Feasibility of Rapid Prototyping Manufacturing of Multi-Probe for Measuring Total Pressures at High Temperatures = Viabilidad de la Fabricación por Prototipado Rápido de una Multisonda para la Medida de Presiones Totales a Altas Temperaturas

Rodríguez Monroy, Carlos and Calvo Narvaez, Felix (2015). Feasibility of Rapid Prototyping Manufacturing of Multi-Probe for Measuring Total Pressures at High Temperatures = Viabilidad de la Fabricación por Prototipado Rápido de una Multisonda para la Medida de Presiones Totales a Altas Temperaturas. In: "13th LACCEI Annual International Conference: “Engineering Education Facing the Grand Challenges, What Are We Doing?”", July 29 - 31, 2015, Santo Domingo, República Dominicana. ISBN 13 978-0-9822896-8-6. pp. 1-8.

Description

Title: Feasibility of Rapid Prototyping Manufacturing of Multi-Probe for Measuring Total Pressures at High Temperatures = Viabilidad de la Fabricación por Prototipado Rápido de una Multisonda para la Medida de Presiones Totales a Altas Temperaturas
Author/s:
  • Rodríguez Monroy, Carlos
  • Calvo Narvaez, Felix
Item Type: Presentation at Congress or Conference (Article)
Event Title: 13th LACCEI Annual International Conference: “Engineering Education Facing the Grand Challenges, What Are We Doing?”
Event Dates: July 29 - 31, 2015
Event Location: Santo Domingo, República Dominicana
Title of Book: 13th LACCEI Annual International Conference: “Engineering Education Facing the Grand Challenges, What Are We Doing?”
Date: 2015
ISBN: 13 978-0-9822896-8-6
Subjects:
Freetext Keywords: Rapid prototyping, laser sintering, Multiprobe, aircraft engines, total pressures
Faculty: E.T.S.I. Industriales (UPM)
Department: Ingeniería de Organización, Administración de Empresas y Estadística
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

The variation in total pressure along the turbine engine is essential both to determine its efficiency to understand its operation. Due to rising temperatures in the combustion chamber and turbine aircraft engines latest generation of the development of probes capable of withstanding the high temperatures of these is necessary. Designing a multiprobe by laser sintering is novel by reduced meter size, choosing its shape, and manufacturing it from a single piece. 7 sensors are placed on a given turbine at various radial and circumferential positions to find the flow pressure profile section in position. It has demonstrated the technical feasibility, as theoretically design meets the structural and heat transfer conditions, and thus has been validated as microstructural dimensional model. Considering the economic viability of the proposed alternative method of manufacture is not so obvious, if the costs of manufacturing processes are considered. Keywords? Rapid prototyping, laser sintering, Multiprobe, aircraft engines, total pressures.

More information

Item ID: 42298
DC Identifier: http://oa.upm.es/42298/
OAI Identifier: oai:oa.upm.es:42298
Official URL: http://www.laccei.org/index.php
Deposited by: Memoria Investigacion
Deposited on: 29 Jun 2016 17:44
Last Modified: 02 Aug 2016 08:08
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