In one embodiment, systems and methods include using an inspection system to remove or seal foreign object debris. An inspection system comprises a borescope; wherein a plurality of optical fibers is disposed within the borescope; a mounting system; an articulation system; and a controller, wherein the controller comprises a display; wherein a proximal end of the borescope is coupled to the mounting system, wherein the mounting system is configured to secure the inspection system to an external surface, wherein the mounting system is coupled to the articulation system, wherein the articulation system is configured to actuate the borescope, wherein the articulation system is communicatively coupled to the controller.

In one embodiment, systems and methods include using an inspection system to remove or seal foreign object debris. An inspection system comprises a borescope; wherein a plurality of optical fibers is disposed within the borescope; a mounting system; an articulation system; and a controller, wherein the controller comprises a display; wherein a proximal end of the borescope is coupled to the mounting system, wherein the mounting system is configured to secure the inspection system to an external surface, wherein the mounting system is coupled to the articulation system, wherein the articulation system is configured to actuate the borescope, wherein the articulation system is communicatively coupled to the controller.

Modular apparatus and methods for ultraviolet (UV) light sanitization of an aircraft. The modular apparatus generally comprises a base frame that is universal, and multiple interchangeable modular kits to adapt the base frame to different aircraft cabin geometries. The base frame has integrated therewith circuitry and devices that control ultra-violet C-spectrum (UVC) light sources that are located on a frame of the modular kit. Various embodiments of the modular kits have five parts, and assemble the same way, for different aircraft cabin geometries.

Modular apparatus and methods for ultraviolet (UV) light sanitization of an aircraft. The modular apparatus generally comprises a base frame that is universal, and multiple interchangeable modular kits to adapt the base frame to different aircraft cabin geometries. The base frame has integrated therewith circuitry and devices that control ultra-violet C-spectrum (UVC) light sources that are located on a frame of the modular kit. Various embodiments of the modular kits have five parts, and assemble the same way, for different aircraft cabin geometries.

The invention relates to sanitizing surfaces designed to be touched with sanitation systems and methods for sanitizing such surfaces, such as a control surface which must be touched to either directly or indirectly cause an action. At least one irradiation system includes at least one UVGI emitter in at least one array configured to irradiate at least a portion of a predetermined surface with a predetermined dose of UV radiation, such as after touching of the surface.

An antiviral system comprises, an interior space, and an ultra-violet (UV) illuminator system fixedly mounted within the interior space for illumination of surfaces within the interior space for destruction of pathogens on the surfaces. A plurality of seats can be arranged within the interior space such that the UV illuminator system is configured to illuminate full or partial surfaces of individual seats of the plurality of seats.

An antiviral system comprises, an interior space, and an ultra-violet (UV) illuminator system fixedly mounted within the interior space for illumination of surfaces within the interior space for destruction of pathogens on the surfaces. A plurality of seats can be arranged within the interior space such that the UV illuminator system is configured to illuminate full or partial surfaces of individual seats of the plurality of seats.

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.

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.

The system includes a computer server receiving data representative of the temperature of the cabin and including a database containing, for the aircraft, a predetermined cycle of regulation of the temperature of the air of the cabin; a ground pre-conditioned air unit including: a pre-conditioned air generator and a control module; and a user interface connected to the computer server and transmitting a control signal to the control module; and the control module, upon receiving the control signal, controlling the pre-conditioned air generator, according to the predetermined cycle, which is modulated depending on the data. This system makes it possible to control the temperature of the cabin in real time, so as to correctly disinfect it.