用户名: 密码: 登 录   个人中心   系统维护   用户注册  联系我们
当前位置 >首页 > 标准信息

全文阅读 全文下载 章节阅读

基本信息

ARP699E
High Temperature Pneumatic Duct Systems for Aircraft
High Temperature Pneumatic Duct Systems for Aircraft
2011-06-01
有效
【范围】 This Recommended Practice is intended to outline the design, installation, testing, and field maintenance criteria for a high temperature metal pneumatic duct system, for use as a guide in the aircraft industry. These recommendations are to be considered as currently applicable and necessarily subject to revision from time to time, as a result of the rapid development of the industry.strRefField
【与前一版的变化】

替代标准

相关标准

A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems
BAROMETRY FOR ALTIMETER CALIBRATION
Aircraft Accessory Drag Torque During Engine Starts
Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays
Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights
Electromagnetic Interference on Aircraft From Jet Engine Charging
Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling
Construction and Calibration of Parallel Plate Transmission Line for Electromagnetic Interference Susceptibility Testing
Installation of Liquid Oxygen Systems in Civil Aircraft
Anti Blow-By Design Practice for Cap Seals

包含图表

Autogenous Ignition
Autogenous Ignition
Schematic - Basic Co
TABLE 1
TABLE 1 (Continued)
TABLE 2
TABLE 2 (Continued)
FIGURE 4
FIGURE 5
FIGURE 6
FIGURE 7
FIGURE 8
FIGURE 9
TABLE 3
TABLE 4
FIGURE 10
formula 1
formula 2
FIGURE 11
FIGURE 12
Typical Duct Expansi
Ball and Socket Tie
Ball Joint
Pressure Compensatin
Pressure Compensatin
Seal Type Pressure C
Common Type Bends
FIGURE 20
Rotary Joint Install
Rotary Joint Assembl
FIGURE 24
FIGURE 25
formula 3
FIGURE 26
formula 4
FIGURE 27
formula 5
FIGURE 28
formula 6
FIGURE 29
FIGURE 30
formula 7
FIGURE 31
formula 8
FIGURE 32
FIGURE 33
formula 9
FIGURE 34
FIGURE 35
FIGURE 36
FIGURE 37
FIGURE 38
TABLE 5
TABLE 6
TABLE 7
TABLE 8
Endurance Test Set-U

标准反馈


  • 问题类型:
    反    馈: