Centrifugal Compressor LEI ZHOU MMAE UCF. Spec. of top cycle compressor Pr=2.42 Working fluid: Neon Mass flow rate: 0.51 kg/s Inlet pressure: 2 atm Inlet.

Slides:



Advertisements
Similar presentations
1 Optimal Control of Chiller Condenser Sub-cooling, Compressor Speed, Tower Fan and Pump Speeds, and IGV Omer Qureshi, Hassan Javed & Peter Armstrong,
Advertisements

Entropy balance for Open Systems
LESSON TEN. AIR AND EXHAUST SYSTEMS AND TURBOCHARGERS.
Jet Engine Design Idealized air-standard Brayton cycle
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
Thermodynamics Design of 4- stage Helium compressor L. Zhou MMAE, UCF.
Thermal System Modeling and Co-Simulation with All-Electric Ship Hybrid Power System with All-Electric Ship Hybrid Power System Ruixian Fang 1, Wei Jiang.
ENERGY CONVERSION ES 832a Eric Savory Lecture 11 – A small-scale power plant worked example Department of Mechanical.
Pumps, Compressors, Fans, Ejectors and Expanders
Design Steps : Centrifugal Compressors P M V Subbarao Professor Mechanical Engineering Department A Practice of Progressive Detailing…..
EXERCISE 1 CHAPTER 11.
Gas Turbine engines.
Entropy Physics 313 Professor Lee Carkner Lecture 17.
GAS TURBINE POWER PLANTS
Shaft Power Cycles Ideal cycles Assumptions:
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lecture 29 The Vapor Compression Refrigeration (VCR) Cycle.
EGR 334 Thermodynamics Chapter 9: Sections 7-8
Gas Turbines By: Katie Steddenbenz.
Reciprocating Compressor
Air Compressors.
Examples 1.A single-acting reciprocating compressor induces 1 m 3 of air per minute at b, 15 o C, and delivers it at 7 b. Compression follows pv.
0/11TU Dresden – CERN FCC – Sept 2014 Nelium as Refrigerant for the Beam Screen and Current Lead Cooling of the FCC Fakultaet Maschinenwesen, Institut.
Chap. 3 (Sec. 3-5 to End of Chapter) Mass Flow Rate =  A V (kg/s) Volume Flow Rate = A V (m 3 /s) V = velocity.
Gas Power Cycle - Jet Propulsion Technology, A Case Study
Operation and Maintenance
Vapor and Combined Power Cycles (2)
MINIATURE ENGINEERING SYSTEMS GROUP ( Reverse Turbo Brayton Cycle CryoCooler Development for Liquid Hydrogen Systems.
Unit 4 Exercise – Gas Vapour and Combined Power Cycle
ENTC-370PROF. ALVARADO1 LAB 8: Steam Turbine (Rankine Cycle Experiment) ENTC
Plant Utility System (TKK-2210) 14/15 Semester 4 Instructor: Rama Oktavian Office Hr.: M-F
MINIATURE JOULE-THOMSON CRYOCOOLERS FOR PROPELLENT MANAGEMENT TASK I: Thermodynamic Cycle Analysis and System Optimization Presented by  K.V.Krishna Murty.
Doctoral Degree Defense Defender: Lei Zhou Advisor: Dr. Louis C. Chow Dr. Jay Kapat Committee members: Dr. Louis C. Chow; Dr. Jay Kapat; Dr. Q. Chen;
REVERSE TURBO BRAYTON CYCLE CRYOCOOLER DEVELOPMENT FOR LIQUID HYDROGEN SYSTEMS ( (Department.
Last Time Where did all these equations come from?
Analysis of Axial & Centrifugal Compressors To be Selected as per Specific Speed of Applications…. P M V Subbarao Professor Mechanical Engineering Department.

