A method for coordinating contamination removal on a surface of an aircraft, comprising receiving an electronic contamination removal request, determining location for contamination removal treatment, electronically transmitting location for contamination removal treatment to aircraft, electronically receiving progress of contamination removal treatment, and electronically transmitting progress of contamination removal treatment to aircraft, wherein the progress of contamination removal treatment is displayed on multiple displays to allow for close monitoring of the contamination removal treatment.

A method for coordinating contamination removal on a surface of an aircraft, comprising receiving an electronic contamination removal request, determining location for contamination removal treatment, electronically transmitting location for contamination removal treatment to aircraft, electronically receiving progress of contamination removal treatment, and electronically transmitting progress of contamination removal treatment to aircraft, wherein the progress of contamination removal treatment is displayed on multiple displays to allow for close monitoring of the contamination removal treatment.

A method for de-icing liquid on a surface of an airplane includes supplying de-icing liquid to and through a spraying nozzle of a de-icing vehicle through a pipe that connects the nozzle with a tank assembly of the de-icing vehicle, where the liquid is delivered to the spraying nozzle as a mix of an anti-freeze liquid and additives, the anti-freeze liquid is delivered to the pipe from an anti-freeze liquid tank via a first dosage pump, and the additives are delivered from an additives tank via a second dosage pump.

A method for de-icing liquid on a surface of an airplane includes supplying de-icing liquid to and through a spraying nozzle of a de-icing vehicle through a pipe that connects the nozzle with a tank assembly of the de-icing vehicle, where the liquid is delivered to the spraying nozzle as a mix of an anti-freeze liquid and additives, the anti-freeze liquid is delivered to the pipe from an anti-freeze liquid tank via a first dosage pump, and the additives are delivered from an additives tank via a second dosage pump.

The invention provides a method of sampling de-icing fluid from an airplane de-icer having a spraying nozzle for spraying the de-icing fluid onto a surface of an airplane, the de-icing fluid preferably being produced by the airplane de-icer by mixing a number of ingredients. The method comprises the steps of: i) obtaining a limited sample of the de-icing fluid by diverting at least a part of the de-icing fluid flowing towards the spraying nozzle for a period of time during the spraying of the de-icing fluid onto the surface of the airplane, and ii) collecting sample of the de-icing fluid in a sample container. A system for sampling de-icing fluid is also provided as well as an airplane de-icer comprising the system.

The invention provides a method of sampling de-icing fluid from an airplane de-icer having a spraying nozzle for spraying the de-icing fluid onto a surface of an airplane, the de-icing fluid preferably being produced by the airplane de-icer by mixing a number of ingredients. The method comprises the steps of: i) obtaining a limited sample of the de-icing fluid by diverting at least a part of the de-icing fluid flowing towards the spraying nozzle for a period of time during the spraying of the de-icing fluid onto the surface of the airplane, and ii) collecting sample of the de-icing fluid in a sample container. A system for sampling de-icing fluid is also provided as well as an airplane de-icer comprising the system.

A method and a system for recycling spent ethylene or propylene glycol recovered from aircraft deicing solutions is described. The recovered spent ethylene or propylene glycol contains water and other undesirable substances which require to be removed to produce a solution free of these substances which can be further processed to remove substantially all of the water content and to blend-in additives required to certify the final glycol solution for aircraft deicing. The method and system employs a computer controller for continuous automatic batch processing of the spent glycol, including, in combination, filtering, distillation, blending and testing in specific sequences and achieves an improved quality recycled glycol of a purity of at least 99.5% and preferably between 99.6% to 99.9% glycol concentration.

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.

The present discloses a system for washing and de-icing of aircrafts. The preset invention provides a washing and deicing area comprising one or more gantries to ensure different steps of the washing or the de-icing process. The structure of the one or more gantries is essentially made of telescopic arms allowing more flexibility on the positioning of nozzle clusters during the washing and de-icing process. The use of such a mechanical system is easily accommodated to different aircraft bodies regardless their sizes. The whole functionality and positioning of the system is ensured by a programmable system comprising an aircraft position detection system and an aircraft contour detection system allowing the programmable system to reposition the nozzle clusters in a preferred location while avoiding contact with the aircraft.