V32 发动机零部件 标准查询与下载

SAE AS5831-2006 非螺纹固定空腔、载流、自粘合挠性组合联轴器外壳尺寸

ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS.Table is about DIMENSIONS.

ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS

HB 7781-2005 航空发动机点火器用贵金属催化网管规范

本规范规定了航空发动机点火器用贵金属催化网管的要求、质量保证规定和交货准备等。 本规范适用于制造航空发动机点火器用贵金属催化网管（以下简称催化网管）。

Specification for precious metals of catalytic netty pipe for aeroengine

NAVY A-A-59780-2005 喷漆应用复组件喷射机

Part or identification number (PIN). The following part or identification numbering procedure is for government purposes and does not constitute a requirement for the contractor.

PLURAL COMPONENT SPRAY EQUIPMENT FOR PAINT APPLICATION

SAE AMS3279B-2005 断续使用至350°F(177℃)的整体油箱和油箱空腔用可喷涂密封化合物

This specification covers one type sprayable fuel resistant polythioether urethane sealing compound supplied as a two-component system.

Sealing Compound, Sprayable, for Integral Fuel Tanks and Fuel Cell Cavities, For Intermittent Use to 350°F (177°C)

SAE AMS3378A-2005 通用室温耐硫化非燃料两部分硅酮密封剂

This specification covers a two-component silicone rubber sealant and compatible primers. Primarily for sealing aircraft structures within a temperature range of -65 degrees to +450 degrees F (-54 degrees to +232 degrees C). The sealant is also compatible with AS1241 phosphate ester fire resistant hydraulic fluids.

Sealant, Silicone, Two-Part, General Purpose Room Temperature Vulcanizing Non-Fuel Resistant

NAVY MIL-DTL-32154-2004 包庇轻度引爆集合组

This specification covers the requirements for the shielded mild detonating cord (SMDC) (part no. 30003-841AS425).

CORD ASSEMBLY, DETONATING, SHIELDED MILD

NAVY MIL-DTL-82889 A-2004 导爆索组(DCA)

This specification covers the requirements for two types of detonating cord assemblies (see 6.1).

DETONATING CORD ASSEMBLY (DCA)

NAVY MIL-D-85866 NOTICE 2-2003 Z-1延迟组成

MIL-D-85866, dated 15 October 1990, is hereby reactivated and may be used for existing or new design acquisition.

DELAY COMPOSITION, Z-1

SAE AS5356A-2002 (R)125 psi柔性燃油管路耦合的一般规格;代替1999年8月24日作废的MIL-C-85061B

This specification covers flexible couplings for joining tubing with MS33660 Type A beaded ends for use in aircraft fuel and vent systems.

(R) Coupling, Fuel Line, Flexible, 125 psi General Specification for Should Be Used Instead of MIL-C-85061B, Which Was Cancelled on 24 August 1999

ARINC 627-2 ITEM 2.0-2002 测试程序结构

Atlas Test Program Structure

Atlas Test Program Structure

HB 7689-2001 飞机发动机空气起动系统进气接头

本标准规定了飞机发动机空气起动系统进气接头的尺寸和飞机进气接头周围应留出的最小安装空间。 　　本标准适用于发动机空气起动系统进气接头的设计。

Aircraft engine air starting system air intake fittings

NAVY MIL-DTL-32018-2001 P/N 837AS118型郁闭周边轻度爆震组

This specification covers the requirements for the manufacture and acceptance of the MG40 Canopy Periphery Mild Detonation Cord (MDC) Assembly, P/N 83AS118 , referred to in this document as cord assembly.

CORD ASSEMBLY, MILD DETONATION, CANOPY PERIPHERY, P/N 837AS118

YB 4105-2000 航空发动机用高温轴承钢

High temperature bearing steel for aircraft engine

SAE AS14169-2000 圆形花键和连接器的细节 发动机驱动的配件 FSC 6115C表1-圆形花键.花键设计数据表2-花键连接器设计数据

CIRCULAR SPLINE AND ADAPTER DETAILS ENGINE DRIVEN ACCESSORIES FSC 6115C

CIRCULAR SPLINE AND ADAPTER DETAILS ENGINE DRIVEN ACCESSORIES FSC 6115C TABLE 1 - CIRCULAR SPLINE SPLINE DESIGN DATA TABLE 2 - SPLINE ADAPTER DESIGN DATA

NAVY MIL-E-50796 NOTICE 2-1999 扩大屏蔽轻度导爆索组

MIL-E-50796, including Amendment 1, dated 14 August 1991, is inactive for new design and is no longer used, except for replacement purposes.

EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY

NAVY MIL-D-85306 A NOTICE 1-1999 T-10延迟组成

MIL-D-85306A, dated 7 November 1991, is inactive for new design and is no longer used, except for replacement purposes.

DELAY COMPOSITION, T-10

SAE ARP1400B-1999 (R)通用航空往复式发动机(活塞式)飞机的润滑油过滤器的推荐性实施规程

This SAE Aerospace Recommended Practice (ARP) establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 345 to 689 kPa (50 to 100 psig). This specification defines uniform parameters for the design, manufacture, and test of filters for general aviation lubricating oil systems for aircraft type piston engines.

(R) Recommended Practices for Lubricating Oil Filters, General Aviation Reciprocating Engine (Piston Type) Aircraft

SAE AIR1160C-1999 飞机发动机,辅助驱动装置和法兰标准

This document defines features that require interface definitions between aircraft engines and accessory drives and flanges and summarizes various aerospace standard dimensional performance data. To provide the means by which both engine manufacturers and accessory manufacturers may save appreciable design and development time by utilizing the collective and coordinated efforts and the past experience of the industry in solving the problems of tolerances and performance capability.

Aircraft Engine and Accessory Drives and Flange Standards

NAVY MIL-B-28658 E NOTICE 1-1998 可移动的预制装配式面板建筑物组件

MIL-B-28658E, dated 25 March 1991, is inactive for new design and is no longer used, except for replacement purposes.

BUILDING COMPONENTS, PANELIZED, PREFABRICATED, READY-CUT, RELOCATABLE

NAVY MIL-S-29409 B NOTICE 1-1998 船破损掩蔽组装

SHELTER ASSEMBLY, KNOCKDOWN

SHELTER ASSEMBLY, KNOCKDOWN