A nacelle is provided for an aircraft propulsion system. The nacelle may include an outer barrel and an active laminar flow control system. The active laminar flow control system may include a plurality of suction sources and a plurality of arrays of perforations in the outer barrel. The active laminar flow control system may be configured with a plurality of zones. Each of the zones may include a respective one of the suction sources which is fluidly coupled with a respective one of the arrays of perforations in the outer barrel.
Multi-zone active laminar flow control system for an aircraft propulsion system
2018-03-06
Patent
Elektronische Ressource
Englisch
MULTI-ZONE ACTIVE LAMINAR FLOW CONTROL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM
Europäisches Patentamt | 2016
|MULTI-ZONE ACTIVE LAMINAR FLOW CONTROL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM
Europäisches Patentamt | 2019
|Propulsion systems for laminar flow aircraft
Engineering Index Backfile | 1961
|The Propulsion of Aircraft with Laminar Flow Control
NTIS | 1968
|