UANL - FIME Sistemas de Propulsión y laboratorio 1 IT-8-ACM-02-R03 Revision: 3 VALID From THE: 13 Enero de 2017 AUTONOMOUS UNIVERSITY AGAIN LEÓN FACULTY OF MECHANICAL And ELECTRICAL ENGINEERING ANALYTICAL PROGRAM FIME Name of the unit of learning: Systems of Propulsion and laboratory Weekly frequency: 3 hrs. Face-to-face hours: 42 hrs. Hours of extra work-classroom: 0 hrs. Modality: Present Academic period: Semestral Unit of learning: (X) compulsory ( ) optative Area curricular, according to the educational level: Bachelor ( ) basic Training professional (X) professional Training ( ) University general training ( ) Free election Credits UANL: 4 credits including the laboratory Date of preparation: 30/10/2016 Date of the last update: 30/10/2016 Managers of the design: Eng. Marco Polo Torres Reyna Dr. Eduardo Liceaga Castro Presentation: In this unit of learning divides in 4 phases, in the first phase will study the strengths that act in the aircraft and the thermodynamic fundamental concepts of propulsion, in the second phase, defines and analyses the parametric ideal cycle of an engine of turbo reaction, in the third phase analyses the exert of each component (diffusing, compressor, turbine and camera of combustion), finally in the fourth phase the analysis of the real parametric cycle of the engine of turbo reaction and his exert.
Transcript
UANL - FIME Sistemas de Propulsión y laboratorio
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AUTONOMOUS UNIVERSITY AGAIN LEÓN FACULTY OF MECHANICAL And ELECTRICAL ENGINEERING
ANALYTICAL PROGRAM FIME
Name of the unit of learning: Systems of Propulsion and laboratory Weekly frequency: 3 hrs. Face-to-face hours: 42 hrs. Hours of extra work-classroom: 0 hrs. Modality: Present Academic period: Semestral Unit of learning: (X) compulsory ( ) optative Area curricular, according to the educational level: Bachelor ( ) basic Training professional (X) professional Training ( ) University general training ( ) Free election Credits UANL: 4 credits including the laboratory Date of preparation: 30/10/2016 Date of the last update: 30/10/2016 Managers of the design: Eng. Marco Polo Torres Reyna Dr. Eduardo Liceaga Castro
Presentation:
In this unit of learning divides in 4 phases, in the first phase will study the strengths that act in the aircraft and the thermodynamic fundamental concepts of propulsion, in the second phase, defines and analyses the parametric ideal cycle of an engine of turbo reaction, in the third phase analyses the exert of each component (diffusing, compressor, turbine and camera of combustion), finally in the fourth phase the analysis of the real parametric cycle of the engine of turbo reaction and his exert.
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Purpose: Attain that the student develop general and specific competitions, to attain a high capacity in the solution of problems of engineering and
to his time the practice of the values promoted by the UANL, by means of the application of competitions purchased in several units of learning of basic training professional, such as: thermodynamics, processes of combustion and chemical reactions, for the analysis of the exert and characteristic of the turbines of gas.
Competitions of the graduate profile:
a. Competitions of the University General Training to which contributes this unit of learning: This unit of learning contributes to the development of the following general competitions:
Instrumental competitions:
• It applies strategies of autonomous learning in the different levels and fields of the knowledge that allow him the taking of timely and pertinent decisions in the personal fields, academician and professional.
• It uses the logical languages, formal, mathematician, iconic, verbal and no verbal of agreement to his stage of life, to comprise, interpret and express ideas, feelings, theories and currents of thought with an approach ecumenical.
• It dominates his in shape oral native language and written with correction, importance, opportunity and ethical adapting his message to the situation or context, for the transmission of ideas and scientific findings.
• Use a second language, preferably the English, with clarity and correction to communicate in daily contexts, academicians, professional and scientists.
• It uses the methods and technical of traditional investigation and of avant-garde for the development of his academic work, the exercise of his profession and the generation of knowledges.
Personal competitions and of social interaction
• Practice the values promoted by the UANL: truth, equity, honesty, freedom, solidarity, respect to the life and to the other, respect to the nature, integrity, ethical professional, justice and responsibility, in his personal and professional field to contribute to build a sustainable society.
