全文阅读 全文下载 章节阅读

基本信息

【范围】

This SAE Aerospace Information Report (AIR) defines helicopter turboshaft engine power assurance theory and methods. Several inflight power assurance example procedures are presented. These procedures vary from a very simple method used on some normal category civil helicopters, to the more complex methods involving trend monitoring and rolling average techniques. The latter method can be used by small operators but is generally better suited to the larger operator with computerized maintenance record capability. 1.1 Purpose: This AIR discusses helicopter turboshaft engine power assurance theory and methods. Several inflight power assurance example procedures are presented. These procedures vary from a very simple method used on some normal category civil helicopters, to the more complex methods involving trend monitoring and rolling average techniques. The latter method can be used by small operators but is generally better suited to the larger operator with computerized maintenance record capability.strRefField

【与前一版的变化】

替代标准

AIR4083

相关标准

·AIR1850A

Twin Engine Helicopter Power Requirements

·AIR1963A

Cockpit Information Required for Helicopter Turbine Engine Operation and Maintenance

·AIR4174

A Guide to Aircraft Power Train Monitoring

·AIR4281

Oil Systems for Helicopter Powerplants

·AIR5277A

(R) Aerospace Fluid Power - Waste Reduction Practices for Used Phosphate Ester Aviation Hydraulic Fluid

·AIR5387

Airport Electrical Power System Harmonics

·AIR5642

The Effect of Installation Power Losses on the Overall Performance of a Helicopter

·AIR5696

Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems

·AIR984C

Air Bleed Objective for Helicopter Turbine Engines

·AMS2355K

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

包含图表

FIGURE 1	FIGURE 2	FIGURE 3
FIGURE 4	FIGURE 5	FIGURE 6
FIGURE A1	In-Flight Engine Pow	Engine Thermal Load
FIGURE C1	FIGURE C2