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Author: A-5C Aircraft Tires Committee Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
A tire pressure monitoring system (TPMS) is a means to electronically measure and report the current tire pressure. Some systems are capable of transmitting the information to the flight deck while other systems are for use on the ground by maintenance personnel (only).This SAE Aerospace Recommended Practice (ARP) document is intended to establish overall component and system function guidelines and minimum performance levels for a TPMS. The system should visually indicate the tire inflation pressure status. These guidelines include, but are not limited to: a)Design recommendations for system components, which: 1monitor tire inflation, and, 2are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment. b)Recommended performance and safety guidelines for a TPMS. ARP6137 has been reaffirmed to comply with the SAE five-year review policy.
Author: A-5C Aircraft Tires Committee Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
A tire pressure monitoring system (TPMS) is a means to electronically measure and report the current tire pressure. Some systems are capable of transmitting the information to the flight deck while other systems are for use on the ground by maintenance personnel (only).This SAE Aerospace Recommended Practice (ARP) document is intended to establish overall component and system function guidelines and minimum performance levels for a TPMS. The system should visually indicate the tire inflation pressure status. These guidelines include, but are not limited to: a)Design recommendations for system components, which: 1monitor tire inflation, and, 2are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment. b)Recommended performance and safety guidelines for a TPMS. ARP6137 has been reaffirmed to comply with the SAE five-year review policy.
Author: A-5C Aircraft Tires Committee Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
The intent of this SAE Aerospace Information Report (AIR) is to inform the aerospace industry about various systems available to monitor the inflation pressure and/or temperature of an aircraft tire. The tire pressure monitoring system (TPMS), with cockpit display, is the most widely used of all aircraft tire monitoring systems, and is detailed in this document more than other systems. AIR4830A has been reaffirmed to comply with the SAE five-year review policy.
Author: S-7 Flight Deck Handling Qualities Stds for Trans Aircraft Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
This document recommends design criteria for a Flight Deck Tire Pressure Monitoring System. The requirements arise from operational experience of incidents, which have led to considerable damage to aircraft systems and structures caused by tire debris and wheel fragments. ARP4102/3 has been reaffirmed to comply with the SAE five-year review policy.
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.
Author: Robert Kyle Schmidt Publisher: SAE International ISBN: 0768082188 Category : Technology & Engineering Languages : en Pages : 138
Book Description
The aircraft landing gear system is relatively unique on board an aircraft—it is both structure and machine, supporting the aircraft on the ground, yet providing functions such as energy absorption during landing, retraction, steering, and braking. Advances in Aircraft Landing Gear is a collection of eleven hand-picked technical papers focusing on the significant advancements that have occurred in this field concerning numeric modeling, electric actuation, and composite materials. Additionally, papers discussing self-powered landing gear and more electrical overall aircraft architectures have been included. The content of Advances in Aircraft Landing Gear is divided into two sections: Analysis and Design Methods; and Electric Actuation, Control, and Taxi. For those looking for more information on aircraft landing gears, 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 this committee appears in the appendix.
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.
Author: Highway Tire Committee Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
To establish overall performance guidelines, test methods, and minimum performance levels for a TPMS. The system shall visually indicate the tire inflation pressure status. These guidelines include, but are not limited to: aA test methodology for a device which monitors tire inflation, that is located in/on the tire/wheel environment. bRecommended performance guidelines for a TPMS. Not Applicable.
Author: Michael Kraft Publisher: Elsevier ISBN: 0857096486 Category : Technology & Engineering Languages : en Pages : 358
Book Description
MEMS for automotive and aerospace applications reviews the use of Micro-Electro-Mechanical-Systems (MEMS) in developing solutions to the unique challenges presented by the automotive and aerospace industries. Part one explores MEMS for a variety of automotive applications. The role of MEMS in passenger safety and comfort, sensors for automotive vehicle stability control applications and automotive tire pressure monitoring systems are considered, along with pressure and flow sensors for engine management, and RF MEMS for automotive radar sensors. Part two then goes on to explore MEMS for aerospace applications, including devices for active drag reduction in aerospace applications, inertial navigation and structural health monitoring systems, and thrusters for nano- and pico-satellites. A selection of case studies are used to explore MEMS for harsh environment sensors in aerospace applications, before the book concludes by considering the use of MEMS in space exploration and exploitation. With its distinguished editors and international team of expert contributors, MEMS for automotive and aerospace applications is a key tool for MEMS manufacturers and all scientists, engineers and academics working on MEMS and intelligent systems for transportation. Chapters consider the role of MEMS in a number of automotive applications, including passenger safety and comfort, vehicle stability and control MEMS for aerospace applications are also discussed, including active drag reduction, inertial navigation and structural health monitoring systems Presents a number of case studies exploring MEMS for harsh environment sensors in aerospace
Author: Hilmi Mohd Zahidi Publisher: ISBN: Category : Pressure Languages : en Pages : 60
Book Description
Tyre pressure monitoring system (TPMS) is an electronic system that monitors the air pressure of an automobile tire and alerts the driver by displaying the real pressure or just a warning light. This project is focused on designing and developing a direct TPMS which the measurement of the air pressure is taken directly using pressure sensor. Suitable components are researched to design the prototype. Main components needed are pressure sensor, voltage-to-frequency converter, transmitter, receiver, and frequency-to-voltage converter. To power the prototype, piezoelectric method is chosen instead of using lithium battery. However, due to limitations and problems faced, piezoelectric method will be discussed by assuming the design of power generator. Main components need to be calibrated to ensure the consistency and precision of the prototype in reporting the pressure. Calibration for pressure sensor is performed by simply applying a known value of pressure and the output voltage is measured. For voltage-to-frequency and frequency-to-voltage converters, a known value of voltage or frequency is applied and the output is monitored using voltmeter and oscilloscope. The results show promising data by proving the relationship between the input and output for each component. Piezoelectric method is also discussed but in terms of the design of the circuit. As for the conclusion, although there are many problems and limitations faced, this prototype is a promising product in real worldapplication.
Author: A-5C Aircraft Tires Committee
Author: A-5C Aircraft Tires Committee
Author: A-5C Aircraft Tires Committee
Author: S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
Author: Paul Arthur Grygier
Author: Robert Kyle Schmidt
Author: Robert Kyle Schmidt
Author: Robert Kyle Schmidt
Author: Highway Tire Committee
Author: Michael Kraft
Author: Hilmi Mohd Zahidi