Aircraft deicing vehicle's 185 non - continuous rotary type structures

• Main Authors: YANG XIAOHUAI, WANG HUICONG
• Format: Patent
• Language: Chinese; English
• Published: 28.09.2018
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; PERFORMING OPERATIONS; TRANSPORTING

The utility model discloses an aircraft deicing vehicle's 185 non - continuous rotary type structures, the stay cable mechanism comprises a supporting column, support column one end fixedly connectedwith speed reducer, speed reducer one end is provided with gyration motor, the support column upper end is provided with power gear, slewing bearing outer lane and slewing bearing inner circle, innerring of the slewing bearing is located inside the slewing bearing outer lane, power gear is located slewing bearing outer lane one side, mesh between drive gear that slewing bearing outer lane outer wall surface was provided with and the power gear and be connected. This aircraft deicing vehicle's 185 non - continuous rotary type structures, through setting up non - continuous rotary type structure, gyration motor carries out corotation when gyration motor starts, power gear drives drive gear and drives the slewing bearing outer lane and rotate 180 backs, gyration motor turn around, with slewing bearing outer lane gyra