83.160.20 标准查询与下载

KS M ISO 9475:2010 有内胎和无内胎的航空器轮胎.气门咀、孔及帽.试验方法

이 표준은 이너 튜브가 있거나 또는 없는 항공기 타이어용 밸브 코어 및 캡의 시험방법과 최

Aircraft inner tube and tubeless tyre valves-Cores and caps-Test methods

SAE ARP5257B-2010 轮胎超速着陆试验

This document covers the basis of, and test procedure for, an overspeed landing testing on aircraft tires with rated speeds of 190 mph (306 km/h) and above. The conditions requiring an overspeed test, alternatives, test requirements and pass/fail criteria are addressed. The purpose of this ARP is to define a test procedure for the qualification of aircraft tires to an overspeed landing requirement.

Tire Overspeed Landing Test

GOST R ISO 3324-2-2009 航空器轮胎及轮辋.第2部分:轮胎测试方法

Aircraft tyres and rims. Part 2. Test methods for tyres

SAE AIR5797-2008 航空器轮胎轮廓开发和实验室测试的实施

This SAE Aerospace Information Report (AIR) describes the current process for performing comparative wear testing on aircraft tires in a laboratory environment. This technique is applicable to both radial and bias tires, and is pertinent for all aircraft tire sizes.This AIR describes a technique based upon “wear” energy. In this technique, side wear energy and drag wear energy are computed as the tire is run through a prescribed test program. The specifics that drive the test setup conditions are discussed in Sections 4 through 7. In general, the technique follows this process:• A test profile is developed from measured mechanical property data of the tires under study.• Each tire is repeatedly run to the test profile until it is worn to the maximum wear limit (MWL). Several tires, typically 5 to 10, of each tire design are tested.• Wear energy is computed for each test cycle and then summed to determine total absorbed wear energy.• An index is calculated for each tire design. This is accomplished by dividing the total linear inches of wear at the most worn point into the total wear energy.• The indexes are then normalized to provide a comparative wear rate. The described technique is not meant to provide an absolute wear rate or wear index because the technique does notproduce results that allow the user to say a tire will last for a specific number of landings. However, it does provide a comparative index. It will make a distinction from one tire design to another by indicating a percentage difference inabrasive wear rate under representative operational conditions. The technique has been demonstrated in a number of test programs and is shown to have an extremely high correlation to field data. Supporting data is included in Section 9.

Aircraft Tire Wear Profile Development and Execution for Laboratory Testing

SAE ARP5543-2008 结合膨胀压力计的航空器轮膨胀阀

This specification covers the recommended design, construction, performance and testing requirements for aircraft wheel inflation valves incorporating an inflation pressure gauge which are mounted on the aircraft wheel. These valve/gauge assemblies should be appropriate for use on all aircraft types supported by tubeless tire/wheel assemblies.

Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge

KS W ISO 3324-2:2007 航空轮胎和轮辋.第2部分:轮胎试验方法

이 규격은 다음 범위 내에서 항공기용 신생 및 재생 타이어를 시험하는 방법에 대하여 규정한

Aircraft tyres and rims－Part 2：Test methods for tyres

SAE ARP4955A-2007 航空器轮胎静态和动态性能的测量用推荐实施规程

The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish guidelines for the measurement of static and dynamic characteristic properties of aircraft tires. It is intended as a general guide toward standard practice, but may be subject to frequent changes to keep pace with experience and technical advances. This revision (Revision A) is also intended to provide suggested guidelines for synthesizing tire dynamic data necessary for landing gear shimmy analyses.

(R) Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires

TIS 2301-2006 航空轮胎

Aircraft tire

SAE ARP5542-2004 手持式飞行器轮胎充气气压量规

This SAE Aerospace Recommended Practice (ARP) covers the design, construction, performance and testing requirements for hand held aircraft tire inflation pressure gauges with valve stem attachment chuck to be used with all aircraft types. The gauges in this specification are those which are designed to read the tire inflation pressure from a position adjacent to the tire.

