A comprehensive model of a novel rotating spool compressor

被引:19
|
作者
Bradshaw, Craig R. [1 ]
Groll, Eckhard A. [2 ]
机构
[1] Torad Engn, Alpharetta, GA 30004 USA
[2] Purdue Univ, Herrick Labs, W Lafayette, IN 47907 USA
关键词
Spool compressor; Comprehensive model; Novel compressor; Geometry model; ROTARY-COMPRESSOR;
D O I
10.1016/j.ijrefrig.2013.07.004
中图分类号
O414.1 [热力学];
学科分类号
摘要
A comprehensive simulation model of a novel rotating spool compressor is presented. The spool compressor provides a new rotary compression mechanism with easily manufactured components. A detailed analytical geometry model of the spool compressor is presented, which includes the geometry of the vane. This geometry model is included in an overall comprehensive compressor model that includes sub-models for friction, leakage, and heat transfer. The results of the comprehensive model were validated using experimental data from a prototype compressor. The prototype compressor has an overall displacement of 23.9 cm(3), and was operated using R410A as the working fluid. The model predicts the volumetric efficiency, discharge temperature, and shaft power of the prototype compressor to within 3.13% MAE, 16.5 K and -13.2 W average deviation, respectively. The trends and spread in the data indicate that additional effort should be focused on the operation of the active sealing elements within the compressor. (C) 2013 Elsevier Ltd and IIR. All rights reserved.
引用
收藏
页码:1974 / 1981
页数:8
相关论文
共 50 条
  • [21] A COMPREHENSIVE ANALYTICAL SHOCK LOSS MODEL FOR AXIAL COMPRESSOR CASCADES
    Banjac, Milan
    Savanovic, Teodora
    Petkovic, Djordje
    Petrovic, Milan V.
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2A, 2021,
  • [22] THEORETICAL MODEL FOR ROTATING STALL IN THE VANELESS DIFFUSER OF A CENTRIFUGAL COMPRESSOR.
    Frigne, P.
    Van den Braembussche, R.
    Journal of Engineering for Gas Turbines and Power, 1985, 107 (02) : 507 - 513
  • [23] A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades
    Banjac, Milan
    Savanovic, Teodora
    Petkovic, Djordje
    Petrovic, Milan, V
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (09):
  • [24] RADIAL COMPRESSOR WITH ROTATING DIFFUSER
    JAEKN, M
    CHEMIKER-ZEITUNG, 1970, 94 (21): : 843 - &
  • [25] COMPRESSOR-TURBINE MATCHING OF 2-SPOOL TURBO-PROPS
    MORLEY, AW
    AERONAUTICAL QUARTERLY, 1958, 9 (01): : 17 - 33
  • [26] Theoretical study of a novel refrigeration compressor - Part II: Performance of a rotating discharge valve in the revolving vane (RV) compressor
    Teh, Y. L.
    Ooi, K. T.
    Djamari, D. Wibowo
    INTERNATIONAL JOURNAL OF REFRIGERATION-REVUE INTERNATIONALE DU FROID, 2009, 32 (05): : 1103 - 1111
  • [27] Optimization of a three spool axial compressor to increase the efficiency of a gas turbine engine
    Marchukov, Evgenii
    Egorov, Igor
    Popov, Grigorii
    Baturin, Oleg
    Goriachkin, Evgenii
    Novikova, Yulia
    INTERNATIONAL CONFERENCE ON COMPRESSORS AND THEIR SYSTEMS 2019, 2019, 604
  • [28] Core-compressor rotating stall simulation with a multi-bladerow model
    Vahdati, M
    Sayma, AI
    Imregun, M
    UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES, 2006, : 313 - +
  • [29] An enhanced compressor map extension method suited for spool speeds down to 1%
    Kurzke, Joachim
    JOURNAL OF THE GLOBAL POWER AND PROPULSION SOCIETY, 2024, 8 : 215 - 226
  • [30] A THEORETICAL-MODEL FOR ROTATING STALL IN THE VANELESS DIFFUSER OF A CENTRIFUGAL-COMPRESSOR
    FRIGNE, P
    VANDENBRAEMBUSSCHE, R
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (02): : 507 - 513