B64F5/23

METHOD AND SYSTEM FOR DISPENSING FLUID ONTO AN AIRPLANE SURFACE
20250361030 · 2025-11-27 ·

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.

METHOD AND SYSTEM FOR DISPENSING FLUID ONTO AN AIRPLANE SURFACE
20250361030 · 2025-11-27 ·

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.

METHOD OF APPLYING ICE REMOVAL FLUID TO A FOLDING WING AIRCRAFT AND METHOD OF OPERATING A FOLDING WING AIRCRAFT
20260021906 · 2026-01-22 ·

A method of applying an ice-removal fluid (113) to a folding wing aircraft (100) is described, the method comprising applying the ice-removal fluid (113) to the folding wing portion (103) and holding the folding wing portion in an over-folded position (111) once the ice-removal fluid (113) has been applied. A method of operating an aircraft (100) during ground based operations is further described using the method of applying an ice-removal fluid (113).

METHOD OF APPLYING ICE REMOVAL FLUID TO A FOLDING WING AIRCRAFT AND METHOD OF OPERATING A FOLDING WING AIRCRAFT
20260021906 · 2026-01-22 ·

A method of applying an ice-removal fluid (113) to a folding wing aircraft (100) is described, the method comprising applying the ice-removal fluid (113) to the folding wing portion (103) and holding the folding wing portion in an over-folded position (111) once the ice-removal fluid (113) has been applied. A method of operating an aircraft (100) during ground based operations is further described using the method of applying an ice-removal fluid (113).

Multifunctional aircraft deicing vehicle with steam jet

Provided is a steam jet multifunctional aircraft deicing vehicle with steam jet, includes a vehicle body, where a steam generating assembly is arranged in the vehicle body, and the steam generating assembly is connected with a steam conveying assembly. A moving assembly is rotatably connected above the vehicle body, and the moving assembly is rotatably connected with an execution assembly. The execution assembly includes a first spray head assembly and a second spray head assembly. The steam conveying assembly includes a first supercharger and a second supercharger arranged side by side, where an air outlet end of the first supercharger is communicated with one end of a first air outlet pipe, and an other end of the first air outlet pipe is communicated with spray heads of the second spray head assembly through a first air pipeline.

Multifunctional aircraft deicing vehicle with steam jet

Provided is a steam jet multifunctional aircraft deicing vehicle with steam jet, includes a vehicle body, where a steam generating assembly is arranged in the vehicle body, and the steam generating assembly is connected with a steam conveying assembly. A moving assembly is rotatably connected above the vehicle body, and the moving assembly is rotatably connected with an execution assembly. The execution assembly includes a first spray head assembly and a second spray head assembly. The steam conveying assembly includes a first supercharger and a second supercharger arranged side by side, where an air outlet end of the first supercharger is communicated with one end of a first air outlet pipe, and an other end of the first air outlet pipe is communicated with spray heads of the second spray head assembly through a first air pipeline.