Application of the Theory of Similitude to the Design of Control Systems for Gas Turbine Engines,
Abstract
The report discusses the questions related to optimum design using the theory of similitude of automatic control systems for aircraft gas turbine engines(GTE) considered as objects with characteristics varying during flight. The equation of motion of the controlled object, expressed in terms of reduced variables, is unique for all conditions of its operation and may be represented as a graph of the 'dynamic characteristic of a GTE' that can be used as a basis to determine the required control laws. The selection of the optimal formula for the control system is done by using power complexes of GTE parameters. A foundation is provided for the principles of designing a single control system that combines higher reliability of control in the entire range of flight conditions with reliability of control.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 25, 1973
- Accession Number
- AD0764683
Entities
People
- Yu. V. Lyubomudrov
Organizations
- National Air and Space Intelligence Center