Clinical Psychology and Well-Being: Approaches, Applications and Issues.
Manned and unmanned VTOL rotorcraft maneuvering in low-level flight, take-offs and landing, and in confined landing zones LZ often lack situational awareness of obstacles in the rear hemisphere of the aircraft, especially at night and in degraded visual environments DVE.
Aircraft are typically equipped with forward and down-ward looking sensors, but lack full degree coverage to detect and alert the crew and aircraft of obstacles as the aircraft is maneuvered in LZs and nap-of-the-earth NOE flight. The objective is to provide the aircrews and remote operators with sufficient warning to avoid obstacles in the rear hemisphere of the aircraft during turns and rearward maneuvers within threshold ft and objective ft radius of main and tail rotor tips and to provide an automated"stop"of the maneuver to the aircraft flight controls of immediate threat obstacles.
The technical approach should provide at a minimum sufficient warning to the operator of obstacles feet from the tail rotor, tailboom and rear half of the main rotor disk, such that the aircraft is not inadvertently maneuvered into the obstacle.
For future unmanned systems the concept is to provide suitable cuing for the UAS to autonomously avoid obstacles in the rear hemisphere while maneuvering into or out of a pick-up or drop zone. The study should include: The study should also include a plan for any further required development, and life-cycle cost estimates.
Deliverable is the feasibility study as described above. This phase should include: A detailed project plan and test plan should be developed for integration and demonstration of the hardware and software. Hardware and software must be certified as airworthy for experimental purposes, and proper certification obtained from the FAA for UAS experimental testing.
Objective is to demonstrate a TRL 6 suitable for transition to a PM for final development and acquisition. Deliverables include the prototype hardware and software, technical data, test results, and final project report. Develop a flight qualified, airworthy prototype design suitable for installation on any specified VTOL aircraft.
Design, fabricate, acquire and integrate hardware to be installed and tested on the VTOL aircraft. Demonstrate operational suitability, reliability, and safety of the prototype to adequately demonstrate a TRL 8 for acquisition. Commercial applications would include commercial UAS and commercial helicopters, especially those performing logistical services, transmission line and pipeline monitoring services, cargo delivery, emergency medical services and other rotorcraft that require the capability to operate and land in urban areas or confined sites with complex terrain and unknown obstacles.
Waveform design principles for automotive radar systems: Research activities in automotive radar: The Fourth International Kharkov Symposium on, Design considerations and technology assessment of phased-array antenna systems with RF MEMS for automotive radar applications: Gas turbine metallic combustor liner walls, along with turbine blades, vanes and shrouds are typically coated with an intermediate bond coat and a porous, ceramic-based thermal barrier coating TBC system to enable effective high temperature operation.
In the case of conventional yittria-stabilized zirconia TBCs, the coating structure is columnar, which allows the CMAS material to wick between the columns.
This could be accomplished by a completely different coating micro-structure that is not columnar and is resistant to CMAS or by adding a protective layer to more conventional TBCs that stops the CMAS from getting into the columnar structure.
The small business is encouraged to work with and establish a clear transition path with a turbine engine manufacturer. The optimized coating technology shall be applied to hot section component s for full engine test validation to TRL 6. Validation will include a sand test demonstration with appropriate cyclic content.
The resulting technology will enable significantly enhanced durability of hot section components of future advanced engines with high turbine inlet temperatures operating in sandy environments. Both military and commercial aircraft applications are likely to encounter such an environment and thereby will derive benefit from this technology.
Journal of Thermal Spray Technology. Materials Science and Engineering A. Grant, Stephan Krmer, Jan P.
Develop and validate advanced, low cost manufacturing methods such as water jet drilling or Direct Metal Laser Sintering DMLS to effectively manufacture advanced combustor liners with angled and shaped effusion film cooling holes. Small angled holes aka effusion are used to provide effective film cooling on gas turbine combustor liners, comprised of thermal barrier coated TBC sheet metal.
The potential exists to shape effusion cooling holes to further improve the film cooling effectiveness.
Current effusion holes are typically laser drilled into the liner.LEISA seeks to combine indigenous and scientific knowledge and to influence policy formulation to create a conducive environment for its further development.
LEISA is a concept, an approach and a. International Conference on Enterprise Information Systems, Main Topic Areas: Databases and Information Systems Integration, Artificial Intelligence and Decision Support Systems, Information Systems Analysis and Specification, Software Agents and Internet Computing, Human-Computer Interaction the system's operation details and some.
Human formulation has different requirements than animal formulation. A comparison between animal and human formulation strategies is presented.
In conclusion, for non-BCS 1 compds., the right-first-time polymorph and formulation selection ensures consistent pharmacokinetic performance and avoids bridging BA/BE studies.
Upon formulation, solutions will be administered in a manner compatible with the dosage formulation and in such amount as is therapeutically effective.
The formulations are easily administered in a variety of dosage forms, such as the type of injectable solutions described above, but drug release capsules and the like can also be employed.
May 27, · Method for applying environmental-resistant MCrAlY coatings on gas turbine components (LPPS) or electron beam physical vapor deposition (EBPVD).
some examples of heat treatments are described below for applications in which such a treatment is desired or necessary. professionals in microlithography, nanotechnology, and related fields. The SPIE (LPPs), to a description of prominent DPP and LPP systematic formulation, physical insight into emerging ideas, as well as a system-level view of the parameter tolerances required in.