Browse Topic: Cooperative programs
America Makes, the National Additive Manufacturing Innovation Institute, announced the 15 awardees of its second call for additive manufacturing (AM) applied research and development projects. Driven by the National Center for Defense Manufacturing and Machining, America Makes will provide $9 million in funding toward these projects with $10.3 million in matching cost share from the awarded project teams for total funding worth $19.3 million. The projects are expected to commence in early Spring.
Engineering VP Scott Kunselman talks about working with Fiat, taking the lead in vehicle electrification, and putting the mojo back into Chrysler's product-development team. After 25 years of riding one of the auto industry's wildest roller coasters, Scott Kunselman now works on comparatively stable ground. More relaxed it's not, however. As Chrysler's Senior Vice President- Engineering, he's charged with integrating his company's product-development activities with those of Fiat. That means launching more than 20 new or significantly revamped North American models, consolidating four vehicle platforms, and working with his colleagues in Turin to commonize three other platforms, along with billions worth of related systems and components.
For companies that do not need NASA-developed technology or advanced test facilities but still want to leverage some of the brain power of NASA’s engineering teams to solve a design problem in their product, NASA funds the Space Alliance Technology Outreach Program (SATOP). Administered by Bay Area Houston Economic Partnership, SATOP is a cooperative program among Florida, New Mexico, New York, and Texas that brings together more than 55 space companies, universities, colleges, and NASA centers to make NASA expertise available to small businesses.
A report describes the completed first phase of a NASA/industry cooperative program of research on metal-matrix composites (MMCs) as lightweight, strong, high- temperature-resistant materials for use in future aircraft engines. The first phase of the research included assessment of life- and fracture-prediction methods, determination of fracture strengths and fatigue lives, and experiments in nondestructive evaluation. The metal-matrix composite specimens used in these studies were rings made of silicon-carbide-based fibers in a titanium-alloy matrix. The particular composite material was chosen because extensive data on the material were already available and the material is representative of composites that would be used in aircraft engines. Five fracture- and life prediction analysis methods were applied to the rings; their predictions were compared with each other and with experimental data on fracture of the rings. Manufacturing defects prevented the researchers from conducting planned cyclic tests. Fatigue-life predictions ranged from 1,000 to 15,000 cycles. Fracture-stress predictions were less scattered, ranging from 25 to 40.1 kpsi (172 to 276 MPa). Low-resolution x-ray computed tomography proved to be an effective non-destructive evaluation technique.
This paper describes a fuzzy logic (FL) approach to the design, implementation, and tuning of an expert knowledge-based TCS for a four-wheel drive vehicle. Military and commercial mutual interests in TCS technology are highlighted as the underlying motivation for this government, industry, academia cooperative program. Coordinated parallel efforts to model the TCS equipped vehicle and to perform basic on-vehicle TCS experiments provided additional information to augment the knowledge obtained from a study of commercial TCSs and the tire traction literature. The general traction control problem is discussed along with the hardware considerations for a TCS. The design and integration of the resulting FL-based TCS are described along with a representative sample of the test results documenting the system's performance.
This is the fourth in a series of tests conducted as a Coordinating Research Council cooperative program to evaluate the measurement methods used to analyze diesel exhaust gas constituents. A multi-cylinder engine was circulated to 15 participants who measured emissions at three engine conditions. All 15 participants measured nitric oxide and carbon monoxide with several laboratories measuring nitric oxide by both NDIR (Non-Dispersive Infrared) and CHEMI (Chemiluminescence). Some participants also measured carbon dioxide, nitrogen dioxide, oxygen, and unknown span gases. The test results are compared with the Phase III cooperative tests which involved simultaneous measurement of emissions by participants. The precision of the results was poorer in Phase IV than Phase III.
This paper presents some results of wind tunnel tests and analytical studies of a Grumman aircraft design called HELICAT which features a prop rotor mounted in a tilting pod at each wing tip. The rotor incorporates an offset flapping hinge with positive (pitch reducing) delta-3. The test program was divided between evaluation of the Helicat prototype design and investigation of a "research" whirl flutter configuration. Most of this paper is devoted to the whirl flutter investigation. One case of blade flutter was encountered in the Helicat configuration; 83 cases of whirl flutter were obtained in the research configuration. Forward, backward, and bimodal whirl flutter were encountered. The parametric study of whirl flutter included variations in blade pitch-flap coupling, hinge offset, rotor pod pitch and yaw stiffness, and damping. Analytical correlation studies showed good agreement with the test data. Testing of this semi-span dynamically similar model was performed in the 16-foot Transonic Dynamics Tunnel at NASA, Langley, under a NASA/Grumman cooperative program during the period 3 February through 8 April 1971.
A Coordinating Research Council cooperative program was conducted to evaluate the measurement methods used to analyze nitric oxide and carbon monoxide in diesel exhaust. Initially, a single-cylinder test engine was circulated among participants with poor results. Tests were then conducted at one site using a multicylinder diesel engine. Six organizations participated in the program. Exhaust analyses were conducted at steady-state engine conditions and on a 3 min cycle test. Span gases of unknown concentration were also analyzed. The participants results varied but averaged less than ±5% standard deviation both within (repeatability) and among (reproducibility) the instruments. The short cycle test was in good agreement with the steady-state measurements. No significant difference in the use of Drierite, nonindicating Drierite, or Aquasorb desiccants was evident in sampling system tests. The instrumentation and methods used in this study were satisfactory for conducting emission measurements of diesel exhaust.
THE development of a practical method for producing steel cartridge cases became necessary when the critical shortage of copper made it imperative that the standard brass cases be replaced with ones made of steel. A group of manufacturers, including Buick, worked on the problem with the Ordnance Department, and a cartridge case committee was formed, consisting of representatives from both Ordnance and industry. Very successful results have accrued from this cooperative program, and, according to latest reports, steel cartridge cases in practically all calibers will soon be in volume production. This paper tells the story of how the process developed by the Buick engineers was accomplished, and describes the method in detail. The Buick process has been applied successfully to the manufacture of steel cases of the 75-mm size, which are now being produced in large quantities. Thirty-one major manufacturing operations are used in the production of these cases, the most interesting and unique ones being a series of four cold-drawing operations. These are carried out on a 750-ton double-acting press, where the cup is drawn from 6 in. to 15 in., and to the approximate form of the finished case, there being no substantial change in the diameter during the draw.
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