SAE AIR 1064D-2007
制动系统动力学

(R) Braking System Dynamics

SAE AIR 1064D-2007 发布历史

The aircraft landing gear is a complex multi-degree of freedom dynamic system, and may encounter vibration or dynamic response problems induced by braking action. The vibratory modes can be induced by brake and tire-ground frictional characteristics, antiskid operation, brake design features, landing gear design features, and tire characteristics. The impact of this vibration can range from catastrophic failure of critical system components or entire landing gears, to fatigue of small components, to passenger annoyance. It is therefore important that the vibration is assessed during the design concept phase, and verified during the development and testing phases of the system hardware. This SAE Aerospace Information Report (AIR) has been prepared by a panel of the A-5A Subcommittee to present an overview of the landing gear problems associated with aircraft braking system dynamics, and the approaches to the identification, diagnosis, and solution of these problems. All pertinent system modes of vibration are described. In addition, facilities and techniques available for test and evaluation are presented and discussed, and useful references are cited. The terminology used is intended to be consistent with SAE AIR 1489, Aerospace Landing Gear Systems Terminology, but some terminology herein is not yet included in SAE AIR 1489. The panel members include representatives from major brake, landing gear, aircraft, and brake control system manufacturers. In addition, drafts of the document were circulated for input beyond the SAE to other experts in the field.

SAE AIR 1064D-2007由美国机动车工程师协会 US-SAE 发布于 2007-09-01。

SAE AIR 1064D-2007 在中国标准分类中归属于: V35 航空器及其附件综合，在国际标准分类中归属于: 49.045 结构和结构元件。

SAE AIR 1064D-2007 发布之时，引用了标准

• SAE AIR 4894-1995 起落架稳定性

SAE AIR 1064D-2007的历代版本如下：

• 2007年09月01日 SAE AIR 1064D-2007 制动系统动力学

SAE AIR 1064D-2007 制动系统动力学 由 SAE AIR 1064C-1997 变更而来。

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标准号

SAE AIR 1064D-2007

发布日期

2007年09月01日

实施日期

废止日期

无

中国标准分类号

V35

国际标准分类号

49.045

发布单位

US-SAE

引用标准

SAE AIR 1489 SAE AIR 4894-1995 1999-01-3404 2000-01-1699 2000-01-5599 2002-01-2948 2002-01-2949 2005-01-3436 2005-01-3437 710401 821393 851937 951416 952020 PT-37 PT-66

被代替标准

SAE AIR 1064C-1997

适用范围

The aircraft landing gear is a complex multi-degree of freedom dynamic system, and may encounter vibration or dynamic response problems induced by braking action. The vibratory modes can be induced by brake and tire-ground frictional characteristics, antiskid operation, brake design features, landing gear design features, and tire characteristics. The impact of this vibration can range from catastrophic failure of critical system components or entire landing gears, to fatigue of small components, to passenger annoyance. It is therefore important that the vibration is assessed during the design concept phase, and verified during the development and testing phases of the system hardware. This SAE Aerospace Information Report (AIR) has been prepared by a panel of the A-5A Subcommittee to present an overview of the landing gear problems associated with aircraft braking system dynamics, and the approaches to the identification, diagnosis, and solution of these problems. All pertinent system modes of vibration are described. In addition, facilities and techniques available for test and evaluation are presented and discussed, and useful references are cited. The terminology used is intended to be consistent with SAE AIR 1489, Aerospace Landing Gear Systems Terminology, but some terminology herein is not yet included in SAE AIR 1489. The panel members include representatives from major brake, landing gear, aircraft, and brake control system manufacturers. In addition, drafts of the document were circulated for input beyond the SAE to other experts in the field.