Organizational maintenance repair parts and special tools lists : grader, road, motorized, DED, 13,000 pressure at blade, 12 foot blade, 6 wheels, 4 driving, 2 steerable, leaning front wheels, w/scarifier : Army model 440HA NSN 3805-00-931-7881 : Army model 440HAROPS NSN 3805-01-018-2866.

Includes indexes.

Organizational maintenance repair parts and special tools lists : crane, wheel mounted, 20 ton at 10 foot radius, 2 engines, diesel engine driven, 4x4 air transportable, phase III, w/blade, bulldozer, earth moving, w/block,tackle, 20 ton, w/boom, crane, 30 foot, Army model M2380, NSN 3810-00-763-7728, American Hoist and Derrick model 2380 and Army model M2385 ...

Includes index.

Operator and organizational maintenance manual : grader, road, motorized, diesel engine driven, 13,300 lb. pressure at blade, 12 ft. blade, 6 wheels, 4 driving, 2 steerable, leaning front wheels, w/scarifier (Letourneau-Westinghouse model 440HA), FSN 3805-931-7881.

"March 1967."

Operator and organizational maintenance manual : grader, road, motorized, diesel engine driven, 12 foot blade, (Caterpillar model 112F), FSN 3805-902-3083 w/Martin GS55 graderscraper, FSN 3805-900-8545.

"April 1968."

Operator's manual : grader, road, motorized, diesel driven, 12,100 to 14,300 lb pressure at blade, (Huber-Warco model 4D), FSN 3805-542-2995 winterized, FSN 3805-542-2996 nonwinterized.

Includes index.

Technical manual, operator and organizational manual : grader, road, motorized, DED, type 1, 6 wheel, 4 wheel drive, front wheel steering, 12-foot blade, Caterpillar model 120, FSN 3805-466-0084.

Includes index.

Direct support, general support, and depot maintenance manual : grader, road, motorized, diesel engine driven, 12 foot blade (Caterpillar model 112F), FSN 3805-902-3808, w/Martin GS55 graderscraper, FSN 3805-900-8545.

"March 1968."

Unit maintenance repair parts and special tools lists : grader, road, motorized, DED, 13,000 lb pressure at blade, 12 foot blade, 6 wheels, 4 driving, 2 steerable, leaning front wheels with scarifier : Army model 440HA (NSN 3805-00-931-7881) : Army model 440HAROPS (NSN 3805-01-018-2866).

"May 1992."

Intermediate direct support and intermediate general support maintenance repair parts and special tools lists ... : crane, wheel mounted, 20 ton at 10 foot radius, 2 engines, diesel engine driven, 4x4, air transportable, phase III; w/blade, bulldozer, earth moving; w/block, tackle, 20 ton; w/boom, crane 30 foot, Army model M2380 ....

"November, 1988."

The application of robotics to the turbine blade encapsulation process

A survey of the existing state-of-the-art of turbine blade manufacture highlights two operations that have not been automated namely that of loading of a turbine blade into an encapsulation die, and that of removing a machined blade from the encapsulation block. The automation of blade decapsulation has not been pursued. In order to develop a system to automate the loading of an encapsulation die a prototype mechanical handling robot has been designed together with a computer controlled encapsulation die. The robot has been designed as a mechanical handling robot of cylindrical geometry, suitable for use in a circular work cell. It is the prototype for a production model to be called `The Cybermate'. The prototype robot is mechanically complete but due to unforeseen circumstances the robot control system is not available (the development of the control system did not form a part of this project), hence it has not been possible to fully test and assess the robot mechanical design. Robot loading of the encapsulation die has thus been simulated. The research work with regard to the encapsulation die has focused on the development of computer controlled, hydraulically actuated, location pins. Such pins compensate for the inherent positional inaccuracy of the loading robot and reproduce the dexterity of the human operator. Each pin comprises a miniature hydraulic cylinder, controlled by a standard bidirectional flow control valve. The precision positional control is obtained through pulsing of the valves under software control, with positional feedback from an 8-bit transducer. A test-rig comprising one hydraulic location pin together with an opposing spring loaded pin has demonstrated that such a pin arrangement can be controlled with a repeatability of +/-.00045'. In addition this test-rig has demonstrated that such a pin arrangement can be used to gauge and compensate for the dimensional error of the component held between the pins, by offsetting the pin datum positions to allow for the component error. A gauging repeatability of +/- 0.00015' was demonstrated. This work has led to the design and manufacture of an encapsulation die comprising ten such pins and the associated computer software. All aspects of the control software except blade gauging and positional data storage have been demonstrated. Work is now required to achieve the accuracy of control demonstrated by the single pin test-rig, with each of the ten pins in the encapsulation die. This would allow trials of the complete loading cycle to take place.

Radially rotating miniature heat pipes for turbine blade cooling applications

Aerospace turboengines present a demanding challenge to many heat transfer scientists and engineers. Designers in this field are seeking the best design to transform the chemical energy of the fuel into the useful work of propulsive thrust at maximum efficiency. To this aim, aerospace turboengines must operate at very high temperatures and pressures with very little heat losses. These requirements are often in conflict with the ability to protect the turboengine blades from this hostile thermal environment. Heat pipe technology provides a potential cooling means for the structure exposed to high heat fluxes. Therefore, the objective of this dissertation is to develop a new radially rotating miniature heat pipe, which would combine the traditional air-cooling technology with the heat pipe for more effective turboengine blade cooling. ^ In this dissertation, radially rotating miniature heat pipes are analyzed and studied by employing appropriate flow and heat transfer modeling as well as experimental tests. The analytical solutions for the flows of condensate film and vapor, film thickness, and vapor temperature distribution along the heat pipe length are derived. The diffuse effects of non-condensable gases on the temperature distribution along the heat pipe length are also studied, and the analytical solutions for the temperature distributions with the diffuse effects of non-condensable gases are obtained. Extensive experimental tests on radially rotating miniature heat pipes with different influential parameters are undertaken, and various effects of these parameters on the operation of the heat pipe performance are researched. These analytical solutions are in good agreement with the experimental data. ^ The theoretical and experimental studies have proven that the radially rotating miniature heat pipe has a very large heat transfer capability and a very high effective thermal conductance that is 60–100 times higher than the thermal conductivity of copper. At the same time, the heat pipe has a simple structure and low manufacturing cost, and can withstand strong vibrations and work in a high-temperature environment. Therefore, the combination of the traditional air-cooling technology with the radially rotating miniature heat pipe is a feasible and effective cooling means for high-temperature turbine blades. ^

Bifurcation and dynamic response analysis of a rotating blade excited by upstream vortices

Acknowledgements The authors acknowledge the projects supported by the National Basic Research Program of China (973 Project)(No. 2015CB057405) and the National Natural Science Foundation of China (No. 11372082) and the State Scholarship Fund of CSC. DW thanks for the hospitality of the University of Aberdeen.

Improved damage detectability in a wind turbine blade by optimal selection of vibration signal correlation coefficients

Piotr Omenzetter and Simon Hoell’s work within the Lloyd’s Register Foundation Centre for Safety and Reliability Engineering at the University of Aberdeen is supported by Lloyd’s Register Foundation. The Foundation helps to protect life and property by supporting engineering-related education, public engagement and the application of research.

Sound generation by vortex-blade interactions

Abstract not available