Axial compressor

About: Axial compressor is a research topic. Over the lifetime, 12035 publications have been published within this topic receiving 127766 citations.

Modeling and control of compressor flow instabilities

Abstract: Compressors are widely used for the pressurization of fluids. Applications involve air compression for use in aircraft engines and pressurization and transportation of gas in the process and chemical industries. The article focuses on two commonly used types of continuous flow compressors: the axial compressor, where the gaseous fluid is processed in a direction parallel to the rotational axis, and the radial or centrifugal compressor, where the pressurized fluid leaves the compressor in a direction perpendicular to the rotational axis. In these machines, the entering fluid is pressurized by first accelerating it via the kinetic energy imparted in the rotors and then converting the kinetic energy into potential energy by decelerating the fluid in diverging channels. Toward low mass flows, stable operation of axial and radial compressors is constrained by two aerodynamic flow instabilities: rotating stall and surge. The article gives an overview of the current state of modeling and control of these instabilities.

Turbofan gas turbine engine

Abstract: A turbofan gas turbine engine comprising in axial flow series a fan, a booster compressor and a core engine is provided with a diffuser The diffuser is positioned axially between the booster compressor and the compressor of the core engine to efficiently diffuse the air from the fan to the compressor of the core engine The diffuser comprises a plurality of circumferentially arranged geodesic pipe diffusers, the pipe diffusers extend axially and radially and the outlets of the pipe diffusers are displaced circumferentially by an angle of between 20° and 60° with respect to the inlets of the pipe diffusers The geodesic pipe diffusers allows the airflow between the fan and the core engine to be diffused adequately without compromising the efficiency of the core engine, or the high mass flow rate of the fan and also minimizes the length, weight and drag of the gas turbine engine

Wind turbine with mixers and ejectors

Abstract: A method is disclosed for improving the operational effectiveness and efficiency of wind turbines. Applicants' preferred method comprises: generating a level of power over the Betz limit for an axial flow wind turbine, of the type having a turbine shroud with a flared inlet and an impeller downstream having a ring of impeller blades, by receiving and directing a primary air stream of ambient air into the flared inlet and through the turbine shroud; rotating the impeller inside the shroud by the primary air stream, whereby the primary air stream transfers energy to the impeller; entraining and mixing a secondary flow stream of ambient air exclusively with the primary air stream, which has passed through the impeller, via a mixer and an ejector sequentially downstream of the impeller. Unlike gas turbine mixers and ejectors which also mix with hot core exhaust gases, Applicants' preferred method entrains and mixes ambient air (i.e., wind) exclusively with lower energy air (i.e., partially spent air) which has passed through a turbine shroud and rotor. Applicant's method further comprises harnessing the power of the primary air stream to produce mechanical energy while exceeding the Betz limit for operational efficiency of the axial flow wind turbine over a non-anomalous period.