V22 机械配件、构件 标准查询与下载

HB 2-23-2004 挤压型材合页片

本标准规定了挤压型材合页片的结构、尺寸要求。 本标准适用于盖板、舱门和挡板铵链用合页片。

Extruding shapes hinge

HB 3-22-2004 焊接卡箍

Clamp weleded

BS ISO 15864:2004 航天系统.航空器、子系统和部件的一般试验方法

This International Standard provides the baseline standard on the subject of testing at the system, subsystem and unit levels for applicable unmanned spacecraft programmes. It also provides the requirements for documentation associated with testing activities. The acceptance criteria, specifications or procedures, and other detail test requirements applicable to a particular programme are defined in the applicable technical specifications and statement of work. When requirements have to be verified by measuring product performance and function under various simulated environments, the method is referred to as "Test". The requirements of this International Standard may be tailored for each specific space programme application.

Space systems - General test methods for space craft, subsystems and units

DLA MS90402 ADMIN NOTICE 1-2004 紧箍螺杆

The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at www.dodssp.daps.mil.

SCREW, CAPTIVE

SAE MA2096C-2004 24度锥角沉头配件端设计标准(米制)

(R) FITTING END, 24℃, BULKHEAD, DESIGN STANDARD, METRIC FSC 4730

(R) FITTING END, 24℃, BULKHEAD, DESIGN STANDARD, METRIC FSC 4730

SAE AS8879D-2004 螺纹.增加内径的尺寸可控的圆角半径的UNJ型材

This SAE Aerospace Standard (AS) specifies the characteristics of screw threads - UNJ profile inch series, including a mandatory controlled radius as specified in Table 1 at the root of the external thread. The minor diameter of both external and internal threads provides a basic thread height of .5625H to accommodate the external thread maximum root radius. The following detailed design requirements are included: a. Screw threads - UNJ basic profile and design profiles. b. Standard series of diameter-pitch combinations for nominal thread diameters from 0.060 to 6.000 inches. c. Standard thread classes and form tolerances. d. Formulae for thread dimensions and tolerances. e. Method of designating UNJ threads. f. Tables for selected diameter-pitch combinations for close tolerance mechanical thread applications. g. Tables for screw thread - UNJ profile thread limit dimensions. This document specifies the geometric design for each characteristic of screw threads - UNJ profile inch series and the conformance requirements. In addition, the purpose of this standard is to: a. Define the geometric requirements for a selected series of Unified Screw Threads, modified to provide a radius at the external thread root. b. Establish requirements for a continuous radius at the root of the external threads. c. Establish requirements for an increase in the minor diameter of both internal and external threads to accommodate the external thread root radius.

Screw Threads - UNJ Profile, Inch Controlled Radius Root with Increased Minor Diameter [Superseded: OASD MIL-S-8879 C CANC NOTICE 3, OASD MIL-S-8879 C NOTICE 2, OASD MIL-S-8879 C NOTICE 1, OASD MIL-S-8879 C (1), OASD MIL-S-8879 C, OASD MIL-S-008879

SAE AS7949B-2004 飞机机架抗摩擦滚珠轴承的一般标准

This standard covers ball bearings in the - 65°F to 350°F temperature range as specified on the applicable drawing standards.

(R) Bearings, Ball, Airframe, Antifriction, General Standard for

SAE AS5609-2004 飞行器/存储通用接口控制文献格式标准

This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of Interface Control documents. The Common Interface Control Document Format Standard defines a common format for aircraft/store interface documents to foster increased interoperability. It is designed with the versatility to serve differing ICD philosophies and organizations. This aerospace standard defines the common technical data sections for the Common Interface Control Document Format down to the third header level for the majority of Subsections. The Common Interface Control Document Format Aerospace Standard provides a structured document format in appendixes supported by example paragraphs, drawings, etc.

Aircraft/Store Common Interface Control Document Format Standard

BS EN 12312-6:2004 航空器地面支持设备.特殊要求.去冰和防冻设备

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, operation and maintenance of deicers and equipment designed exclusively for deicing and washing of aircraft with deicing/antiicing/washing liquids when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some performance requirements recognised as essential by authorities, aircraft and GSE manufacturers as well as airlines and handling agencies. NOTE Safety of aircraft in connection with deicing/antiicing operations is not dealt with in this European Standard. Any, even minor, aircraft deicing or antiicing operation directly affects flight safety on take-off. Prevention of aeronautical accidents resulting from in-flight icing principally concerns the fluids and methods used, but it may in certain cases also concern deicing or antiicing equipment design or operation. These aeronautical aspects are not covered in this European Standard (see also Joint Aviation authorities (JAA), Joint Aviation Regulations (JAR) JAR-OPS subpart D 1.345 and any associated material). This standard applies to: — self-propelled deicers with fixed platform or hinged boom; — towable deicers with fixed platform or hinged boom; — stationary deicing/antiicing equipment (e.g. fixed boom, gantry or tower cranes equipped with aircraft deicing/antiicing fluid systems). This standard does not apply to: — fixed installations, such as separate storage tanks or heating and filling stations, which are not an integrated part of the stationary deicing equipment; — hydraulic control systems; — pneumatic systems; — flow generating systems as such. This standard does not establish requirements for noise and vibration. Noise and vibration are dealt with respectively in prEN 1915-4 and prEN 1915-3. This standard is not dealing with hazards in respect to a standard automotive chassis and the traffic on the apron. This part of EN 12312 is not applicable to deicers and deicing/antiicing equipment which are manufactured before the date of publication by CEN of this standard.

