Wear and Related Characteristics of an Aircraft Tire During Braking

Wear and Related Characteristics of an Aircraft Tire During Braking PDF Author: John L. McCarty
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Wear, Friction, and Temperature Characteristics of an Aircraft Tire Undergoing Braking and Cornering

Wear, Friction, and Temperature Characteristics of an Aircraft Tire Undergoing Braking and Cornering PDF Author: John L. McCarty
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44

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Advances in Aircraft Brakes and Tires

Advances in Aircraft Brakes and Tires PDF Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768082498
Category : Technology & Engineering
Languages : en
Pages : 126

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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.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772

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Friction Characteristics of Three 30 by 11.5-14.5, Type 8, Aircraft Tires with Various Tread Groove Patterns and Rubber Compounds

Friction Characteristics of Three 30 by 11.5-14.5, Type 8, Aircraft Tires with Various Tread Groove Patterns and Rubber Compounds PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Friction Characteristics of Three 30 X 11.5-14,5, Type VIII, Aircraft Tires with Various Tread Groove Patterns and Rubber Compounds

Friction Characteristics of Three 30 X 11.5-14,5, Type VIII, Aircraft Tires with Various Tread Groove Patterns and Rubber Compounds PDF Author: Thomas J. Yager
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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NASA Technical Paper

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

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NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1034

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Experimental Investigation of the Braking and Cornering Characteristics of 30 X 11.5-14.5, Type VIII, Aircraft Tires with Different Tread Patterns

Experimental Investigation of the Braking and Cornering Characteristics of 30 X 11.5-14.5, Type VIII, Aircraft Tires with Different Tread Patterns PDF Author: Robert C. Dreher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

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The Elastic Response of Bias-ply Aircraft Tires to Braking Forces

The Elastic Response of Bias-ply Aircraft Tires to Braking Forces PDF Author: John A. Tanner
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Book Description
A study was made to evaluate the elastic behavior of a braked rolling tire and to relate this behavior to the tire characteristics obtained from simple static flexure tests. The study consisted of static and braked-rolling tests of two types of bias-ply aircraft tires and an analysis which related tire reaction to the braking forces. The results of this investigation indicate that the elastic response of an aircraft tire to braking forces can be defined by the displacement distribution along the tire periphery and by the fore-and-aft spring constant. Changes in the rolling radius due to braking can be predicted with reasonable accuracy from elastic measurements of the static free-tread periphery or from elastic measurements within the footprint during low-speed braking, assuming there is no slippage between the tire and the pavement. The results of these tests further indicate that what was heretofore considered as pure tire slippage under braked-rolling conditions may be wholly or in part the result of tire elasticity. The elasticity must be considered in the design or application of efficient automatic braking systems.