NAVY MIL-P-17945 A NOTICE 1-1991 海军舷侧综合使用外围型的离心泵

dated 13 October 1977, has been reviewed and be inactive for new design.

PUMPS, CENTRIFUGAL, PERIPHERAL TYPE, MISCELLANEOUS NAVAL SHIPBOARD USE

NAVY MIL-F-21173 C-1991 美国海军陆战队司令官个人人造纤维旗帜

FLAG, INDIVIDUAL: RAYON, COMMANDANT, USMC

FLAG, INDIVIDUAL: RAYON, COMMANDANT, USMC

NAVY MIL-P-24765-1991 (海军舷侧)不间断电力供应

This specification covers the detail requirements for a 60 hertz (Hz) static uninterruptible power supply (UPS) for non nuclear Navalshipboarduse. Only one classification of power supply is covered by this specification

POWER SUPPLY, UNINTERRUPTIBLE, STATIC (NAVAL SHIPBOARD)

NAVY MIL-T-960 E (3)-1991 海军舰间歇放电和连续流蒸汽陷阱

This amendment forms a part of MILT-%OE(SHIPS), dated 21 June 1963,and is approved for use by Naval Sea Systems Command, Department of the　Navy and is available for use by all departments and agencies of the　Department of Defens

TRAPS, STEAM, INTERMITTENT DISCHARGE AND CONTINUOUS FLOW, NAVAL SHIPBOARD

HB 6484-1990 飞机燃油系统原理图推荐符号

本标准规定了飞机燃油系统原理图中常用的符号。 　　本标准适用于飞机燃油系统原理图的绘制，在飞机燃油系统原理图中，用本标准中规定的符号代表各种相应的燃油系统附件。

Schematic Recommended Symbols for Aircraft Fuel System

HB 6451-1990 飞机燃油系统供输油附件压力术语

本标准规定了燃油系统供输油附件的压力术语。 　　本标准适用于供输油分系统燃油附件。

Aircraft fuel system delivery accessories pressure terminology

HB/Z 176-1990 航空发动机燃油与控制系统 回油活门设计指南

本标准规定了航空发动机燃油与控制系统中回油活门组件的设计内容、技术性能、计算公式和特性，以及试验等方面的要求。 　　本标准适用于航空发动机燃油与控制系统中的回油活门组件，可作为设计时的依据。其它系统中的回油活门组件也可参照执行。

Design guidelines for oil return valves of aeroengine fuel and control systems

SAE AIR1168/3-1990 气动热力系统工程和设计

This section presents methods and examples of computing the steady-state heating and cooling loads of aircraft compartments. In a steady-state process the flows of heat throughout the system are stabilized and thus do not change with time. In an aircraft compartment, several elements compose the steady-state air conditioning load. Transfer of heat occurs between these sources and sinks by the combined processes of convection, radiation, and conduction in the following manner: 1) convection between the boundary layer and the outer airplane skin; 2) radiation between the external skill and the external environment; 3) solar radiation through transparent areas directly on flight personnel and equipment and on the cabin interior surfaces; 4) conduction through the cabin walls and structural members; 5) convection between the interior cabin surface and the cabin air; 6) convection between cabin air and flight personnel or equipment; and 7) convection and radiation from internal sources of heat such as electrical equipment.

Aerothermodynamic Systems Engineering and Design

NAVY MIL-STD-1322-68-1990 MK 19 MOD 15型引爆装置,用于国内和海外输送的集装物资,置于MK 4 MOD 2型集装箱内

C ONTAINERL OADIN G AND CARL OADING MILITARY TDA SYSCOM STANDARDS, REFER TO INDEX TO STANDARDS,

UNIT LOAD FOR DOMESTIC AND OVERSEAS SHIPMENT EXPLODER MECHANISM, MK 19 MOD 15 IN CONTAINER, MK 4 MOD 2

ARMY MIL-I-48086 (4)-1990 M36A2型装药推进剂的推进增量(由推进剂M8制作)

This Amendment forms a part of Military Specification MIL-1-48086(M U)dated 1 September 1972, and is approved for use by the U.S. Army Armament,Munitions and Chemical Command, and is available for use by all Departments and Agencies of the Department of Defense.

INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A2 (MADE FROM PROPELLANT M8)

NAVY MIL-V-2961 D-1990 用于天然气服务的球型减压阀[代替使用: 海军 MIL-V-002961 A]

This specification covers self-contained globe (in-line and offset) pressure reducing valves for gas (air or nitrogen) service intended for shipboard and marine environment use (see 6.1) Guidance in the selection and installation of these valves is contained in M“[L-HDBK-227.

VALVES, GLOBE, PRESSURE REDUCING, GAS SERVICE [Use In Lieu Of: NAVY MIL-V-002961 A]

NAVY MIL-M-29417 (1)-1990 燃油泵模块

This amendment forms a part of MIL-M-29417 (MC) dated 30 November 1984, and is apppoved for use bv the U. S. Marine Corps,Department of the Navy aria is available for use by all Departments and Agencies of the Department of Defense.

MODULE, FUEL PUMP (SIXCON)

NAVY MIL-P-85548 B-1990 N-60计算机辅助扫描技术合成推进剂

PROPELLANT, COMPOSITE, CAST, N-60

PROPELLANT, COMPOSITE, CAST, N-60

NAVY MIL-I-87070 A-1990 海军肩章(装饰)和官员徽章级别

This specification covers the requirements €or soft shoulder marks for Navy rank officers with embroidered insignia.

INSIGNIA, RANK, OFFICERS, SHOULDER MARK, NAVY (EMBROIDERED)

ISO 7314:1989 航空航天器.燃油系统.软管组件、金属管

Aerospace; fluid systems; hose assembly metal

NAVY RR-S-331 D-1989 用于采木桩的鞋[使用代替: 海军 RR-S-00331 A]

This specification covers point-type and boot-type shoes for timber piles

SHOES: FOR WOOD PILES [Use In Lieu Of: NAVY RR-S-00331 A]

NAVY A-A-50433-1989 抗海水冲刷油脂

AST14 Standards are available Philadelphia, Pa. 19103. 2. It shall be incumbent on tLe any grease supplied for this of NAVSSA S9520-AB-AT14-010 /(U) and NiVSSA T6350-~-HBl?-010. Points of contact at Naval Sea Systems Command are NAVSRA 05M32 (ph 202-692-0144), NAVSEA PMS 390 (ph 202-746-3323), and NAVSEA 56Y14 (ph 202-692-5473). from ASTM, 1916 Race Street, procuring agency to insure that CID aoIuDlies with the requirements

GREASE, SEA WATER WASH RESISTANT

HB/Z 151-1989 航空发动机燃油与控制系统柱塞式燃油泵设计指南

本标准规定了发动机燃油与控制系统柱塞式燃油泵的设计方法、计算公式、参数选择及试验内容等。 　　本标准适用于航空发动机控制系统主燃油泵和加力燃油泵的设计。并以具有流体静压支承柱塞的变量泵作为设计对象。

Piston fuel pump design guidelines for aeroengine fuel and control systems

HB/Z 153-1989 航空发动机燃油与控制系统圆截面定值节流嘴设计指南

本标准规定了发动机燃油与控制系统圆截面定值节流嘴（以下简称节流嘴）设计的方法，参数的选择及试验内容。 　　本标准适用于发动机燃油与控制系统的设计，液压控制系统亦可参照使用。

Design guidelines for circular section constant value throttle nozzles of aero-engine fuel and control systems

HB/Z 152-1989 航空发动机燃油与控制系统喷嘴 挡板液压元件设计指南

本标准规定了工作介质为燃油的喷嘴-挡板液压元件的设计、计算、试验和确定结构参数的原则。 　　本标准适用于航空发动机燃油与控制系统中喷嘴-挡板液压元件的设计工作。

Design guidelines for nozzle baffle hydraulic components of aero-engine fuel and control systems