The relationship between the circumferential velocity and energy losses in the flow part of the inflow turbine with partial blading of the runner

. Low-consumption turbomachines are devices that play an important role in the drive of various units in the field of shipbuilding, aircraft engineering and other branches of heavy engineering. They have some advantages over a high-average power turbine. The largest number of low-consumption turbomachines are made partial, i


Introduction
The vast majority of low-consumption marine turbomachines are manufactured with partial intake -partial.This is due to a number of advantages compared to the use of small full-size underwater turbines.The paper considers the very principle of a turbine with partial blading of the runner (TPBR) without reference to the thermodynamic properties of the working fluid.Lowcost marine turbines that can be considered in this study, including steam turbines, gas turbines, have their advantages and limitations.For example, steam turbines have high efficiency and good reliability, but they require large dimensions and a long time to heat.Gas turbines, on the other hand, are compact and can quickly achieve operating parameters, but their efficiency may be lower, especially at low loads.Therefore, the choice of turbine type should be based on specific requirements and operating conditions [1][2][3][4].
The optimal choice will allow achieving high efficiency of utilization turbo generators, which will lead to a reduction in fuel consumption and material costs in marine engines [5].The use of utilization turbogenerators in collaboration with internal combustion engines is one of the measures that can improve the efficiency of marine engines.This is an important step in the development of marine energy, which will help reduce the negative impact on the environment and ensure more efficient use of resources [6].
The main graphs characterizing the efficiency of turbine stages that are found in the scientific literature are graphs of the dependence of the efficiency coefficient on u 1 /C 0 .This parameter is the main speed characteristic of the stage.According to this parameter, the optimum point of kinetic energy losses, the velocity coefficient of the nozzle diaphragm and the runner are also fixed.Determining the optimal operating mode of the turbine stage while obtaining maximum efficiency with minimal kinetic energy losses is an urgent topic for research.

Goals and objectives of the study
The purpose of this study is to obtain polynomial dependences of energy losses in the flow part of the nozzle diaphragm and runner from the main speed characteristic of the u 1 /C 0 stage.
Research objectives: -based on previous numerical experiments conducted in this field [7][8][9].The loss coefficients in the nozzle diaphragm and runner are determined; -the method of mathematical approximation determines the polynomial dependences of kinetic energy losses on partiality and u 1 /C 0 ; -comparison of the values of the velocity coefficients of the nozzle diaphragm and runner obtained numerically with the result of the obtained mathematical dependencies.
The article [7] examines the study of models in which the velocity coefficients of nozzle diaphragm (ND) and runner (R) are determined based on experimental data.However, using a numerical experiment, it is possible to identify the distinctive features of the flow in these models and decide on the need for a semi-experimental study of the flow characteristics in ND and R using a simulation bench.Such a study was carried out in a scientific paper [8] on a simulation stand using the ANSYS CFX software.In Fig. 1 shows one of the stages of an inflow low-consumption TPBR.
The simulation of gas dynamic processes occurring in the turbine stage in the study was carried out using the ANSYS Workbench software package [9].With the help of this complex, a three-dimensional model of the turbine stage with varying degrees of impeller damping was created.Using the finite element method, a computational grid was generated, a computational model was created, and boundary conditions for a numerical experiment were set.The results of the study In [7], a TPBR was studied at various degrees of partial R. The values of the velocity coefficient ND and the velocity coefficient R were obtained.The velocity coefficients of ND and R with the energy loss coefficients in the flow part of ND and R have a cer-tain interdependence expressed by the formulas [8].Fig. 2 shows the dependences of the loss coefficients in the flow part of the ND for the stage in the range of ε from 0.059 to 1.00 and π t from 1.5 to 2.5 from u 1 /C 0 [10,11].The graphs of the dependence of the loss coefficient in the flow part of ND are a graphical representation of energy losses, which can be used to create polynomials expressing the dependence of ζ ND on the parameters u 1 /C 0 and ε.The loss coefficient in ND can be expressed as a function of u 1 /C 0 has the general form:

Vestnik of Astrakhan
For each degree of partiality in the range from 0.059 to 1.00, the polynomial has coefficients shown in Tables 1-3 [12].A mathematical model that allows us to determine the loss coefficient in the flow part of the ND depending on two factors (ε and u 1 /C 0 ) is presented in the form of a two-parameter dependence ζ ND = f(ε, u 1 /C 0 ), for each π t .
A graphical representation of the two-parameter dependence ζ ND = f(ε, u 1 /C 0 ), with π t = 1.5 is shown in Fig. 3.This model makes it possible to more accurately estimate the value of ζ ND for various combinations of the values of ε and u 1 /C 0 .Similarly, the empirical dependences for the loss coefficient in the runner are determined (Fig. 4) [13].The loss coefficient in R can also be expressed as a function u 1 /C 0 has the general form: For each degree of partiality in the range from 0.059 to 1.00, the polynomial has coefficients shown in Tables 4-6.In general, the analysis of the dependence graphs presented in Fig. 4 shows the possibility of obtaining cubic two-parameter polynomials ζ R = f(ε, u 1 /C 0 ).
A graphical representation of the two-parameter dependence ζ R = f(ε, u 1 /C 0 ), with π t = 1.5 is shown in Fig. 5.The adequacy of any mathematical model must be verified by a physical experiment.Due to the lack of results of a physical experiment on the energy loss coefficients in the flow part of the runner and nozzle diaphragm for the stage under study, the adequacy of the polynomial dependence can be performed using such an integral characteristic as efficiency.
When introducing the obtained energy loss dependencies into the existing mathematical model, the deviation of the internal efficiency between the calculated and the obtained input of the physical experiment is no more than 2.5%, which does not exceed the experimental error.

Conclusion
In the course of the study, the following tasks were completed and the relevant conclusions were obtained: -based on previous studies, graphs of the dependence of energy losses in the flow part of ND and R on u 1 /C 0 were constructed; -using mathematical approximation methods, mathematical dependences of energy losses in were obtained for each degree of partiality ζ ND = f(ε, u 1 /C 0 ) and ζ R = f(ε, u 1 /C 0 ); -the obtained polynomial dependencies can be used to calculate the flow part from a turbine stage of this type and will allow modeling the parameters for further improvement.

Fig. 1 .
Fig. 1.Diagram (a) and three-dimensional model (b) of a low-flow turbine stage

Fig. 2 .
Fig. 2. Two-dimensional dependence of the loss coefficient in the flow part of ND on u 1 /C 0 with a degree of partiality ε from 0.059 to 1.00: a -by π t = 1.5; b -by π t = 2.0; c -by π t = 2.5

Fig. 3 .
Fig. 3. Three-dimensional dependence of the loss coefficient in the flow part of the ND on u 1 /C 0 and the degree of partiality ε, with π t = 1.5

Fig. 4 .
Fig. 4. Two-dimensional dependence of the loss coefficient in the flow part of R on u 1 /C 0 with a degree of partiality ε from 0.059 to 1.00: a -by π t = 1.5; b -by π t = 2.0; c -by π t = 2.5

Fig. 5 .
Fig. 5. Three-dimensional dependence of the loss coefficient in the flow part of the R on u 1 /C 0 and the degree of partiality ε, with π t = 1.5