Aircraft ground support equipment - Specific requirements - De-icers and de-icing/anti-icing equipment

SAE USCAR24-2004 USCAR(安全气囊)气体发生器技术要求和验证

This specification establishes the performance, and validation requirements for the inflator assembly used in airbag modules. Pretensioners are covered only in respect to their effluents as included in Section 3.2.3, Effluents and their autoignition performance as included in Section 3.2.5, Autoignition, High Temperature Oven Performance/Autoignition of Heat Aged Inflators.

USCAR Inflator technical requirements and validation

ARMY A-A-52536 VALID NOTICE 1-2004 12.14和16A.W.G.号电器接触

A-A-52536, dated 20 November 1995, has been reviewed and determined to be valid for use in acquisition

CONTACT, ELECTRICAL NO. 12, 14, AND 16 A.W.G.

SAE AMS4827E-2004 轴承,含铅青铜80Cu-10Pb-10Sn钢背

This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing. These products have been used typically for bushings and bearings.

Bearings, Leaded Bronze 80Cu - 10Pb - 10Sn Steel Back

BS ISO 14952-4:2004 航天系统.液体系统的表面清洁度.粗略清洁过程

This part of ISO 14952 provides requirements related to rough-cleaning processes used to prepare parts and components for precision cleaning. It identifies precleaning processes that can be used for ground support equipment, launch vehicles and spacecraft. Rough cleaning removes contaminants such as weld scale, heat-treat scale, corrosion, oxide films, oils, grease, shop soil, fuel and carbon deposits. Rough cleaning is considered a normal shop process and usually does not require special environmental controls, packaging, handling or storage beyond accepted good practice. This part of ISO 14952 is applicable equally to ground support equipment, launch vehicles and spacecraft. NOTE The cleanliness level achieved by rough cleaning does not normally require verification beyond visual inspection. (Wipe test, waterbreak test, ultraviolet inspection, special lights and mirrors are considered aids to visual inspection.)

Space systems - Surface cleanliness of fluid systems - Rough-cleaning processes

BS ISO 14952-5:2004 航天系统.液体系统的表面清洁度.干燥过程

This part of ISO 14952 provides guidance related to processes used to dry parts and components that have been subjected to solvent-based or water-based cleaning processes, and identifies drying processes that can be used for equipment that has been cleaned for use in ground support equipment, launch vehicles and spacecraft. Vacuum drying can be used to remove entrapped fluids from intricate parts when normal purging methods have been found to be ineffective.

Space systems - Surface cleanliness of fluid systems - Drying processes

BS ISO 14952-3:2004 航天系统.液体系统的表面清洁度.不挥发性残流物和颗粒污染物的测定用分析程序

This part of ISO 14952 provides sampling and analytical test methods to validate the cleanliness levels of parts and components that have been precision cleaned, and identifies processes that may be used for the verification of cleanliness in ground support equipment, launch vehicles and spacecraft. This part of ISO 14952 is used to sample and verify the level of cleanliness of parts and components that have been precision cleaned and applies equally to parts, components and systems in ground support equipment, launch vehicles and spacecraft.

Space systems - Surface cleanliness of fluid systems - Analytical procedures for the determination of nonvolatile residues and particulate contamination

BS ISO 14952-6:2004 航天系统.液体系统的表面清洁度.精确清洁过程

This part of ISO 14952 specifies precision-cleaning processes for parts, components and systems used in flight-critical fluid applications. It can be used on equipment for ground support equipment, launch vehicles and spacecraft. This part of ISO 14952 identifies precision-cleaning processes and procedures that can be used on parts and components used in fluid systems and is applicable equally to ground support equipment, launch vehicles and spacecraft.

Space systems - Surface cleanliness of fluid systems - Precision-cleaning processes

HB 7737-2004 飞机辅机零件专用环氧聚酰胺涂料规范

本规范规定了飞机辅机零件专用环氧聚酰胺涂料 H04 - 68 各色环氧聚酰胺磁漆和 H06 - 28 锯黄环 氧聚酰胺底漆的要求、质量保证规定、交货准备及说明事项。 本规范适用于飞机辅机零件专用的环氧聚酰胺涂料。

Specification for special epoxy polyamide coatings for parts of aircraft accessories

BS ISO 14952-2:2004 航天系统.液体系统的表面清洁度.清洁度等级

This part of ISO 14952 defines the cleanliness levels used in the cleaning, analysis, and verification procedures for space fluid systems. It establishes a common nomenclature for use in describing cleanliness levels for equipment used in ground support equipment, launch vehicles and spacecraft. This part of ISO 14952 is used to specify the cleanliness level of fluid system components and equipment used in space systems. It is applicable equally to ground support equipment, launch vehicles and spacecraft.

Space systems - Surface cleanliness of fluid systems - Cleanliness levels

BS ISO 14952-1:2004 航天系统.液体系统的表面清洁度.词汇

This part of ISO 14952 defines the basic terms for use in cleaning processes for equipment and components used in space fluid systems. It is applicable to terms used in the description of processes for the cleaning, analysis and verification of fluid systems used in ground support equipment, launch vehicles and spacecraft.

Space systems - Surface cleanliness of fluid systems - Vocabulary

DLA A-A-59238 VALID NOTICE 1-2004 机械传动的圆形金属剪切机 [代替:DLA MIL-S-80093 B CANC 通告 1,DLA MIL-S-80093 B,DLA MIL-S-80093 A,DLA MIL-S-80093 (1),DLA MIL-S-80093]

A-A-59238, dated 26 May 1998, has been reviewed and determined to be valid for use in acquisition

SHEARING, MACHINES, METAL, CIRCULAR, POWER-DRIVEN [Superseded: DLA MIL-S-80093 B CANC NOTICE 1, DLA MIL-S-80093 B, DLA MIL-S-80093 A, DLA MIL-S-80093 (1), DLA MIL-S-80093]