“…An energy delivery index W can be defined as in Eq. (25) to relate the compression station outlet energy delivery to the power supplied for compressing the gas.…”
Section: Surge Avoidance During Start-up and Normal Operationmentioning
confidence: 99%
“…[11] the use of pulsed air injection to control rotating stall in low speed axial flow compressors was presented and jet injection with a high order Galerkin method was studied in Ref. [25]. In Ref.…”
“…An energy delivery index W can be defined as in Eq. (25) to relate the compression station outlet energy delivery to the power supplied for compressing the gas.…”
Section: Surge Avoidance During Start-up and Normal Operationmentioning
confidence: 99%
“…[11] the use of pulsed air injection to control rotating stall in low speed axial flow compressors was presented and jet injection with a high order Galerkin method was studied in Ref. [25]. In Ref.…”
“…3 and according to Equ. (24), that the stability of the compression systems dependent on the throttle coefficient, (27) where o h is the new nominal value of the throttle position, 1 K is the gain which will eliminate the hysteresis between the steady axisymmetric flow and rotating stall. To increase the compressor limit of stability, substituting the modified throttle characteristic,…”
Section: Compressor Instability Elimination By Modifying the Throttlementioning
confidence: 99%
“…Rotating stall was controlled using pulsed air injection that is distributed around the annulus of the flow compressor [26]. Protz [27] and Yeung [28] have investigated air injection controllers, and Weigl et al [29], Protz [30], D'Andrea et al [31] have carried out successful experiments. However, most of the control-oriented studies published during the last decade employ simplified versions of an ordinary partial differential equation compressor model by Moore and Greitzer [3] because of its remarkable ability to qualitatively describe and predict compressor operation.…”
Aerodynamic instabilities due to rotating stall initiation and surge trigger in the axial flow compressors were investigated using different mathematical models. Limit of stability of the rotating stall was detected using simple model that considers transport of energy by the rotor wakes passing through the stator. Active suppression of the aerodynamic instabilities in the axial flow compressors were demonstrated using mechanical compensated system with controlled plenum simultaneously with air injection through reed valve. A nonlinear controller based on a bifurcation theory was used to design feedback control system for eliminating surge and rotating stall as well hysteresis. The bifurcation analysis was performed to determine the effect of throttle gain on the compressor limit of stability and then modifying the throttle characteristic to eliminate hysteresis and suppresses surge. The Moore-Greitzer model was extended to include the influences of the air injection on the axial flow compressors performance characteristics and to enhance the limit of stabilities of both the stall and the surge. Comparisons of the present theoretical results with the available previous experimental and theoretical results were carried out.
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