Integrated competitions:
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• Assume the committed leadership with the social and professional needs to promote the pertinent social change.
b. Specific competitions of the graduated profile to which contributes the unit of learning:
Apply methods and technical of scientific and technological investigation, collaborating in groups of generation and application of the knowledge, for the development of projects of engineering. Generate models in mathematical language that describe the behavior of a system, phenomenon or process, by means of the approach of hypothesis, that allow him validate them by analytical methods or computational tools.
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Graphic representation
Competitions of the Unit of Instrumental
Learning
Uses the logical languages, formal, mathematician, iconic, verbal and no verbal of agreement to his stage of life, to comprise, interpret and express ideas, feelings, theories and currents of thought with an approach ecuménico.
It dominates his in shape oral native language and written with correction, importance, opportunity and ethical adapting his message to the situation or context, for the transmission of ideas and scientific findings.
Use a second language, preferably the English, with clarity and correction to communicate in daily contexts, academicians, professional and scientists.
It uses the methods and technical of traditional investigation and of avant-garde for the development of his academic work, the exercise of his profession and the generation of knowledges.
Applies strategies of autonomous learning in the different levels and fields of the knowledge that allow him the taking of timely and pertinent decisions in the personal fields, academician and professional.
Personal and of Social Interaction
Practises the values promoted by the UANL: truth, equity, honesty, freedom, solidarity, respect to the life and to the other,respect to the nature, integrity, ethical professional, justice and responsibility, in his personal and professional field to
contribute to build a sustainable society
Integrator Assume the committed leadership with the social and professional needs to promote the pertinent social change
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Thematic unit 1: Fundamentals of the systems of propulsion Particular competitions: Comprise how the systems of propulsion are involved with the forces that act in the aircraft, in addition to knowing the thermodynamic fundamentals of the systems of propulsion.
Elements of Competition
Evidences of learning
Criteria of performance Activities of learning Contents Resources
Comprise how the systems of propulsion are involved with the forces that act in the aircraft, in addition to knowing the thermodynamic fundamentals of the systems of propulsion.
It report the fundamentals of the systems of propulsion. Problems resolved of the Thematic Unit I.
Report:
• Presentation
• Spelling
• Content
• References
• Date of delivery Problems resolved:
• Procedure
• Result
Investigate and elaborate a report of the fundamentals of the systems of propulsion and show the compression of this thematic unit. Resolution of problems using the basic principles.
What is Propulsion? Engines with taking of air. I exert of the aircraft. Equation of state and conservation of mass. Equation of energy, entropy and moment of constant flow. Equation of push. Propulsive efficiency Components of an engine of turbo reaction. Brayton Cycle
Classroom of class Computer Video Projector/screen Database UANL CONRICYT Books of text Scientific articles Internet
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Thematic unit 2: Parametric Cycle Ideal of the engine of turbo reaction Particular competitions: Define the parametric cycle ideal of an engine of turbo reaction and know how the conditions of flight are involved for the calculation of the performances of the components of the engine.
Elements of Competition
Evidences of learning
Criteria of performance Activities of learning Contents Resources
Comprise the importance of the analysis of the parametric cycle of an engine first approximation for the design of an engine.
Report of the parametric cycle ideal of the engine of turbo reaction. Problems resolved of the Thematic Unit II.
Report:
• Presentation
• Spelling
• Content
• References
• Date of delivery Problems resolved:
• Procedure
• Result
Investigate and elaborate a report with the importance of the analysis of the parametric cycle. Resolution of problems using the basic principles.
Notation of the parametric cycle Design of entrances of the parametric cycle. Steps for the analysis of the parametric cycle of an engine. Assumption for the analysis of the parametric cycle ideal. Turborreactor Ideal.
Classroom of class Computer Video Projector/screen Database UANL CONRICYT Books of text Scientific articles Internet
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Thematic unit 3: Performance of the components. Particular competitions: The student will comprise the losses of efficiency in the main components of an engine of turbo reaction by diverse thermodynamic factors and the variation of the specific heats
Elements of Competition
Evidences of learning
Criteria of performance Activities of learning Contents Resources
Calculate the efficiency in the main components of an engine of turbo reaction considering the specific heats variation.
Report of the real performance of the components. Problems resolved of the Thematic Unit III.
