【考案の名称】航空機用除氷車輛

Japanese Patent JPH0740399

U

The invention relates to suspension means for a spray nozzle, especially for spraying a spray fluid for deicing an aircraft. For example, the invention will be intented for a vehicle for deicing aircraft. According to the present application, the vehicle for deicing aircraft includes an undercarriage (1) having a lifting device (4,5,6,7) which at its free end carries a cabin structure (3), and having a spray device for spaying an aircraft with a deicing fluid, said spray device comprising a pump and an associated spray nozzle (40). The cabin structure (3) carries a longitudinally adjustable lightweight boom (20) carrying at its free end the spray nozzle (40). According to the present invention, the suspension means for the spray nozzle (40) are characterized in that the nozzle (40) is pivotally suspended about a horizontal axis (32) in a fork (25) carried by the end of a boom (20), the nozzle (40), being connected to a generally U-shaped yoke (28) having outwardly extending ends supported in arms (26,27) of the fork (25), said yoke (28) being connected to a remote control activator (47) carried by the fork (25), and that the nozzle (40) is connected to the yoke (28) by a shaft (42) whose central axis (51) is perpendicular to and intersecting the pivot axis (32) of the yoke (28) in a point generally located in the axis (45) of the spray direction of the nozzle (40). said shaft (42) being connected to a remote control activator (48) carried by the yoke (28).

JP2009045598	FLUID STIRRING APPARATUS
WO/2022/131496	REMOTE MAINTENANCE MANAGEMENT SYSTEM FOR FIREFIGHTING VEHICLE
JP2002174380	INLET-RIGHT-ANGLED ELBOW

Bestelgard, Gottfredo

JP4828392U

July 18, 1995

June 17, 1992

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Bestelgard, Gottfredo

A62C27/00; A62C31/24; B05B13/04; B60P3/30; B05B17/00; B64F5/00; (IPC1-7): B64F5/00; B05B17/00; B60P3/30

Heiyoshi Odashima

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