LEVER MECHANISM FOR CONTROLLING AIRCRAFT TAIL WHEEL BRAKE SHOES

Beschreibung

At the moment skid 1 contacts the earth in landing, cam 2, of suitable profile, moves piston 3 to the right. At this, fluid from chamber 5 is delivered through connections 6 to the brakes. Springs 4 take up a part of the force developed in braking.
$3968$LHP,Co$

Verknüpfte Datensätze

Dokumente:

Hydraulic, pneumatic and electric mechanisms [Streambook]

Permanentlinks

DMG-Lib		https://www.dmg-lib.org/dmglib/handler?image=26659023
Europeana		http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_26659023.html

Datenbereitsteller

TU Ilmenau

http://www.tu-ilmenau.de

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LEVER MECHANISM FOR CONTROLLING AIRCRAFT TAIL WHEEL BRAKE SHOES