BCWC Water-cooled water chillers with centrifugal compressor/s
Distributed 2-stage RTBC LH 2 Pipeline Cryocooler System Design LEI ZHOU MMAE UCF.
CENTRIFUGAL PUMP Module 3.2 Vertical Pump Construction
DRAFT. Introduction  Mechanical Power Reciprocating Engines Turbines Turbines are compact machines (high power to weight ratio, having less balancing.
Gas dynamics of Real Combustion in Turbo Combustor P M V Subbarao Professor Mechanical Engineering Department Make Sure that design is Acceptable to Gas.
MINIATURE JOULE-THOMSON CRYOCOOLERS FOR PROPELLENT MANAGEMENT
ENERGY CONVERSION MME 9617A Eric Savory Lecture 10 – Analyzing a complete plant: Energy conversion cycles Department.
Vapor compression cycle performance. 1- Effect of evaporation pressure “ or temperature” for the following figs: R-22, 4.5% clearance, 50 L/s displacement.
Miniature Engineering Systems Group Two-Stage Cryocooler Development for Liquid Hydrogen Systems.
Issues about the full scale thermosiphon (TSP ) D. Giugni Thermosiphon Review III, May 28 th 2010 D. GiugniThermosiphon Review III, May
Single Stage Centrifugal Compressor Development Kevin Finney Ray Zhou Xiaoyi Li Krishna Murty Jinying Zhu Brian Gulliver Dipjyoti Acharya July 23, 2003.
1.8 K cycle and specificities CC: - 3D wheels - Bearings (300K) HX: - Very Low Pressure “Mixed” Compression P ratio ≈ 80 HX Stainless Steel Plate Axial-centrifugal.
Status of the Marco chiller and Marco capacity analyses Bart Verlaat, Lukas Zwalinski, Maciej Osterga, Jan Godlewski MPI Munich,1 March.
“THERMODYNAMIC AND HEAT TRANSFER” University of Rome – Tor Vergata Faculty of Engineering – Department of Industrial Engineering Accademic Year
Gas Movers and Compressors Fans Centrifugal blowers and compressors Rotary blowers and compressors Reciprocating compressors Ejectors Discharge pressure.
L.J.INSTITUTE OF ENGINEERING AND TECHNOLOGY compressors Shah Aadishkumar Aileshbhai (enrollment no ) (div A roll no. 55) Guided by Mr.hemangsir.
Closed Brayton Cycle Power Conversion Design James C. Conklin 18 February 2004
Advantages of Rotating Machines Less balancing problems Low lubricating oil consumption Higher reliability.
Gas Power Cycles.
PNEUMATICS Chapter 3 ROTARY COMPRESSORS
BRAYTON CYCLE AND EFFECT OF INTERCOOLING , REHEAT AND REGENRATION
Unit 61: Engineering Thermodynamics
TURBO POWER Turbine Technology
Aspen Hysys V8.8: Tutorial 4
Unit 2 Aircraft Propulsion
Power Plant Technology Combined Cycle and Renewable Energy Power Systems (Assignment 1) by Mohamad Firdaus Basrawi, Dr. (Eng) Mechanical Engineering Faculty.
Compound VCRS.
Date of download: 12/28/2017 Copyright © ASME. All rights reserved.
Power Plant Technology Steam and Gas Cycle Power Plant (Assignment 2)
ILC Experimental Hall Cryogenics An Overview
By : Jagdeep Sangwan The Vapor Compression Refrigeration (VCR) Cycle.
ENERGY CONVERSION ES 832a Eric Savory
ESR2 Process Cycle Design
ESR2 Process Cycle Design
Presentation transcript:

Centrifugal Compressor LEI ZHOU MMAE UCF

Spec. of top cycle compressor Pr=2.42 Working fluid: Neon Mass flow rate: 0.51 kg/s Inlet pressure: 2 atm Inlet temperature: 310K Outlet pressure: 4.84 atm Outlet Temperature: 365K Shaft power: 85 kW

Preliminary design of top cycle compressor Impeller size: 10 cm Shaft power: 85 kW Revolution speed per minute(RPM): 50K Heat sink of intercooler: 36 kW Heat sink of 2 nd stage: 38 kW Stage efficiency: 83%

Possible motor/compressor Turbocor integrated motor/compressor –R134a 2-stage centrifugal compressor –Oil-free –100 kW motor –Compact design –High reliability

Possible motor/compressor Capstone microturbine –Single stage centrifugal compressor –30 kW compression power –Compact –Oil-free

Turbo expander Very low temperature turbo expander (turbo expander of bottom cycle) –Helium expander –Expansion from 20K to 15K –Impeller size: 3 cm –Mass flow rate: 49 g/s –Power: 1.5 kW