Turbine cleaning system
A spray cleaning device for cleaning an auxiliary power unit (APU) within an aircraft comprises one or more spray nozzles, a water tube for supplying water to the nozzles, and positioning means. A system for cleaning APUs comprises a spray cleaning device and a supply system for providing pressurized and temperature controlled washing fluid to the cleaning device. A method for cleaning APUs comprises providing a spray cleaning device, attaching the cleaning device to an air inlet structure of an aircraft, and supplying washing fluid to the cleaning device at a desired spray pressure, spray temperature, and spray droplet size.
1. A spray cleaning device for cleaning an auxiliary power unit (APU) located inside the body of an aircraft, said cleaning device comprising:
one or more spray nozzles arranged to spray into an air intake of the APU;
a water tube for supplying water to said nozzles, said nozzles being attached to a distal end portion of said water tube; and
positioning means rigidly connected to said water tube and adapted to engage with an APU air inlet for positioning the nozzles inside the aircraft body statically with respect to the APU.
2. The spray cleaning device of claim 1 , wherein said positioning means comprises a clamping member adapted to engage with a structure on the aircraft body to clamp the spray cleaning device in a desired position.
3. The spray cleaning device of claim 1 , wherein said positioning means comprises a support member adapted to be held against a selected part of the aircraft body for holding the spray cleaning device firmly in a desired position without clamping it to the aircraft body.
4. The spray cleaning device of claim 1 , wherein said positioning means is connected to a distal rigid portion of the water tube.
5. The spray cleaning device of claim 1 , and further comprising:
at least one of a rigid elongated tube and a flexible hose removably connected to the water tube.
6. The spray cleaning device of claim 5 , wherein said rigid elongated tube is telescopically extendable.
7. The spray cleaning device of claim 1 , wherein said distal end portion of the water tube is curved so as to direct the one or more spray nozzles to a desired location in the APU to be cleaned.
8. The spray cleaning device of claim 1 , wherein the water tube is branched to provide at least two rigid distal end portions, each comprising at least one spray nozzle.
9. The spray cleaning device of claim 8 , wherein the at least two rigid end portions are adapted for independent positioning of the nozzles.
10. The spray cleaning device of claim 2 , wherein the clamping member comprises two arms in a V-configuration, at least one of said arms being spring-loaded.
11. The spray cleaning device of claim 10 , wherein both arms are spring-loaded.
12. The spray cleaning device of claim 10 , wherein spring force resulting from the spring loaded arms urges said arms apart.
13. The spray cleaning device of claim 12 , further comprising means for urging the arms towards each other against the spring force.
14. The spray cleaning device of claim 10 , wherein each arm comprises friction increasing means.
15. The spray cleaning device of claim 10 , further comprising a remote control means for urging the arms towards each other.
16. The spray cleaning device of claim 15 , wherein said remote control means comprises a wire fixedly attached to a first of the arms and looped around a pulley attached to a second of the arms, wherein downward tension on the wire causes the first and second arms to move towards each other.
17. The spray cleaning device of claim 15 , wherein said remote control means comprises at least one gear attached to at least one of the arms, and a motor attached to the at least one gear for driving said gear, wherein operating the motor drives the at least one gear such that the arms are urged together.
18. A system for cleaning an auxiliary power unit (APU) in aircrafts with bodies, comprising:
a spray cleaning device, comprising:
one or more spray nozzles arranged to spray into an air intake of the APU;
a water tube for supplying water to said nozzles, said nozzles being attached to a distal end portion of said water tube; and
a positioning means rigidly connected to said water tube for positioning the nozzles inside the aircraft body with respect to the APU, wherein the positioning means comprises two arms in a V-configuration, at least one of said arms being spring-loaded; and
a supply system for providing pressurized and temperature controlled washing fluid to the spray cleaning device.
19. The system of claim 18 , wherein the supply system delivers washing fluid at a pressure of 30-85 Bar, a temperature of −70 degree C., and with a spray droplet mean size of 40-250 mum.
20. The system of claim 18 , wherein distal ends of the arms are positioned stationary in the aircraft body to position the nozzles inside the aircraft body.