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  4. Investigation of a force-guided assembly strategy for radial mounting of jet engine blades
 
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Investigation of a force-guided assembly strategy for radial mounting of jet engine blades

Publikationstyp
Conference Paper
Date Issued
2019
Sprache
English
Author(s)
Dammann, Maik  orcid-logo
Schüppstuhl, Thorsten  orcid-logo
Institut
Flugzeug-Produktionstechnik M-23  
TORE-URI
http://hdl.handle.net/11420/4411
Start Page
187
End Page
196
Citation
In: Schüppstuhl T., Tracht K., Roßmann J. (eds) Tagungsband des 4. Kongresses Montage Handhabung Industrieroboter. Springer Vieweg, Berlin, Heidelberg. 2019
Contribution to Conference
MHI-Fachkolloquium 2019  
Publisher DOI
10.1007/978-3-662-59317-2_19
Publisher
Springer Vieweg
Increasing air traffic and growing pressure on costs in aviation MRO, especially for jet engines, demand for an increase of process efficiency. While research concentrates on inspection and repair methods, the potential for automated reassembly is thereby mostly neglected. An approach for automated assembly of compressor and turbine blades is introduced in [1]. Part of this approach is a force-guided assembly, which is performed by an industrial robot. The aim of this force-guidance is to compensate positioning deviations, which can occur at different steps throughout the assembly process. Furthermore, sticking of blades during tangential movement, as a consequence of tilting, needs to be avoided. In this paper the proposed force-guided assembly strategy is investigated concerning its capacity of fulfilling the two claims stated above. Therefore, the hardware setup which is used to conduct the assembly and the process execution are described, as well as sources of positioning deviations are identified. Furthermore, the implementation of the force-control on the specific type of robot controller is described. Applying this force-control multiple experiments with defined positioning deviations are conducted. Furthermore, variations of additional assembly parameters are taken into account. The subsequent evaluation will allow a comparison of deviations, occurring during assembly process and the ability to compensate them. Potential for further optimization is stated in the conclusion.
Subjects
Force-Control
Blade Assembly
Jet Engine
MRO
DDC Class
600: Technik
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