Report:
• Presentation
• Spelling
• Content
• References
• Date of delivery Problems resolved:
• Procedure
• Result
Investigate and elaborate a report of the real performance of the components. Resolution of problems employing the basic principles.
Introduction Variation in the properties of the gas Performance of the components Recovery of nozzle and diffuser Efficiencies of compressor and turbine. Efficiency of the burner Performance of components with variable Cp.
Classroom of class Computer Video Projector/screen Database UANL CONRICYT Books of text Scientific articles Internet
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Thematic unit 4: Parametric Cycle and Analysis of the Exert of a real engine. Particular competitions: The student will apply the fundamental concepts of the engine of turbo reaction and will calculate the real parametric cycle, in addition to the analysis of performance of the engine.
Elements of Competition
Evidences of learning
Criteria of performance Activities of learning Contents Resources
Calculate the real parametric cycle of an engine of turbo reaction and make the analysis of the performance.
Report of the parametric cycle and analysis of the real perfomance of a motor. Problems resolved of the Thematic Unit IV.
Report:
• Presentation
• Spelling
• Content
• References
• Date of delivery Problems resolved:
• Procedure
• Result
Investigate and elaborate a report of the real parametric cycle and the analysis of the performance of the engine. Resolution of problems employing the basic principles.
Introduction. Estimation of the real parametric cycle of the engine of turbo reaction. Calculation of the performance of an engine of turbo reaction.
Classroom of class Computer Video Projector/screen Database UANL CONRICYT Books of text Scientific articles Internet
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Integral evaluation of processes and products (grade / summative evaluation) Evidence Grade Mid term exam 20 % Final exam 20 % Integrator product 20 % Activities of thematic unit I 10 % Activities of thematic unit II 10 % Activities of thematic unit III 10 % Activities of thematic unit IV 10 % Total 100%
Integrator product of learning: Presentation of a report and simulation of a real aircraft making a manoeuvre (straight level flight, climbing, approaching, coordinated turn or path of real flight) that evidence the skills of the student for the application of the physical principles are in an aircraft. The student will contemplate in the simulation all the physical effects presents generated by the loss of weight by fuel.
Sources of support and query: Book: Elements of Propulsion. Gas Turbines and Rockets.
Author: Jack D. Mattingly Publisher: AIAA Education series.
Book: Gas turbine Propulsion Systems
Author: Bernie MacIsaac Publisher: John Wiley & Sons
Book: Principles of Jet Propulsion and Gas Turbines
Author: Maurice Joseph Zucrow Publisher: John Wiley
o Subject: What is the thrust?
Link: https://www.grc.nasa.gov/www/k-12/airplane/thrust1.html Last review: 26 October 2016
o Subject: Programs and presentations of fundamental.
League: https://www.grc.nasa.gov/www/k-12/airplane/topics.htm Last review: 26 October 2016
Magazine: Journal of Propulsion and Power
Year: 1999 # Of magazine: 1
Month: January - February Name of the article: Performance Increases for Gas-Turbine Engines Through Combustion Inside the Turbine Author: Srignano and F. Liu
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Profile of the educational: The professor will have to have minimum degree of Aeronautical Engineering or in affine branches and preferably Mastery and/or Ph.D. with firm bases in areas of investigation applied, being honest, responsible and with an ethical. It will have to show knowledge, skill and experience in the area of Engines of Reaction, as well as a second language (Groins). Bibliographic index card of the professor: Eng. Marco Polo Torres Reyna
He studied Aeronautical Engineer (2015) in the FIME, Universidad Autónoma de Nuevo León, actually is studying the Mastery in Sciences of the Aeronautical Engineering with Dynamics of flight orientation (2017) in the FIME, UANL. He has publications in congresses. During his stay in the FIME worked in the laboratory of Systems of Propulsion (2013-2015). From January of 2016 is Professor of Partial Time of the FIME, UANL.
JEFATURA DE ACADEMIA JEFATURA DE DEPARTAMENTO
M.C. Daniel Librado Martínez Vázquez Dr. Luis Arturo Reyes Osorio
COORDINACIÓN GENERAL SUBDIRECCIÓN ACADÉMICA ACADEMICA DE AERONÁUTICA Dr. Arnulfo Treviño Cubero Dr. Ulises Matías García Pérez
