Sentence examples for maximum cycle pressure from inspiring English sources

Its effect on maximum cycle pressure and temperature must be studied as they represent important parameters in the design of engine's different parts.

These operating ranges are as follows: minimum cycle temperature ranges between 302 and 315 K, maximum cycle temperature ranges between 1,320 and 1360 K, maximum cycle pressure ranges between 1.449 and 2.830 MPa, and conductance of the heat exchanger ranges between 20.7 and 29.6 kW/K.

These operating ranges are minimum cycle temperature ranges between 302 and 315 K, maximum cycle temperature ranges between 1,320 and 1,360 K, maximum cycle pressure ranges between 1.449 and 2.830 MPa, and conductance of the heat exchanger ranges between 20.7 and 29.6 kW/K.

Compared to the case of a constant compression ratio, the increase in maximum cycle pressure is about 0.53 MPa at 1,500 rpm and 0.55 MPa at 2,460 rpm passing through 0 MPa at both 1,900 and 2,800 rpm with variable compression ratio.

Table 3 Simultaneously optimum operating design parameters to achieve optimum performance parameters of an irreversible gas turbine Brayton cycle Design parameters Optimum range Compressor inlet air temperature, T1, K 302 to 315 Maximum cycle temperature, T6, K 1,340 to 1,360 Maximum cycle pressure P4, kPa 1,440 to 2,830 Heat exchanger conductance, UA, kW/K 20.7 to 29.6.

Results show that the thermal efficiency improves with a decrease in minimum cycle temperature and with increase in maximum cycle temperature and pressure.

The effect of maximum cycle temperature on the optimum pressure ratio is negligible for lower values of minimum cycle temperature and maximum pressure, and the effect becomes significant with an increase in these parameters.

Moreover, the effects of the important operating parameters, including the maximum cycle temperature, environmental temperature and condenser pressure on the optimum pressure were investigated.

Optimal values for Brayton cycle pressure ratio, concentration ratio of the parabolic dish collector, and maximum temperature ratio of the Brayton cycle are obtained corresponding to the optimal efficiency of the coupled system.

The effects of the engine design and operating parameters on the general and maximum performances of the DACE have been investigated with respect to the variation of the cycle pressure ratio and cycle temperature ratio in the CTM section.

The efficiency of the coupled system is expressed in terms of three parameters namely the Brayton cycle pressure ratio, the concentration ratio of the parabolic dish collector, and the maximum temperature ratio of the Brayton cycle.