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Performance Analysis of the Integrated V2527-Engine Fan at Ground Operation

Schnell, Rainer and Ebel, Paul-Benjamin and Becker, Richard-Gregor and Schoenweitz, Dirk (2013) Performance Analysis of the Integrated V2527-Engine Fan at Ground Operation. 13th Onera-DLR Aerospace Symposium ODAS, 27.-29. Mai 2013, Palaiseau.

Full text not available from this repository.

Abstract

The paper focuses on the holistic assessment of the integrated fan stage of DLRs Advanced Technology Research Aircraft ATRA, an Airbus A320 equipped with two IAE-V2527 engines. For the entire engine and all its components, a cycle model was established in order to derive realistic operating conditions for all components. The model was validated against experimental data taken by the Electronic Engine Control (EEC) at the aircrafts last shop visit at Lufthansa Technik. Furthermore the engines nacelle and major fan components including its disk, casing, Outlet Guide Vanes (OGV) and Booster-Inlet Guide Vanes (IGV) etc. were optically scanned and transferred to surfaced based CAD models in a reverse engineering approach to obtain the geometry in a most accurate manner. This allowed for dedicated CFD studies of the fan itself and by including the nacelle its interaction with ground induced inlet distortions at realistic engine operating conditions as being derived from the cycle analysis. A mechanical model of the hollow, honeycomb structured fan blade was set up based on the information from computer tomography (CT) scans of one blade and corresponding experimental determination of the blades Eigen-Frequencies. This model allowed for the cold-to-hot transformation of the fan blade geometry under running conditions. The updated CFD results in terms of stage performance with the realistic deformed geometry will then be used to update the cycle model in an iterative manner. Furthermore, a parametric study characterizing the fan inlet flow at the nacelle entry at varying boundary conditions (e.g. cross flows, different fan mass flow rates etc.) was carried out, allowing to quantify the nacelle induced inlet distortions potentially influencing the fan performance.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Performance Analysis of the Integrated V2527-Engine Fan at Ground Operation
Authors:
AuthorsInstitution or Email of Authors
Schnell, RainerAT-FUV
Ebel, Paul-BenjaminBK
Becker, Richard-GregorAT-TRW
Schoenweitz, DirkAT-FUV
Date:May 2013
Refereed publication:Yes
Status:Published
Keywords:Turbomachinery, Fan, V2500, Aerodynamics, Cycle Analysis, FEM, Nacelle Aerodynamics
Event Title:13th Onera-DLR Aerospace Symposium ODAS
Event Location:Palaiseau
Event Type:international Conference
Event Dates:27.-29. Mai 2013
Organizer:Onera
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Virtual Engine and Validation Methods
Location: Köln-Porz , Stuttgart
Institutes and Institutions:Institute of Structures and Design > Computer Supported Component Design
Institute of Propulsion Technology > Engine
Institute of Propulsion Technology > Fan and Compressor
Deposited By: Dr.-Ing. Rainer Schnell
Deposited On:20 Jun 2013 11:06
Last Modified:20 Jun 2013 11:06

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