Performance Analysis and Aerodynamic Design of Axial Flow Compressors
الشريط الجانبي للمقالة
محتوى المقالة الرئيسي
الملخص
The main objective of the paper is to analyze the
performance of axial flow compressors and to generate a
systematic design approach which enables to design
subsonic flow ones. In order to investigate the validity of this
approach, the LP axial flow compressor of the RR Spey
MK511 turbofan engine is taken as an example. The design
calculations were based on thermodynamics, gas dynamics,
fluid mechanics and empirical relations. The flow is
assumed to be of two-dimensional compressible type with
constant axial and rotor blade velocities with a free-vortex
swirl distribution. Design calculations include
thermodynamic properties of the working fluid, number of
compressor performance parameters such as, stage
temperature rise and number, flow and blade angles (blade
twist), velocity triangles and relative inlet Mach number at
rotor blades tips as well as blades tip and hub diameters. A
repeated calculation is made to determine these parameters
along compressor stages. The variation of velocity whirl
components, air and blade angles, deflection and degree of
reaction from root to tip of the blades were also determined.
The twist of the blades along the blade length is set
according to the recommended values in order to obtain
smooth blade twist profile.
تفاصيل المقالة
هذا العمل مرخص بموجب Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
المراجع
Bathic, William. "Fundamentals of Gas Turbines". Jhon Wiley &
Sons, Inc, Second Edition, 1996.
Cohen H., Rogers G.F.C.,&Hill Saravanamuttio H.L.H."'Gas
Turbine Theory". Longman Group limited, Burt Harlow, Essex, U.K. 4
edition, 1996.
Hill and Peterson "Mechanics and Thermodynamics of propulsion",
nd
, Addison-Wesley Publishibg, Inc. USA, 1992.
Rolls-Royce Spey, "World Encyclopedia of Aero Engines - 5th
edition" by Bill Gunston, Sutton Publishing, 2006, p.197.
Niclas Falck "Axial Flow Compressor Mean Line Design", Thermal
Power Engineering, Energy Sources, Lund University, Sweden,
February 2008.
B.B.Raval & V.G.Virani "Aerodynamic Design of Axial Flow
Compressor", IJEDR, Volume 2, Issue 1 , ISSN: 2321-9939, 2014.
Gaddam Srikanth Ȧ, S.Srinivas Prasad , V.Mahesh Kumar Ȧ and
B.Mounica Reddy "Design Methodology of a Two Stage Axial
Compressor", International Journal of Current Engineering and
Technology, E-ISSN 2277 – 4106, P-ISSN 2347 – 5161, 2014.
Meherwan P. Boyce, "Gas turbine Engineering Handbook", Gulf
Professional Publishing, third Edition, 2006.
Ronald H Aungier, "Axial Flow Compressor: A strategy for
Aerodynamic Design and Analysis".Wiley Publication, ISBN: 978-186058-422-0,
May
Akin Keskin “Application of multi-objective optimization to axial
compressor preliminary design” Aerospace Science and Technology 10
(2006) 581–589.
Fengrui Sun “Optimum design of a subsonic axial flow compressor
stage” Applied Energy 80 (2005) 187–195. DOI: https://doi.org/10.1016/j.apenergy.2004.03.008
B.T. Lebele-Alawa, “Rotor-blades‟ profile influence on a gasturbines
compressor
effectiveness",
Applied
Energy
(2008).
Pp.494–
X.C. Zhu, “The Off-Design Performance Prediction of Axial
Compressor Based on A 2d Approach” .Journal Of Theoretical and
Applied Mechanics 51, 3, (2013). Pp. 523-531. DOI: https://doi.org/10.1007/s00466-012-0817-4
Wall R. Axial-flow compressor performance prediction. AGARDLS-83
(June):41–434.
Calvert WJ, Ginder RB. Transonic fan and compressor design.
Proc Instn Mech Engrs1999;213(C5):419–36.
Gallimore SJ. Axial-flow compressor design. Proc Instn Mech
Engrs 1999;213(C5):437–49. DOI: https://doi.org/10.1016/S0304-3975(98)00320-X
Egorov IN., "Optimization of multi-stage axial compressor in a
gas-turbine engine system". ASME paper, 92-GT-424 1992.
N. Cumpsty, "Compressor Aerodynamics", Krieger Publishing
Company,2004.