Hand Held Aircraft Tire Inflation Pressure Gauges

NAVY MS14147 REV A VALID NOTICE 3-2004 重整NAVY飞机轮胎业务适应性(飞行)试验

MS14147A remains inactive for new design, however, the document is valid for use.

SERVICE SUITABILITY (FLIGHT) TESTING OF REBUILT NAVY AIRCRAFT TIRES

KS W ISO 3324-1:2002 航空轮胎和轮辋.第1部分:规范

이 규격은 신생 및 재생 항공기 타이어와 림에 대하여 규정한다.

Aircraft tyres and rims－Part 1：Specifications

SAE ARP5507-2002 航空器轮胎到轮子的工作特性

The performance of an aircraft tire/wheel assembly in service is dependent on the geometrical fit, load distribution, and performance at the tire/wheel interface while rolling. This document focuses on the tire-to-wheel circumferential movement for a new tubeless tire.

Aircraft Tire-to-Wheel Performance Characteristics

KS W 1537-1999(2009) 飞机轮胎和轮辋 - 第1部分:规范

Aircraft tyres and rims－Part 1：Specification

KS W 1538-1999(2009) 飞机轮胎和轮辋 - 第2部分:轮胎试验方法

Aircraft tyres and rims－Part 2：Test methods for tyres

NAVY MS14147 REV A NOTICE 2-1999 重整NAVY飞机轮胎业务适应性(飞行)试验

MS14147A(AS) is inactive for new design and is no longer used except for replacement purposes.

SERVICE SUITABILITY (FLIGHT) TESTING OF REBUILT NAVY AIRCRAFT TIRES

SAE ARP1322A-1998 超压释放装置

This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and test recommendations for aircraft tubeless tire and wheel overpressurization release devices to protect from possible explosive failure of the contained air chamber due to overinflation. This device will not protect against flash fire explosive conditions within the air chamber which may occur due to extremely overheated brakes. To protect against this condition, nitrogen or other inert gas should be used for inflation. This document recommends minimum requirements for aircraft tubeless tire and wheel overpressurization release devices. Overpressurization Release Devices shall be furnished in a range of sizes to accommodate the sizes and inflation pressure requirements of tubeless tires and wheels used on aircraft.

Overpressurization Release Devices

ISO 3324-2:1998 航空轮胎和轮辋 第2部分:轮胎试验方法

This part of ISO 3324 specifies test methods for new and retreaded civil aircraft tyres in the following categories: a) low-speed tyres: for ground speeds up to and including 104 kn; b) high-speed tyres: for ground speeds above 104 kn. NOTE — 1 kn = 1,85 km/h = 1,15 mile/h.

Aircraft tyres and rims - Part 2: Test methods for tyres

SAE ARP4955-1997 飞机轮胎静态和动态特性测量的推荐规程

The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish guidelines for the measurement of static and dynamic characteristic properties of aircraft tires. It is intended as a general guide toward standard practice, but may be subject to frequent changes to keep pace with experience and technical advances. It replaces the previous SAE document, AIR1380.

Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires

SAE ARP5257-1997 轮胎超速着陆测试

This document covers the basis of, and test procedure for, an overspeed landing testing on aircraft tires with rated speeds of 190 mph (306 km/h) and above. The conditions requiring an overspeed test, alternatives, test requirements and pass/fail criteria are addressed. The purpose of this ARP is to define a test procedure for the qualification of aircraft tires to an overspeed landing requirement.

Tire Overspeed Landing Test

NAVY MS14193 NOTICE 2-1997 飞机轮胎寿命周期成本(LCC)规程

This notice should be filed in front of MS14193(AS), dated 9 October 1979, and Notice 1, dated 14 May 1987.

AIRCRAFT TIRE LIFE CYCLE COSTING (LCC), PROCEDURES FOR