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

Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description


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

Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description


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

Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires PDF Author: A-5C Aircraft Tires Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description
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. This document has been reaffirmed to comply with the SAE 5-Year Review policy.

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

Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires PDF Author: A-5C Aircraft Tires Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description
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. ARP4955A has been reaffirmed to comply with the SAE five-year review policy.

Aircraft Tires

Aircraft Tires PDF Author: Kyle Schmidt
Publisher: SAE International
ISBN: 1468604643
Category : Transportation
Languages : en
Pages : 135

Book Description
Landing gear provides an intriguing and compelling challenge, combining many fields of science and engineering. Designed to guide the interested reader through aircraft tire design, selection, and integration to the aircraft landing gear, this book presents a specific element of landing gear design in an accessible way. The author’s two volume treatise, The Design of Aircraft Landing, was the inspiration for this book. The Design of Aircraft Landing is a landmark work for the industry and utilizes over 1,000 pages to present a complete, in-depth study of each component that must considered when designing an aircraft’s landing gear. While recognizing that not everyone may need the entire treatise, Aircraft Tires: Key Principles for Landing Gear Design is one of three quick reference guides focusing on one key element of aircraft design and landing gear design. This volume features tire construction and terminology, mechanics of pneumatic tires, tire performance and modeling as well reviewing undesirable tire behavior. R. Kyle Schmidt has over 25 years’ experience across three countries and has held a variety of variety of engineering roles relating to the development of new landing gears and the sustainment of existing landing gears in service.

A Comparison of Some Static and Dynamic Mechanical Properties of 18x5.5 and 49x17 Type VII Aircraft Tires as Measured by Three Test Facilities

A Comparison of Some Static and Dynamic Mechanical Properties of 18x5.5 and 49x17 Type VII Aircraft Tires as Measured by Three Test Facilities PDF Author: Samuel Kelly Clark
Publisher:
ISBN:
Category :
Languages : en
Pages : 86

Book Description


Advances in Aircraft Brakes and Tires

Advances in Aircraft Brakes and Tires PDF Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768082366
Category : Technology & Engineering
Languages : en
Pages : 126

Book Description
An aircraft’s interface with the ground—through its wheels, tires, and brakes—is critical to ensure safe and reliable operation, demanding constant technology development. Significant advancements have occurred with almost all civil airliners entering service with radial tires, and with the Boeing 787 having entered service in 2011 with electrically actuated carbon-carbon brakes. This book is divided into three sections: tires, control systems, and brakes, presenting a selection of the most relevant papers published by SAE International on these matters in the past fifteen years. They have been chosen to provide significant interest to those engineers working in the landing gear field. With almost all current large civil aircraft (and many smaller aircraft) opting exclusively for carbon-carbon brakes, a number of papers addressing the challenges of this technology are included. Papers touching on tire behavior and papers discussing brake control strategies are provided. For those looking for more information on aircraft landing gears, brakes, and tires, the SAE A-5 committee (the Aerospace Landing Gear Systems Committee), which meets twice a year, serves as a useful forum for discussion on landing gear issues and development. A current listing of documents produced and maintained by the A-5 committee is included in the appendix.

The Design of Aircraft Landing Gear

The Design of Aircraft Landing Gear PDF Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768099439
Category : Technology & Engineering
Languages : en
Pages : 1092

Book Description
The aircraft landing gear and its associated systems represent a compelling design challenge: simultaneously a system, a structure, and a machine, it supports the aircraft on the ground, absorbs landing and braking energy, permits maneuvering, and retracts to minimize aircraft drag. Yet, as it is not required during flight, it also represents dead weight and significant effort must be made to minimize its total mass. The Design of Aircraft Landing Gear, written by R. Kyle Schmidt, PE (B.A.Sc. - Mechanical Engineering, M.Sc. - Safety and Aircraft Accident Investigation, Chairman of the SAE A-5 Committee on Aircraft Landing Gear), is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. The Design of Aircraft Landing Gear is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design. With those requirements and compromises in mind,The Design of Aircraft Landing Gear starts with the study of airfield compatibility, aircraft stability on the ground, the correct choice of tires, followed by discussion of brakes, wheels, and brake control systems. Various landing gear architectures are investigated together with the details of shock absorber designs. Retraction, kinematics, and mechanisms are studied as well as possible actuation approaches. Detailed information on the various hydraulic and electric services commonly found on aircraft, and system elements such as dressings, lighting, and steering are also reviewed. Detail design points, the process of analysis, and a review of the relevant requirements and regulations round out the book content. The Design of Aircraft Landing Gear is a landmark work in the industry, and a must-read for any engineer interested in updating specific skills and students preparing for an exciting career.

Quasi-Static and Dynamic Response Characteristics of F-4 Bias-Ply and Radial-Belted Main Gear Tires

Quasi-Static and Dynamic Response Characteristics of F-4 Bias-Ply and Radial-Belted Main Gear Tires PDF Author: Pamela A. Davis
Publisher:
ISBN:
Category : Damping (Mechanics)
Languages : en
Pages : 48

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 32

Book Description


Airfield Compatibility

Airfield Compatibility PDF Author: Kyle Schmidt
Publisher: SAE International
ISBN: 1468604678
Category : Transportation
Languages : en
Pages : 135

Book Description
Landing gear provides an intriguing and compelling challenge, combining many fields of science and engineering. Designed to guide the interested reader through the key principles of aircra¬ft compatibility with the ground and ground infrastructure (airfields, heliports, etc.), this book presents a specific element of landing gear design in an accessible way. The author’s two volume treatise, The Design of Aircraft Landing, was the inspiration for this book. The Design of Aircraft Landing is a landmark work for the industry and utilizes over 1,000 pages to present a complete, in-depth study of each component that must considered when designing an aircraft’s landing gear. While recognizing that not everyone may need the entire treatise, Airfield Compatibility: Key Principles for Landing Gear Design is one of three quick reference guides focusing on one key element of aircraft design and landing gear design. This volume centers on how to ensure that the aircraft is compatible with the ground surfaces that it will encounter in use. R. Kyle Schmidt has over 25 years’ experience across three countries and has held a variety of variety of engineering roles relating to the development of new landing gears and the sustainment of existing landing gears in service.