Concept studies on a multifunctional unit for hydraulic supply and high lift actuation in aircraft

Publikationstyp
Conference Paper
Date Issued
2019-10
Sprache
English
Author(s)
Nordmann, Lennard  
Thielecke, Frank  
Lücken, Peter  
Hamm, Martin  
Institut
Flugzeug-Systemtechnik M-7  
TORE-URI
http://hdl.handle.net/11420/4763
Citation
ASME/BATH Symposium on Fluid Power and Motion Control, FPMC: (2019-10)
Contribution to Conference
Symposium on Fluid Power and Motion Control, ASME/BATH, FPMC 2019  
Publisher DOI
10.1115/FPMC2019-1678
Scopus ID
2-s2.0-85084163403
This paper investigates the potential of a new functionality of the hybrid Power Control Unit (PCU) in zonal electrohydraulic aircraft systems. The conventional PCU, as a hydraulic consumer, is the central drive for the leading and trailing edge flaps of an aircraft. Through extended functionality, it can also be operated as pump to provide hydraulic power in certain flight phases. The paper elaborates and presents different concepts for the integration of such a multifunctional PCU and evaluates the potential regarding mass savings and improvement of reliability. In subsequent simulation studies, the most promising concept is validated and analysed regarding the arising challenges.
DDC Class
000: Allgemeines, Wissenschaft