A method and system for automating de-icing procedures for aircraft including the transmission of messages and illumination of guidance lights for pilots to direct their aircraft for de-icing. The system further includes apparatus for generating a safety zone to provide further protection of damage or injury to personnel or aircraft or de-icing machinery.

A method and system for automating de-icing procedures for aircraft including the transmission of messages and illumination of guidance lights for pilots to direct their aircraft for de-icing. The system further includes apparatus for generating a safety zone to provide further protection of damage or injury to personnel or aircraft or de-icing machinery.

A system for automated de-icing or contamination removal of an aircraft. The system includes a mobile platform, the mobile platform including a set of wheels and a swerve drive for controlling movement of the set of wheels along with a contamination removal apparatus mounted to the mobile platform for delivering contamination removal treatment to the aircraft. The system also includes a processor for receiving instructions associated with the contamination removal treatment from an external party and for controlling the mobile platform and contamination apparatus to deliver the contamination removal treatment.

A system for automated de-icing or contamination removal of an aircraft. The system includes a mobile platform, the mobile platform including a set of wheels and a swerve drive for controlling movement of the set of wheels along with a contamination removal apparatus mounted to the mobile platform for delivering contamination removal treatment to the aircraft. The system also includes a processor for receiving instructions associated with the contamination removal treatment from an external party and for controlling the mobile platform and contamination apparatus to deliver the contamination removal treatment.

A method and system for automating de-icing procedures for aircraft including the transmission of messages and illumination of guidance lights for pilots to direct their aircraft for de-icing. The system further includes apparatus for generating a safety zone to provide further protection of damage or injury to personnel or aircraft or de-icing machinery.

A method and system for automating de-icing procedures for aircraft including the transmission of messages and illumination of guidance lights for pilots to direct their aircraft for de-icing. The system further includes apparatus for generating a safety zone to provide further protection of damage or injury to personnel or aircraft or de-icing machinery.

A method for applying a fluid, such as deicing fluid, to a surface of an airplane. A vehicle loaded with a fluid has a nozzle for spraying said fluid onto said surface and at least one sensor and a processing unit is provided for determining a 3D representation of the surface onto which fluid is to be added. The 3D representation is used to determine boundary conditions for a path along which the nozzle is moved relative to the surface and the fluid is being dispensed onto the surface as said nozzle is being moved along the path.

A method for applying a fluid, such as deicing fluid, to a surface of an airplane. A vehicle loaded with a fluid has a nozzle for spraying said fluid onto said surface and at least one sensor and a processing unit is provided for determining a 3D representation of the surface onto which fluid is to be added. The 3D representation is used to determine boundary conditions for a path along which the nozzle is moved relative to the surface and the fluid is being dispensed onto the surface as said nozzle is being moved along the path.

An electrically operated aircraft deicing vehicle includes a chassis having longitudinally extending beams. The chassis supports a rechargeable battery system including one or more battery modules and a charging unit, front and rear axles, a positioning system for a fluid spraying system and a fluid tank system containing deicing fluid. An electric drive motor is operably coupled to the battery system. The electric drive motor is positioned aft of the front axle and between the longitudinally extending beams of the chassis. The electric drive motor is operable to rotate the front wheels. A hydraulic pump system is powered by the battery system. The hydraulic pump system is operably coupled to the positioning system enabling movement of the fluid spraying system. A heat transfer unit is positioned forward of and is operably coupled to the battery system for thermally conditioning the battery system.

An electrically operated aircraft deicing vehicle includes a chassis having longitudinally extending beams. The chassis supports a rechargeable battery system including one or more battery modules and a charging unit, front and rear axles, a positioning system for a fluid spraying system and a fluid tank system containing deicing fluid. An electric drive motor is operably coupled to the battery system. The electric drive motor is positioned aft of the front axle and between the longitudinally extending beams of the chassis. The electric drive motor is operable to rotate the front wheels. A hydraulic pump system is powered by the battery system. The hydraulic pump system is operably coupled to the positioning system enabling movement of the fluid spraying system. A heat transfer unit is positioned forward of and is operably coupled to the battery system for thermally conditioning the battery system.