IP Library Granted Patent US 11,310,872
Granted Patent B2
US 11,310,872 · App. 16/401,020 · Granted Apr 19, 2022

Metal and composite leading edge assemblies

Inventor: A. David Sandiford (Lake Hughes, CA)
Assignee: ITT Manufacturing Enterprises LLC
H05B3/18B29C44/188B29C69/00B29C70/682B29C70/683B29C70/84B29C70/88B29C70/885B29D99/0025B64D15/12B64D29/00B64D29/04B64D33/02B64D41/00H05B3/0014H05B3/26H05B3/28B29K2105/04B29K2105/046B29K2105/20B29K2703/04B29K2995/0016B29L2031/08B29L2031/3076B29L2031/34B29L2031/7504B64D2033/0233B64D2041/002C23C14/20
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Quick Facts
Patent No.
US 11,310,872
App. No.
16/401,020
Granted
Apr 19, 2022
Kind
B2
Abstract

Various components and methods related to a leading edge assembly are disclosed. The leading edge assembly can include an outer strike shell and a foam core. The foam core can be located inside the outer strike shell. The leading edge assembly can include a heating element with a plurality of sensors and wires. A method of manufacturing a leading edge assembly can include forming a composite layer, applying a metallic layer to the composite layer, installing an electronic device, and inserting a foam core into a cavity bounded by the composite layer and/or the electronic device.

Claims (17)

1. A method for manufacturing a leading edge assembly, the method comprising:

forming a composite layer;

applying a metal layer to an exterior surface of the composite layer;

installing an electronic component to an interior surface of the composite layer;

injecting a foam core material into a cavity bounded by the interior surface of the composite layer and/or the electronic component;

forming a channel in the foam core material, the channel configured to engage with a portion of an air inlet component; and

curing the foam core material in the cavity.

2. The method of manufacturing of claim 1 , wherein forming the composite layer comprises laying-up multiple layers of a composite on a curved surface of a mold.

3. The method of manufacturing of claim 2 , wherein the composite comprises glass reinforced resin.

4. The method of manufacturing of claim 2 , wherein forming the composite layer further comprises applying a vacuum to the layers of composite.

5. The method of manufacturing of claim 1 , wherein applying the metal layer to the exterior surface of the composite layer comprises using vapor deposition to deposit a metal to the exterior surface of the composite layer.

6. The method of manufacturing of claim 1 , wherein applying the metal layer to the exterior surface of the composite layer comprises plating the exterior surface of the composite layer with a metal.

7. The method of manufacturing of claim 6 , wherein plating the exterior surface of the composite layer with a metal comprises using electroless or electrolytic nickel plating.

8. The method of manufacturing of claim 1 , wherein installing the electronic component to the composite layer comprises embedding a heating element in the composite layer.

9. The method of manufacturing of claim 1 , further comprising forming a front mold and a rear mold from a master plug, wherein the front mold includes a curved surface and the rear mold includes a protrusion, the protrusion configured to form the channel.

10. The method of manufacturing of claim 1 , wherein injecting the foam core material into the cavity bounded by the interior surface of the composite layer comprises injecting the foam core material as a liquid into the cavity via a port in a rear mold structure.

11. The method of manufacturing of claim 1 , further comprising installing the composite layer in an outer mold before injecting the foam core material.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 14, 2024
From: ITT MANUFACTURING ENTERPRISES LLC
To: ITT AEROSPACE CONTROLS LLC
Reel/Frame 068891/0123 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 2, 2019
From: SANDIFORD, A. DAVID
To: ITT MANUFACTURING ENTERPRISES LLC
Reel/Frame 049067/0763 →
Continuity (2)
Division 14929058 · Oct 30, 2015
Related Publication 20190261462A1 · Aug 22, 2019
Cited By (1)
US 12,428,165