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ARP1507A
Helicopter Engine/Airframe Interface Document and Checklist
Helicopter Engine/Airframe Interface Document and Checklist
1997-06-01
有效
【范围】 This SAE Aerospace Recommended Practice (ARP) provides a guide for the preparation of a Helicopter Engine/Airframe Interface Document and Checklist. This document and checklist is intended to provide complete relevant information on the characteristics, performance, and engine interfaces. Of most importance is the identification of the data and the location of data to assure that the engine manufacturer and the airframe manufacturer supply information that can be easily located by either manufacturer.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

Gas Turbine Engine Steady State Performance Presentation for Digital Computer Programs
Helicopter Engine - Rotor System Compatibility
Turbine Drive Shaft Connection
Engine Erosion Protection (Helicopter)
Turbine Engine Starting System Design Requirements
Air Bleed Objective for Helicopter Turbine Engines
Cooling of Turbine Engines in Helicopters
Aircraft Accessory Drag Torque During Engine Starts
Aircraft Engine and Accessory Drives and Flange Standards
Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling
Gas Turbine Engine Transient Performance Presentation for Digital Computer Programs
Aircraft
Standard Indoor Method of Collection and Presentation of the Bare Turboshaft Engine Noise Data
Helicopter and V/STOL Aircraft Noise Measurement Problems
Evaluation of Helicopter Turbine Engine Linear Vibration Environment
Gas Turbine Engine Inlet Flow Distortion Guidelines
Electromagnetic Compatibility on Gas Turbine Engines for Aircraft Propulsion
Aircraft Gas Turbine Engine Monitoring System Guide
Defining and Measuring Factors Affecting Helicopter Turbine Engine Power Available

包含图表

Starting and Operati
Externally Applied F
Starting Torque and
Engine Ground Starti
Gearbox Pads and Dri
FIGURE A1
FIGURE A1 (Continued
FIGURE A1 (Continued
FIGURE A1 (Continued
FIGURE A1 (Continued

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