to DMG-Lib main page
Home  · Site map  · Contact  ·
DMG-Lib Home + News
Browse
Search
Experience DMG-Lib
About us
Help
 		 
Advanced Search   Mechanism Search

LEVER MECHANISM FOR CONTROLLING AIRCRAFT TAIL WHEEL BRAKE SHOES
Click to enlargeClick to enlarge Description

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$

Linked items
Documents: Hydraulic, pneumatic and electric mechanisms  [Streambook]
Permanent links
DMG-Lib FaviconDMG-Lib https://www.dmg-lib.org/dmglib/handler?image=26659023
Europeana FaviconEuropeana  http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_26659023.html
Data provider
ITUIlmenau TU  http://www.tu-ilmenau.de
nach oben up
Corporate information  · Data Privacy Protection Provision  · Conditions of Use      
×