Weeping ferrofluid anti-ice system

Patent metadata

Field	Value
Publication number	US-10144522-B2
Application number	US-201514688614-A
Country	US
Kind code	B2
Filing date	Apr 16, 2015
Priority date	Apr 16, 2015
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

Method, system, and aircraft for providing anti-ice protection including a supply of ferrofluid that is flowed out of orifices along a first region of an aerodynamic surface, is provided. The flowed ferrofluid is urged toward an aperture on a second region. The aperture is arranged relative to a magnetic field generator. A magnetic field generated by the magnetic field generator attracts the ferrofluid into the aperture while water droplets carried by the ferrofluid continue past the aperture.

First claim

What is claimed is:

1. An ice prevention system, comprising:
a reservoir containing a ferrofluid;
at least one orifice in fluid communication with the reservoir and arranged on a first region of an aerodynamic surface through which the ferrofluid can be flowed onto the first region of the aerodynamic surface, wherein ferrofluid on the first region flows to a second region;
at least one aperture arranged on the second region of the aerodynamic surface, wherein the aperture is in fluid communication with the reservoir;
a first magnetic field source arranged relative to the at least one aperture, wherein the magnetic field is oriented to attract ferrofluid that is proximate to the aperture on the second region of the aerodynamic surface into the aperture; and
a pump in fluid communication with the reservoir, wherein the pump is configured to flow the ferrofluid from the at least one aperture to the reservoir and from the reservoir to the at least one orifice.

2. The ice prevention system of claim 1 , wherein the first magnetic field source comprises at least one of a permanent magnet and an electromagnet.

3. The ice prevention system of claim 1 , further comprising a heater arranged between the reservoir and the at least one orifice, wherein the heater heats the ferrofluid being flowed to the at least one orifice.

4. The ice prevention system of claim 1 , further comprising induction coils arranged under the aerodynamic surface, wherein operation of the induction coils heats the ferrofluid on the aerodynamic surface.

5. The ice prevention system of claim 1 , further comprising one or more second magnetic field sources arranged under the aerodynamic surface, wherein the magnetic field lines direct movement of the ferrofluid along the aerodynamic surface from the first region to the second region.

6. The ice prevention system of claim 1 , further comprising a filter arranged between the at least one aperture and the reservoir, wherein the filter removes contaminants from the ferrofluid.

7. The ice prevention system of claim 1 , wherein the ferrofluid comprises a hydrophobic fluid.

8. The ice prevention system of claim 1 , wherein the ferrofluid comprises nanometer-sized magnetic particles.

Assignees

• Boeing Co

Inventors

• Mackin Steve G

Classifications

• B64D15/08 Primary

  exuded from surface · CPC title

• B64D15/22

  Automatic initiation by icing detector · CPC title

• B64D2033/0233

  comprising de-icing means · CPC title

• B64D33/02

  of combustion air intakes · CPC title

• B64D15/12

  by electric heating (heating arrangements specially adapted for transparent or reflecting areas H05B3/84) · CPC title