BAA requirements, efforts to be made to include "proposed framework preliminary identification of potential small-scale applications, scalability evaluation of future large-scale application of high-M number of these technologies."
BAA also seek to meet VAATE targets to 2000 as the baseline, a large turbofan engine, the power weight ratio increased 200%, 20% reduction in fuel consumption and development, acquisition, cost reduction of 60% to maintain the concept of a very efficient engine capacity design.
Other special research tasks include investigating whether existing UAV demonstrator engine can be upgraded in order to improve fuel efficiency, increase extraction power driver loads, Peugeot Cartridge and improve cost-effectiveness.
Advice, the development of an air-air heat exchanger cooling the cooling air, which can be mounted on a turbine engine air flow path, the minimum pressure loss and cooling aircraft engine temperature exceeds 399oC (750oF) systems.
Also sought for "harsh node" hot zone (smart nodes) and - conceptual design "of the engine area (engine-area) communication network" distributed control system. The study will determine whether "with a system on a chip" (system on a chip) node requires 0.15 micron fabrication process.
Also, in order to analyze the development of the new engine design tools and new probabilistic methods used to improve engine performance, cost and reliability for the purpose of quantification of uncertainty, BAA called for forming a government, university and industry researchers alliance.
No comments:
Post a Comment