Browse Topic: Thermal testing

Items (84)
A-4 Aircraft Instruments Committee
The Tiltrotor Test Rig (TTR) is a NASA project, joint with the U.S. Army and Air Force, to develop a new, large-scale proprotor test system for the National Full-Scale Aerodynamics Complex (NFAC). The first wind-tunnel entry was completed in November 2018 with a modern, 26-ft diameter proprotor. The primary purpose was to complete the development of the TTR, including systems integration with the NFAC. The TTR and rotor were tested up to 273 knots in axial flow. This is the highest airspeed ever achieved by a full-scale proprotor in any wind tunnel. Extensive conversion-mode data were also acquired, and hover/climb conditions were explored. Additional testing included aerodynamic tares, motor tests, thermal tests, modal vibration tests, and other checkout activities. This paper summarizes the results of the test, including examples of the most significant data.
W., C.Sheikman, AlexNorman, Thomas
The scope of this SAE Information Report is to provide general information relative to the nature and use of infrared techniques for nondestructive testing. The document is not intended to provide detailed technical information, but will serve as an introduction to the theory and capabilities of infrared testing and as a guide to more extensive references.
Metals Technical Committee
Effect of Thermal Behavior of Friction Materials on Brake Squeal2014-01-25149/28/2014
Brake noise is an emerging concern in Indian Auto-industry; with brake squeal being the most evident form of brake NVH. Squeal noise generation attributes to many parameters including kinematics of braking parts during pressure application, structural dynamic behavior which in turn depends on coupling at resonant frequencies of different parts of a brake assembly, material of brake parts, operating clearances in the mating parts etc. The genesis of brake squeal lies in the generation of unstable frictional forces during braking event. These frictional forces induce uncontrolled amplification of brake parts vibration, which in turn tend to produce perceivable sound or noise. The magnitude this vibration induced squeal depends on co-efficient of friction, braking pressure, speed and temperature of friction material. It is known from typical squeal evaluations on dynamometer that at different temperatures of friction, the ability/ occurrence, of squeal is different, typically in the range of 50°C to 200°C. This could be linked to the thermo-elastic behavior of friction, as it is a heterogeneous material comprising thermally sensitive raw contents as compared to other parts of brake assembly which are largely a base of iron and less sensitive to change elasticity in above temperature range. The change in elastic behavior of friction can shift the resonant frequencies of pads/shoes and hence affect propensity of the squeal for a given brake. This behavior of friction needs an objective judgment, especially with different types of fiction materials like NAO, Low Metal, Semi-Metallic used in automotive brake applications. This paper focuses on comparative analysis carried out on two identified brakes viz. a disc brake (of an SUV) and a drum brake (of a small car) using 3 different friction parts per brake for NAO and low metal type. The thermal behavior of friction in terms of shift in resonant frequencies of pads/shoes and associated change in modal loss factor, as a measure of structural damping at identified temperatures, have been objectively compared between different grades for a given brake type. Its significance towards brake noise has been discussed.
Mahale, PrashantBohari, AzizM P, Raajha
Characterization of PU Foam for High Temperature Applications in Automobiles2014-01-10354/1/2014
Due to continuous demands from OEM's to reduce weight and make more compact vehicles, high heat generation from vehicle has become common phenomenon. Thermal insulation is a need of the hour to cater to such demands. The temperature rise is more critical around engine areas. OEM's use many design solutions to cater to such heat build up's. One of the design solutions includes use of thermally insulating materials e.g. Foams, insulating fabrics etc… First section of this paper deals with comparative study of polyurethane (PU) soft foam and rigid skin polyurethane foam. To define the base line, the samples were subjected to various tests to determine physical, thermal and chemical properties. Also both the types of foams were subjected to high temperature and low temperature heat ageing. From the experiments, it was observed that soft PU foam provides better re-bounce property than rigid skin PU foam. This is an important property to be considered, when foam is subjected to compression load during fitment. Foam would regain its shape and size on removal of load and hence provides better stability. Also, thermal conductivity of both the foams is compared to check for their ability to provide thermal insulation. Based on above results, soft PU foam was further tested for performance level tests to understand the foam behavior under simulated thermal test conditions. The thermal test method was developed to simulate heat generation during actual driving conditions. Foam was also subjected to physical test till failure including compression set. The test results are discussed and concluded for selection of better foam for the under the hood application. The results of this study were useful for determining optimum foam structure providing good insulation with lower weight.
