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HYDRAULIC MECHANISM FOR TURNING AN AIRCRAFT NOSE WHEEL STRUT |
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Description
Strut 5 turns about fixed axis A and is connected by turning pairs B and C to links 6 and 7 which, in turn, are connected by turning pairs D and E to cylinders 1 and 2. The lengths of the links comply with the conditions: A͞B=A͞C and B͞D=C͞E. When hydraulic fluid is delivered to the right end of cylinder 1 and to the left end of cylinder 2, the former moves to the right and the latter to the left, turning strut 5 of the nose wheel, through links 6 and 7, clockwise. Rods 3 and 4 of pistons b and a are attached to a fixed frame. Fluid from the exhaust ends of the cylinders is discharged to the tank. |
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HYDRAULIC MECHANISM FOR TURNING AN AIRCRAFT NOSE WHEEL STRUT
Cliquez pour agrandir
Strut 5 turns about fixed axis A and is connected by turning pairs B and C to links 6 and 7 which, in turn, are connected by turning pairs D and E to cylinders 1 and 2. The lengths of the links comply with the conditions: A͞B=A͞C and B͞D=C͞E. When hydraulic fluid is delivered to the right end of cylinder 1 and to the left end of cylinder 2, the former moves to the right and the latter to the left, turning strut 5 of the nose wheel, through links 6 and 7, clockwise. Rods 3 and 4 of pistons b and a are attached to a fixed frame. Fluid from the exhaust ends of the cylinders is discharged to the tank.
$4307$CHP,FD$
| Documents: |
Hydraulic, pneumatic and electric mechanisms [Streambook] |
 DMG-Lib |
 https://www.dmg-lib.org/dmglib/handler?image=26998023 |
|
 Europeana |
 http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_26998023.html |
 Ilmenau TU |
http://www.tu-ilmenau.de |
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