On-board water spray system for aircraft
A system for simulating wet runway conditions by using a liquid container that is placed inside an aircraft. The liquid container is connected to a nozzle that sprays water in front of the wheels of the aircraft. A valve is used to control the flow of water from the nozzle. Systems, such as the braking system of the aircraft, can then be tested in wet runway conditions simulated by the system. The amount of water sprayed from the nozzle can also be electronically controlled in relation to the speed of the aircraft, such that the nozzle sprays a nearly uniform layer of liquid in front of the wheels. The system can also be modified to include two tanks to manipulate the center of gravity of the aircraft.
1. A system for simulating wet runway conditions, the system comprising:
a tank situated on an aircraft which receives air under pressure from an air source to compel the delivery of water from the tank to a nozzle;
a liquid conduit fluidly connecting the tank to the nozzle; and the nozzle positioned to spray water onto a ground surface in front of a wheel of the aircraft;
wherein the tank includes a relief valve which releases air to the atmosphere upon the pressure in the tank reaching a predetermined value to avoid over-pressurization in the tank; and
wherein the air source is bleed air from an engine on the aircraft.
2. The system of claim 1 wherein the bleed air is delivered from a regulated source of air originating from the compressor section of the engine in an air conduit.
3. The system of claim 2 wherein the air conduit includes a shut off valve.