| 摘要 |
A device for defrosting a leading edge of an aircraft, includes at least one opening (52) for ejecting hot air, a pipe (56) for directing the hot air from a power plant to the ejection opening (52), and elements (58) for measuring the pressure inside the pipe (56), characterized in that the pipe (56) includes at least one cross-section reduction called a chokepoint (62) upstream from the elements (58) for measuring pressure.
|
