to DMG-Lib main page
Home  · Site map  · Contact  ·

Advanced Search   Mechanism Search

EMERGENCY AIRCRAFT PNEUMATIC WHEEL BRAKE VALVE MECHANISM

Click to enlargeClick to enlarge Description

When the emergency system is switched in, cam rod 1, linked to this system, is shifted to the left from its middle position, contacting the rounded heads of plungers 2 and 3 and pushing the former downward and allowing the latter to be shifted upward by spring 4. This opens admission valve 2 and closes drain valve 3. Compressed air from the tank is admitted through connection 5, channel a and connection 6 to the brake cylinders, braking the wheels. When the brake lever is released, spring 7 returns cam rod 1 to its middle position in which both of the valves are closed, holding the brakes in the applied position. To release the brakes, cam rod 1 is shifted to the right, at which admission valve 2 remains closed and drain valve 3 is opened, connecting the brake cylinders to the atmosphere through port d (as shown).
$3628$SHP,Va$

Linked items
Documents: Hydraulic, pneumatic and electric mechanisms  [Streambook]
Permanent links
DMG-Lib FaviconDMG-Lib https://www.dmg-lib.org/dmglib/handler?image=26319023
Europeana FaviconEuropeana  http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_26319023.html
Data provider
ITUIlmenau TU  http://www.tu-ilmenau.de
nach oben up
×