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LINK-GEAR RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM |
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 Pinche para ampliar
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Description
Link 1 with wheel a turns about fixed axis A of the aircraft frame member. Link 5 is connected by turning pairs B and C to links 1 and 2. Link 2 turns about fixed axis D of the aircraft frame. Piston rod 3 of retracting cylinder 4 is connected by turning pair E to link 2. Cylinder 4 turns about fixed axis F of the aircraft frame. When piston rod 3 moves into retracting cylinder 4, link 1 is turned counterclockwise and link 2 clockwise, and the landing gear is retracted as shown by the dash lines. |
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LINK-GEAR RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM
Click to enlarge
Link 1 with wheel a turns about fixed axis A of the aircraft frame member. Link 5 is connected by turning pairs B and C to links 1 and 2. Link 2 turns about fixed axis D of the aircraft frame. Piston rod 3 of retracting cylinder 4 is connected by turning pair E to link 2. Cylinder 4 turns about fixed axis F of the aircraft frame. When piston rod 3 moves into retracting cylinder 4, link 1 is turned counterclockwise and link 2 clockwise, and the landing gear is retracted as shown by the dash lines.
$1419$LG,AL$
| Documents: |
Lever mechanisms [Streambook] |
 DMG-Lib |
 https://www.dmg-lib.org/dmglib/handler?image=17170023 |
|
 Europeana |
 http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_17170023.html |
 Ilmenau TU |
http://www.tu-ilmenau.de |
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