IP Library Granted Patent US 11,952,131
Granted Patent B2
US 11,952,131 · App. 18/107,543 · Granted Apr 9, 2024

Composite aerostructure with integrated heating element

Inventors: Kyle B. Hardman (Shady Shores, TX); Mark A. Calder (Midlothian, TX); Ian C. Derx (Rowlett, TX)
Assignee: QARBON AEROSPACE (FOUNDATION), LLC
B64D15/12B29C70/882B64D15/22H05B3/145H05B3/286B29K2071/00B29K2105/101B29K2307/04B29K2995/0005B29L2031/3076H05B2203/003
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Quick Facts
Patent No.
US 11,952,131
App. No.
18/107,543
Granted
Apr 9, 2024
Kind
B2
Abstract

A heated composite structure and a method for forming a heated composite structure. The structure includes carbon fibers embedded within a thermoplastic matrix. The carbon fibers are connected with first and second electrodes that are configured to be connected with an electric source such that applying current to the electrodes causes current to flow through the embedded carbon fibers to provide resistive heating sufficient to heat the composite structure to impede formation of ice on the composite structure.

Claims (13)

1. A heated aerostructure, comprising:

a composite structure, comprising:

a carbon fiber reinforced thermoplastic structural layer;

a reinforced thermoplastic heater layer, comprising:

a plurality of electrically conductive non-metallic fibers comprising a unidirectional carbon fiber reinforced thermoplastic;

a first electrode electrically connected with the conductive non-metallic fibers; and

a second electrode electrically connected with the conductive non-metallic fibers, so that the conductive non-metallic fibers provide an electrical pathway between the first electrode and the second electrode;

wherein the first electrode and the conductive non-metallic fibers are connected such that electric power applied to the first electrode is conducted through the electrically conductive non-metallic fibers to provide resistive heating sufficient to heat the composite structure.

2. The heated aerostructure of claim 1 , wherein the plurality of electrically conductive fibers provide a conductive pathway between the first electrode and the second electrode.

3. The heated aerostructure of claim 2 , wherein the conductive pathway comprises a convoluted path between the first and second electrodes.

4. The heated aerostructure of claim 2 , wherein the conductive pathway comprises a serpentine path between the first and second electrodes.

5. The heated aerostructure of claim 1 , comprising an additional heater layer independently operable from the reinforced thermoplastic heater layer and comprising an electrically insulative layer disposed between and insulating the additional heater layer from the reinforced thermoplastic heater layer.

6. The heated aerostructure of claim 1 , wherein the plurality of electrically conductive non-metallic fibers comprises a convoluted path between the first and second electrodes.

Assignments (3)
SECURITY INTEREST Recorded Sep 8, 2025
From: QARBON AEROSPACE (FOUNDATION), LLC; QARBON AEROSPACE, INC.
To: CITIZENS BANK, N.A.
Reel/Frame 072190/0626 →
INTELLECTUAL PROPERTY SECURITY AGREEMENT Recorded Sep 4, 2025
From: QARBON AEROSPACE (F OUNDATION), LLC; QARBON AEROSPACE, INC.,
To: CITIZENS BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 072808/0876 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 11, 2023
From: HARDMAN, KYLE B; CALDER, MARK A; DERX, IAN C
To: QARBON AEROSPACE (FOUNDATION), LLC
Reel/Frame 065830/0929 →
Continuity (4)
Continuation 16564108 · Sep 9, 2019
Division 16393519 · Apr 24, 2019
Provisional Application 62661917 · Apr 24, 2018
Related Publication 20230182906A1 · Jun 15, 2023