V42 起飞着陆装置 标准查询与下载

HB 6496-1991 飞机液压刹车阀通用技术条件

本标准规定了飞机液压刹车阀（以下简称刹车阀）的技术要求、试验方法和检验规则。 　　本标准适用于输入压力不超过21MPa的Ⅰ型（-55～70℃）和Ⅱ型（-55～135℃）飞机机轮液压刹车系统中的刹车阀。本标准适用于刹车阀新产品的研制及其批量生产。

General specifications for aircraft hydraulic brake valves

HB 6482-1990 起落架系统通用技术要求

本标准规定了常规起落架系统及其部件的性能、研制、相容性和鉴定要求。它与《起落架系统通用技术要求使用指南》（以下简称使用指南）同时使用。在编写具体的型号起落架系统要求时，应逐一填写本标准的空白栏。 　　本标准适用于飞机（含直升机）的起落架系统。在某些条文之后的括号里凡标注“有”或“没有”字样的，表示该条文对所研制的型号“适用”或“不适用”。

General technical requirements for landing gear system

SAE AIR4358-1991 倾斜,自由旋转前起落架的操纵效应

This Aerospace Information Report (AIR) considers the origin of cornering forces generated by tilted, free-swiveling nose gears; the effect of various landing gear parameters on the measured cornering forces; and a method of towing aircraft to measure the resulting steering forces.

Steering Effect of Tilted, Free-Swiveling Nose Gears

SAE AIR4077-1989 启动起落架时机械开关的用法

This Aerospace Information Report (AIR) will examine considerations relative to the use of mechanical switches on aircraft landing gear, and present lessons learned during the period that these devices have been used. The purpose of this AIR is to suggest specification, application, performance, and validation criteria for electromechanical switches used for environmentally severe applications on aircraft landing gear.

Mechanical Switch Usage for Landing Gear Applications

NF L35-182:1988 航空航天系列.耐蚀钢制带径向细齿的止动垫圈.尺寸

Aerospace series. Washers, lock with radial serrations in corrosion resisting steel. Dimensions.

NF L35-183:1988 航空航天系列.耐蚀钢制镀镉带径向细齿的止动垫圈.尺寸

Aerospace series. Washers, lock, with radial serrations, in corrosion resisting steel, cadmium plated. Dimensions.

SAE ARP4102/2-1988 自动制动系统

This document recommends design criteria for an Automatic Braking System. The ABS shall enhance braking performance under most aircraft configurations and all runway conditions.

Automatic Braking System (ABS) [Superseded: SAE ARP 268G]

HB 6176-1988 飞机油气式缓冲器起落架

本规范规定了飞机油气式缓冲器起落架（以下简称起落架）的技术要求。 　　本规范是通用规范。适用于起落架的订货、研制和验证。对于具体型号应按合同条款执行。

Aircraft oil-pneumatic buffer landing gear

SAE AIR4243-1988 着陆场所/起落架的兼容性-SAE简史/兵团合作

This document discusses the work done by the U.S. Army Corps of Engineers and the Waterways Experiment Station (WES) in support of SAE A-5 Committee activity on Aerospace Landing Gear Systems. It is an example of how seemingly unrelated disciplines can be combined effectively for the eventual benefit of the overall aircraft systems, where that system includes the total airfield environment in which the aircraft must operate. In summary, this AIR documents the history of aircraft flotation analysis as it involves WES and the SAE.

Landing Area/Landing Gear Compatibility - A Brief History of SAE/Corps of Engineers Cooperation

SAE AS707B-1988 真空胎飞机轮的热敏感膨胀压力释放装置

This standard establishes minimum design, installation, qualification, and operational requirements for thermally actuated, pressure release devices for use only in tubeless tire type aircraft wheels. These devices are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the assembly to exceed a safe temperature operating level. The objective is to prevent tire or wheel rupture from brake generated heat which could cause serious personnel injuries or serious aircraft operational hazards.

Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft Wheels

2M 45 Pt.1-1986 飞机轮胎和轮辋.第1部分:新轮胎、翻新轮胎和轮辋规范

Definitions, tyre size designation, tyre markings. Tyre dimensional tolerances for new and retreaded tyres. For new tyres only methods for determination of growth allowances and of clearance allowances. A comprehensive specification for rims is also included.

Aircraft tyres and rims. Specification for new tyres, retreads and rims

2M 45 Pt.2-1986 飞机轮胎和轮辋.第2部分:轮胎试验法

Aircraft tyres and rims. Methods of test for tyres

HB 5937-1986 飞机活动式着陆滑行灯试验方法

本标准规定了飞机活动式着陆灯、滑行灯、着陆滑行灯在预定使用条件下的实验室试验方法，以评定产品在着陆起飞使用条件下的适应能力。 　　本标准适用于新研制的产品。超出本标准规定的特殊要求，应在其产品专用标准中规定。

Test method for aircraft movable landing taxi lights

SAE AS666C-1982 航空器无管轮胎车轮用静态密封的空腔设计和O型环选择

This specification has been declared "NONCURRENT" as of January 2005. It is recommended, therefore, that this document not be specified for new designs. Each of these "NONCURRENT" documents is available from SAE. Document made inactive for new designs. Committee feels that the practice amongst wheel manufacturers is to use proprietary gland standards and materials to improve seal integrity rendering this document obsolete for new design. This document shall be retained for historical record only.

Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels

SAE AS666B-1982 用于飞机无内胎轮毂静密封的腔设计和O型圈选择R(1993)

This specification has been declared "NONCURRENT" as of January 2005. It is recommended, therefore, that this document not be specified for new designs. Each of these "NONCURRENT" documents is available from SAE. Document made inactive for new designs. Committee feels that the practice amongst wheel manufacturers is to use proprietary gland standards and materials to improve seal integrity rendering this document obsolete for new design. This document shall be retained for historical record only.

Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels R(1993)

SAE AIR3276-1981 轮毂插销扩展型孔制备

Boss - Plug/Pin, Expansion Type Hole Preparation

Boss - Plug/Pin, Expansion Type Hole Preparation

KS W 2013-1977 航空器重量和重力中心位置测定方法

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Methods of weighing and determination of center of gravity location for aircraft

KS W 2012-1977 航空器组装检测通则

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General Regulation of Aircraft Assembling Inspection

NF L82-680:1970 飞机起落架.飞机轮胎尺寸和间隙的测定

DETERMINING DIMENSIONS AND SAFETY CLEARANCES FOR AIRCRAFT TYRES.

NAVY MIL-L-8552 C (2)-1968 飞机减振器起落架(航空油型)

this amendment foms a part of 1411itarySpecification L-S552c,19 November1965,andiemandatoryforueeby allDepartmnteand Agenciesof theEepartmntof Dafenee.

LANDING GEAR, AIRCRAFT SHOCK ABSORBER (AIR-OIL TYPE)