Airplane cockpit handle control mechanism with damping hand feeling

The utility model discloses an aircraft cockpit handle control mechanism with damping hand feeling. The handle operating mechanism comprises a rod part and a damping part. The rod component is provided with an outer sleeve rod and an inner core rod in the outer sleeve rod. The damping component is p...

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Bibliographic Details
Main Authors CHEN AOJIE, BANG HEE-DEOK, XU YONGPAN
Format Patent
LanguageChinese
English
Published 12.07.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The utility model discloses an aircraft cockpit handle control mechanism with damping hand feeling. The handle operating mechanism comprises a rod part and a damping part. The rod component is provided with an outer sleeve rod and an inner core rod in the outer sleeve rod. The damping component is provided with a first dynamic friction plate, a second dynamic friction plate and a static friction plate between the first dynamic friction plate and the second dynamic friction plate. The first movable friction plate, the second movable friction plate and the outer sleeve rod share the same rotating axis and rotate synchronously. And the static friction plate is fixed. The static friction plate is in surface contact with the first dynamic friction plate and the second dynamic friction plate. The utility model has the beneficial effects that when the outer sleeve rod rotates, the outer sleeve rod drives the first dynamic friction plate and the second dynamic friction plate to synchronously act, and the first dynami
Bibliography:Application Number: CN202323021327U