Probe for measuring the thickness of frost accretion on a surface
View Patent ↗A probe for measuring the thickness of frost accretion on a surface includes a plurality of measuring stages that are stacked substantially orthogonally to the base of the probe. Each measuring stage has an emitter that emits a light beam that is substantially parallel to the base and a receiver that receives the light beam after reflection on the frost.
1. A probe for measuring the thickness of an accretion of frost on an aircraft aerodynamic surface, wherein:
said probe comprises a plurality of measurement stages overlaid at least substantially orthogonally to said accretion of frost; and
each measurement stage comprises:
at least one emitter configured to emit a light beam at least substantially parallel to said accretion of frost, and
at least one receiver configured to receive said light beam after reflection on said frost.
2. The probe as claimed in claim 1 , wherein said emitters are of the light-emitting diode type.
3. The probe as claimed in claim 1 , wherein said receivers are of the photodiode type.
4. The probe as claimed in claim 1 , further comprising a casing, which is secured to said base and which encloses said plurality of overlaid measurement stages, and, at the level of each of said measurement stages, said casing is provided with a transparent window for said light beam.
5. The probe as claimed in claim 4 , wherein the plurality of said windows is formed by a porthole common to all the measurement stages.
6. The probe as claimed in claim 4 , wherein said casing presents an oblong shape.
7. The probe as claimed in claim 4 , further comprising a heater configured to superficially melt the accretion of frost in the vicinity of said probe.
8. A device making it possible to determine the thickness of an accretion of frost on a surface, further comprising a plurality of probes as specified under claim 1 , said probes being distributed over said surface.
9. The device as claimed in claim 8 , intended to determine the thickness and accretion of frost forming on an aerodynamic surface subject to an aerodynamic flow, further comprising a casing, which is secured to said base and which encloses said plurality of overlaid measurement stages, and, at the level of each of said measurement stages, said casing is provided with a transparent window for said light beam, wherein:
said windows of the probes are directed transversely to said aerodynamic flow.
10. The device as claimed in claim 9 , further comprising at least one set of probes disposed in the aerodynamic flow.
11. The device as claimed in claim 10 , wherein said set of probes surrounds the leading edge of said aerodynamic surface.
12. The device as claimed in claim 8 , wherein the bases of said probes are fixed directly to said surface.
13. The device as claimed in claim 8 , wherein the bases of said probes are fixed to a support which is temporarily bonded to said surface, which is parallel to the latter and which leaves an intermediate space with said surface.