Development and Optimization of Screw Machines With a Simulation Model—Part I: Profile Generation

Author:

Stosˇic´ N.1,Hanjalic´ K.2

Affiliation:

1. Department of Mechanical Engineering and Aeronautics, City University, London EC1V 0HB, U.K.

2. Delft University of Technology, Lorentzweg 1, 2628 CJ Delft, The Netherlands

Abstract

This paper presents a method for the design of twin screw compressors and expanders, which is based on a differential algorithm for defining the rotor profiles and an analytical model of the fluid flow and thermodynamic processes within the machine. Part I of the paper describes the algorithm for screw rotor profile generation. It demonstrates the conjugacy condition which, when solved explicitly, enables a variety of primary arcs to be defined either analytically or by discrete point curves. Its use greatly simplifies the design since only primary arcs need to be specified and these can be located on either the main or gate rotor or even on any other rotor including a rack, which is a rotor of infinite radius. Secondary arcs are then generated automatically from this. By such means any profile combination may be considered. The most efficient were obtained from a combined rotor-rack generation procedure. An example of this combination is given which produces a rotor profile with stiff lobes and a higher throughput than any other known type. Part II describes a mathematical model of the compression and expansion processes within positive displacement machines which has been well proven in its use for the design of reciprocating and screw compressors and screw expanders.

Publisher

ASME International

Subject

Mechanical Engineering

Reference29 articles.

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2. Andreev, P. A., 1961, Vintovie kompressornie mashinii (Screw Compression Machines), SUDPROM Leninngrad.

3. Arbon, M., 1994, “The Design and Application of Rotary Twin-shfat Compressors in the Oil and Gas Process Industry,” MEP London.

4. Astberg A., 1982, Patent GB 2092676B.

5. Bammert K., 1979, Patent Application FRG 2911415.

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