×

AIRCRAFT ANTI-ICING SYSTEMS HAVING DEFLECTOR VANES

  • US 20150198061A1
  • Filed: 01/14/2014
  • Published: 07/16/2015
  • Est. Priority Date: 01/14/2014
  • Status: Active Grant
First Claim
Patent Images

1. An apparatus comprising:

  • a skin on an inlet side of a nacelle of an aircraft defining an annular chamber;

    a gas delivery system disposed within the annular chamber to provide a first gas to mix with and entrain a second gas in the annular chamber to define a flow through the annular chamber, wherein the second gas is at a different temperature from the first gas; and

    a deflector vane disposed within the annular chamber to redirect the flow through the annular chamber.

View all claims
  • 1 Assignment
Timeline View
Assignment View
    ×
    ×