V30 发动机总体 标准查询与下载

DLA MS51524 REV A NOTICE 1-1999 37度扩口式组合三通管接头

This notice should be filed in front of MS51524A, dated 17 January 1979.

TEE, TUBE TO SWIVEL, SWIVEL ON BRANCH, 37 DEGREE FLARED [Refer To: SAE J514, SAE J514, SAE J514, SAE J514, SAE J514]

AECMA PREN 4301-1998 航空系列 发动机打印标号方法工程要求.P1版

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members.

Aerospace Series Identification Marking Methods for Engine Items Engineering Requirements Edition P 1

AECMA PREN 4300-1998 航空系列 发动机设计打印标号标准.P1版

This "Aerospace Series'' Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Identification Marking of Engine Items Design Standard Edition P 1

HB 7613-1998 航空涡轮发动机推重比和功重比确定方法

本标准规定了航空涡轮发动机推重比和功重比的确定方法。 　　本标准适用于航空涡轮发动机推重比和功重比的计算。活塞发动机可参考使用。

Determination method of thrust-to-weight ratio and power-to-weight ratio of aero turbine engine

SAE AIR1813A-1998 气体涡轮发动机试验室噪音抑制Coanda/折射概念

Document provides information on how military/commercial/gas turbine engine test cell/system users may benefit from this unique Coanda//refraction concept. The information contains several factors which are considered essential for understanding the practical technical aspects of the concept. These are: a. operation need; b. concept definition; c. developmental program; and d. program results. To present an advanced technology in suppression of gas turbine engine exhaust noise in ground run-up test cells/systems. The discussion herein is limited to turbojet and turbofan type engines, although the concept is equally applicable to turboshaft and turboprop types. To explain specific applications of this technique in various types of test cells.

The Coanda/Refraction Concept for Gas Turbine Engine Test Cell Noise Suppression

ISO 13592:1998 小艇 汽油机回火火焰控制

This International Standard specifies the minimum requirements for construction and testing of engines and devices to prevent the propagation of backfire flames from permanently installed inboard petrol engines to the surrounding atmosphere in small craft of length of the hull up to and including 24 m.

Small craft - Backfire flame control for petrol engines

ARMY MIL-S-20706 A NOTICE 1-1998 悬挂式推土机和背后犁土碎土机组合

This notice should be filed in front of MIL-S-20706A, dated 21 April 1970.MIL-S-20706A is inactive for new design and is no longer used, except for replacement purposes.

SCARIFIER ASSEMBLIES, BACK-RIP, EARTH, DOZER MOUNTED

ARMY MIL-S-52124 B NOTICE 1-1998 功率为75吨每小时的电动的组合屏蔽装置

This notice should be filed in fiont of MILS-S2124B(ME), dated 18 July 1968.

SCREENING UNIT, AGGREGATE, ELECTRIC-MOTOR-DRIVEN, 75-TON-PER-HOUR CAPACITY

HB 7497-1997 航空涡轮发动机重量的确定

本标准规定了航空涡轮发动机重量定义、净重量的确定准则及其构成项目。 　　本标准适用于航空涡轮发动机在净重量方面与飞机的分界，适用于发动机重量的估算、计算与称重。

Determination of Aero Turbine Engine Weight

HB 7508-1997 涡轮涡扇发动机露天基准试车台 基准试车要求

本标准规定了涡喷、涡扇发动机在露天基准试车台上进行基准试车的各种要求。 　　本标准适用于涡喷、涡扇发动机在露天基准试车台上的基准试车。

Requirements for turbofan engine open-air benchmark test bench benchmark test

HB 7507-1997 涡喷涡扇发动机飞行试验台试验要求

本标准规定了涡喷、涡扇发动机在飞行试验台（亦称飞行实验室）上进行飞行的要求和内容。 　　本标准适用于新研制（包括测绘仿制）的和改进、改型的涡喷、涡扇发动机在飞行试验台上的调整试飞、专项试飞和预先研究试飞。

Test requirements for turbojet turbofan engine flying test bench

SAE AIR1850A-1997 双发动机直升机的动力要求

This SAE Aerospace Information Report (AIR) defines the power spectrum during normal and emergency operations of a twin engine helicopter and thereby postulates suitable power plant rating structures. The document does not address the power requirements for single engine helicopters or those with more than two engines.

Twin Engine Helicopter Power Requirements

SAE AIR4083A-1997 直升机功率保证

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. 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.

Helicopter Power Assurance

ARMY MIL-F-20481 B NOTICE 4-1997 M6A1和M10A1组合式地雷引信零件

This notice should be filed in fiont of MIL-M-l2696(AR) dated 13 May 1953

FUZE, MINE, COMBINATION M6A1 AND M10A1, PARTS FOR

KS W 4616-1996 航空器涡轮轴发动机和涡轮螺旋桨发动机通则

이 규격은 항공 터보샤프트 발동기 및 터보프롭 발동기에 대한 성능, 작동 특성, 설계 특징

General specification of turboshaft and turboprop engines for aircraft

KS W 4611-1996 航空器涡轮喷气发动机和涡轮风扇发动机通则

이 규격은 항공 터보제트 발동기 및 터보팬 발동기에 대한 성능, 작동 특성, 설계 특징,

General specification of turbojet engines and turbofan engines for aircraft

KS W 4619-1996 航空器缓冲装置

이 규격은 공기-유압식 완충 착륙 장치에 대한 요구 사항에 대하여 규정한다.

Landing gear, aircraft shock absorber(Air-oil type)

HB 7295-1996 飞机强度和刚度地面试验系统校准方法和要求

本标准规定了飞机及其构件强度和刚度试验项目中，疲劳和静强度（含损伤容限与刚度）试验系统校准的方法和要求。 　　本标准适用于各种军用飞机和直升机，也适用于各种民用飞机。本标准可作为试验委托方（以下简称委托方）拟订试验任务书或与试验承制方（以下简称承制方）签订合同的依据之一，亦可由委托方和承制方协商采用。

Aircraft Strength and Stiffness Ground Test System Calibration Method and Requirements

HB 7290-1996 航空活塞发动机通用规范

General specification for aviation piston engines

HB 7284-1996 民用航空器发动机驱动的直流发电机和起动发电机及发电机控制器最低性能要求

本标准规定了发动机驱动的直流发电机和起动发电机及其配套的发电机控制器（以下简称控制器）的最低性能要求。 　　本标准适用于民用航空器直流电源系统中的发电机和起动发电机及其配套的控制器。

Minimum performance requirements for DC generators and starter generators and generator controllers driven by civil aircraft engines