Mehta, ShrutiHatwalne, MrunalDhule, Mangesh
Integral Molded Brake Pad with Long Fiber Thermosetting Molding Compound for Automotive Brake System2012-01-18349/17/2012
Recently, in view of environment, safety, comfort and convenience for cars, the demand of low fuel consumption is increasing more than before, and weight saving of the automotive parts is pursued. In the tide of weight saving, there is a strong demand of light weightening of the backing plate by replacing steel with plastics. We have been developing long fiber phenolic molding compound, which has excellent mechanical strength and excellent heat resistance, and have examined in order to apply it to the backing plate for brake pad. By applying this material to backing plate, the weight of brake pad can be reduced in half compared with that of conventional pad made of steel. In the automotive parts, it is said that reduction of part weight under the suspension is about ten times as effective for reducing fuel consumption as that of weight upper the suspension, therefore, phenolic brake pad has a big impact. Also, instead of simple replacement of steel plate with phenolic plate, it may be possible to make integral molded brake pad with lining by using a backing plate made from the same kind of resin. Therefore, there will be no possibility of separation at the interface between backing plate and lining. Although the conventional brake pad needs a pretreatment of backing plate and adhesion with lining, all these prior process may be eliminated by integral molding technology. And phenolic backing plate does not need a coating for antirust. Cracks and blisters were not found and the flatness of molded backing plate held about 0.1 mm after thermal test at 500 deg. C. We can contribute to development of a new light weighted caliper brake system by integral molded phenolic brake pad.
Inokuchi, Hideaki
This SAE Recommended Practice applies to functions of motor vehicle signalling and marking lighting devices which use light emitting diodes (L.E.D.’s) as light sources. This report provides test methods, requirements, and guidelines applicable to the special characteristics of L.E.D. lighting devices. This Recommended Practice is in addition to those required for devices designed with incandescent light sources. This report is intended to be a guide to standard practice and is subject to change to reflect additional experience and technical advances.
Signaling and Marking Devices Stds Comm
Mars Exploration Rover Thermal Test Program Overview2004-01-23107/19/2004
In January 2004, two Mars Exploration Rovers (MER) landed on the surface of Mars to begin their mission as robotic geologists. A year prior to these historic landings, both rovers and the spacecraft that delivered them to Mars, were completing a series of environmental tests in facilities at the Jet Propulsion Laboratory. This paper describes the test program undertaken to validate the thermal design and verify the workmanship integrity of both rovers and the spacecraft. The spacecraft, which contained the rover within the aeroshell, were tested in a 7.5 m diameter thermal vacuum chamber. Thermal balance was performed for the near earth (hot case) condition and for the near Mars (cold case) condition. A solar simulator was used to provide the solar boundary condition on the solar array. IR lamps were used to simulate the solar heat load on the aeroshell for the off-sun attitudes experienced by the spacecraft during its cruise to Mars. Each rover was tested separately in a 3.0 m diameter thermal vacuum chamber over conditions simulating the warmest and coldest expected Mars diurnal temperature cycles. The environmental tests were conducted in a quiescent nitrogen atmosphere at a pressure of 8 to 10 Torr. In addition to thermal balance testing, the science instruments on board the rovers were tested successfully in the extreme environmental conditions anticipated for the mission. A solar simulator was not used in these tests.
Pauken, M. T.Kinsella, G. M.Novak, K. S.Tsuyuki, G. T.Phillips, C. J.
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