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Electric actuator
hydraulicfor aircraft

electric actuator
electric actuator
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Characteristics

Type
electric, hydraulic
Applications
for aircraft

Description

During certain aircraft flight phases, particularly during landing, it is necessary to quickly and strongly reduce the wing lift. This is achieved by rising dedicated wing control surfaces against the air flow going along the wing profile. This is achieved with dedicated spoiler actuators that are currently most of the time hydraulically powered. The rear horizontal stabilizer of an aircraft is used to stabilize the airframe during the flight. To adjust this stabilizer at an appropriate position, an actuator is used that drives it to required setting. On most recent aircraft, this actuator, mostly of ball screw type, is hydraulically

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Exhibitions

Meet this supplier at the following exhibition(s):

ILA 2024
ILA 2024

5-09 Jun 2024 Berlin (Germany) Hall Chalets East, 2 - Stand 19, 100

  • More information

    Other LIEBHERR-AEROSPACE & TRANSPORTATION SAS products

    Flight control and actuation systems

    *Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.