V30 发动机总体 标准查询与下载

HB/Z 132.6-1989 航空发动机制造工艺工作导则 工艺装备的选择、请制、设计工作条例

本标准规定了航空发动机工艺装备的选择、请制、设计程序及管理办法。 　　本标准适用于航空发动机的生产准备过程。

Guidelines for the manufacturing process of aero-engines Selection, manufacture and design of process equipment Regulations

HB 6212-1989 涡喷涡扇发动机飞行台试验性能修正规范

本规范规定了涡喷涡扇发动机在飞行试验台（以下简称飞行台）上测取高度速度特性时净推力及燃油消耗量的修正方法。 　　本规范适用于涡喷涡扇发动机飞行台性能试飞。

Performance correction specification for turbojet turbofan engine flight bench test

HB 6213-1989 涡喷涡扇发动机高空模拟试验性能修正规范

本规范规定了高空模拟试验中发动性能计算与修正方法。 　　本规范适用于涡喷、涡扇发动机在连接式高空舱中的试验。

Performance correction specification for high-altitude simulation test of turbojet turbofan engine

HB/Z 132.3-1989 航空发动机制造工艺工作导则 产品图样工艺性审查条例

本标准规定了航空发动机产品图样资料工艺性审查的内容、程序及方法。 　　本标准适用于航空发动机（含航机陆用）新机研制、改进改型、仿制、测绘等机种。修理机亦可参照执行。

Regulations on Manufacturability Examination of Product Drawings in Guidelines for Manufacturing Processes of Aeroengines

HB/Z 132.4-1989 航空发动机制造工艺工作导则 工艺文件管理工作条例

本标准规定了编写工艺文件的基本要求，毛坯图设计、技术条件、说明书、工艺规程编制和工艺文件会签、审批、归档、发放、超越、更改程序。 　　本标准适用于自行设计的，测绘仿制、改进改型以及航机陆用、水用的发动机零部件、整机装配、试车等的工艺文件管理，国际合作、引进技术以及转包生产的工艺文件管理也可参照使用。

Guidelines for aero-engine manufacturing process Work regulations for process document management

HB/Z 132.7-1989 航空发动机制造工艺工作导则 非标准设备请制、标准设备的选择、调配管理条例

本标准规定了非标准设备的分类、请制、设计、制造验收等程序。还规定了标准设备的选择、调配管理办法。 　　本标准适用于工艺技术部门对各类非标准设备、标准设备和仪器的管理。

Aero-engine manufacturing process work guidelines Non-standard equipment request, standard equipment selection, deployment management regulations

ARMY MIL-F-60020 VALID NOTICE 1-1988 组合式M10A2地雷引信零件

MIL-F-60020(AR), dated 31 January 1964, has been reviewed and detemrined to be valid for use in acquisition.

FUZE, MINE, COMBINATION M10A2, PARTS FOR

ARMY MIL-L-63953-1988 锁组合的装配

This specification covers one type of cömbination lock, designated Lock, Combination, Assembly, which is used for multipurpose applications in the WADS program.

LOCK, COMBINATION, ASSEMBLY

ARMY MIL-F-45060 D VALID NOTICE 1-1987 M605组合式地雷引信零件

MILE-45060D(AR), dated 24 September 1975, h w been reviewed and determined-to be valid for use in acquisition.

FUZE, MINE, COMBINATION M605, PARTS FOR

SAE AIR4003-1987 飞机发动机包容性报告

To gather and analyze service data on aircraft propulsion turbine engine rotating part non-containment failures on record, assess the resulting aircraft damage, and determine the rate of past occurrences based on these data. In addition, to classify incidents by cause and consequence, to identify areas of greatest concern, and to recommend areas for greatest potential improvement. While the previous SAE Committee report, AIR 1537, focused solely on fixed wing commercial engine experience, the current Committee decided that the scope should be expanded to collect the data relating to helicopter and general aviation operations. The inclusion of helicopter experience was prompted by the FAA request to anticipate the projected substantial increase in commercial use of helicopters within the next decade. For completeness, general aviation experience, including commuter airlines, was considered significant enough to include in the current committees activities. At the direction of the Aerospace Council, all three classes of engines have been treated in a single report. It is expected that the data, conclusions and recommendations of this report will be accepted as a standard reference by anyone dealing with turbine engine rotor non-containment

Report on Aircraft Engine Containment

HB 5946-1986 飞机发动机用空气涡轮起动机通用技术条件

本标准规定了飞机发动机用空气涡轮起动机的一般要求。 　　本标准适用于新产品的研制及其批生。

General specifications for air turbine starters for aircraft engines

SAE AIR1703-1985 飞行中推力测定

This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1); Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.

In-Flight Thrust Determination

KS W 4041-1984 航空航天磁探伤检测方法

이 규격은 항공 우주용 부품 및 재료의 자기 탐상 검사의 실시에 관하여 일반 요구 사항과

Inspection Process of Magnetic for Aerospace Use

DIN ISO 482:1983 航空和航天.推进装置和元件.编号和旋转方向描述方法

Aircraft; propulsion units and components; methods of numbering and describing directions of rotation

HB 5799-1982 航空发动机改型为非航空用产品型号命名和设计图样技术文件编号制度

本标准适用于航空发动机改型为非航空用的产品。

Retrofit of aero-engines to non-aviation products Model nomenclature and design drawing technical document numbering system

NF L85-100:1980 推进装置及元件.旋转方向的编号和阐述方法

Propulsion units and components. Methods of numbering and describing direction of rotation.

HB/Z 5130-1979 航空发动机干燥空气封存工艺

本工艺适用于各型航空发动机的干燥空气封存，是编制封存工艺说明书或操作规程的指导性技术文件。

Aeroengine dry air storage technology

DLA MS51524 REV A-1979 37度扩口式组合三通管接头

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

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

DLA MS51523 REV A-1979 37度扩口式组合直角三通管接头

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

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

KS W 4021-1977 航空器发动机气缸编号和旋转方向

이 규격은 항공기용 피스턴 엔진의 실린더 번호의 호칭방법 및 회전방향의 정의에 대하여 규정

Aircraft engine cylinder number and direction of rotation