IP Library Granted Patent US 10,543,663
Granted Patent B2
US 10,543,663 · App. 15/427,581 · Granted Jan 28, 2020

Rigidized hybrid insulating non-oxide thermal protection system and method of producing a non-oxide ceramic composite for making the same

Inventors: Vann Heng (Buena Park, CA); Winnie W. Chen (Huntington Beach, CA); Leanne L. Lehman (Aliso Viejo, CA); Patrick J. Mobers (Long Beach, CA); Merna E. Salama (Cerritos, CA); Thomas R. Pinney (Long Beach, CA); Jonathan D. Embler (Tustin, CA); Dan E. Driemeyer (Ballwin, MO)
Assignee: The Boeing Company
B32B18/00B32B5/26B32B7/02B32B7/12B32B27/283B32B37/12B32B37/144B32B37/18B64G1/58C04B37/001C04B37/028B32B2250/03B32B2255/26B32B2262/106B32B2307/304B32B2307/722B32B2307/734B32B2315/02B32B2383/00B32B2605/00C04B2237/02C04B2237/32C04B2237/36C04B2237/363C04B2237/365C04B2237/368C04B2237/38C04B2237/704
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Quick Facts
Patent No.
US 10,543,663
App. No.
15/427,581
Granted
Jan 28, 2020
Kind
B2
Abstract

A thermal protection system is provided for a vehicle substructure. The thermal protection system comprises an outer layer for protecting the vehicle substructure. The thermal protection system further comprises an inner layer for conforming to the vehicle substructure. The thermal protection system also comprises an insulation layer sandwiched between the inner and outer layers. The insulation layer includes a porous low-density ceramic insulating material having a densified portion that covers an inner surface of the outer layer to strengthen adhesion.

Claims (27)

1. A thermal protection system for a vehicle substructure, the thermal protection system comprising:

an outer layer for protecting the vehicle substructure;

an inner layer for conforming to the vehicle substructure, wherein the inner layer comprises a layer of conforming material; and

an insulation layer sandwiched between the inner and outer layers, wherein the insulation layer includes a porous low-density ceramic insulating material having a densified portion that covers an inner surface of the outer layer to strengthen adhesion, and wherein the densified portion comprises an infiltrant received within pores defined by the porous low-density ceramic insulating material,

wherein the conforming material of the inner layer is bonded to an inner surface of the insulation layer.

2. The thermal protection system according to claim 1 wherein the densified portion of the porous low-density ceramic insulating material has a thickness between about 0.10 inches (0.254 centimeters) and about 0.20 inches (0.508 centimeters).

3. The thermal protection system according to claim 1 wherein the outer layer comprises a thin-skin layer of ceramic fiber-reinforced non-oxide ceramic matrix composite, such as carbon-silicon carbide, silicon carbide-silicon carbide, carbon-hafnium carbide, carbon-hafnium boride, carbon-silicon nitride, having a thickness between about 0.04 inches (0.102 centimeters) and about 0.08 inches (0.203 centimeters).

4. The thermal protection system according to claim 1 wherein the outer layer has a coefficient of thermal expansion of about 1.65 ppm/° F.

5. The thermal protection system according to claim 4 wherein the insulation layer has a coefficient of thermal expansion of about 1.58 ppm/° F.

6. The thermal protection system according to claim 5 wherein the combination of the outer, inner, and insulation layers cooperate to enable the thermal protection system to withstand a temperature up to or above 3000° F. without degradation of the thermal protection system while maintaining the vehicle substructure at or below its maximum temperature capability.

7. The thermal protection system according to claim 1 wherein the layer of conforming material is adhesively bonded to the insulation layer.

8. A thermal protection system for a vehicle substructure, the thermal protection system comprising:

an outer rigid layer including a thin-skin layer of non-oxide ceramic composite such as carbon-silicon carbide, silicon carbide-silicon carbide, carbon-hafnium carbide, carbon-hafnium boride, carbon-silicon nitride, having a thickness between about 0.04 inches and about 0.08 inches;

an inner conformal layer conforming to the vehicle substructure; and

a rigid ceramic insulation layer sandwiched between the inner and outer layers, wherein the insulation layer includes a porous low-density ceramic material having a density between about 12 lbs/ft 3 and 25 lbs/ft 3 .

9. The thermal protection system according to claim 8 wherein the thin-skin layer of non-oxide ceramic composite includes carbon-fiber reinforced silicon carbide layer having a coefficient of thermal expansion of about 1.65 ppm/° F.

10. The thermal protection system according to claim 9 wherein the rigid ceramic insulation layer has a coefficient of thermal expansion of about 1.58 ppm/° F.

11. The thermal protection system according to claim 10 wherein (i) the porous low-density ceramic insulating material includes a densified portion that covers an inner surface of the carbon-fiber reinforced silicon carbide layer to strengthen adhesion with the carbon-fiber reinforced silicon carbide layer, and (ii) the combination of the outer, inner, and insulation layers cooperate to enable the thermal protection system to withstand a temperature up to or above 3000° F. without degradation of the thermal protection system while maintaining the vehicle substructure at or below its maximum temperature capability.

12. The thermal protection system according to claim 11 wherein the densified portion of the porous low-density ceramic insulating material has a thickness between about 0.10 inches (0.254 centimeters) and about 0.20 inches (0.508 centimeters).

13. The thermal protection system according to claim 12 wherein the inner conformal layer is bonded with room temperature vulcanization (RTV) silicone and covers an inner surface of the insulation layer.

14. The thermal protection system according to claim 8 wherein (i) the porous low-density ceramic insulating material includes a densified portion that covers an inner surface of the carbon-fiber reinforced silicon carbide layer to strengthen adhesion with the carbon-fiber reinforced silicon carbide layer, and (ii) the combination of the outer, inner, and insulation layers cooperate to enable the thermal protection system to withstand a temperature up to or above 3000° F. without degradation of the thermal protection system while maintaining the vehicle substructure at or below its maximum temperature capability.

15. The thermal protection system according to claim 14 wherein the densified portion of the porous low-density ceramic insulating material has a thickness between about 0.10 inches (0.254 centimeters) and about 0.20 inches (0.508 centimeters).

16. The thermal protection system according to claim 15 wherein the carbon-fiber reinforced silicon carbide layer has thickness between about 0.04 inches (0.102 centimeters) and about 0.08 inches (0.203 centimeters).

17. The thermal protection system according to claim 1 wherein the conforming material comprises silicone.

18. The thermal protection system according to claim 1 wherein the conforming material comprises a strain isolating pad.

19. The thermal protection system according to claim 1 wherein the conforming material of the inner layer is bonded to the inner surface of the insulation layer with room temperature vulcanization (RTV) silicone.

20. The thermal protection system according to claim 1 wherein said densified portion comprises a density between about 24 lbs/ft 3 and about 50 lbs/ft 3 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 8, 2017
From: HENG, VANN; CHEN, WINNIE W.; LEHMAN, LEANNE L.; MOBERS, PATRICK J.; SALAMA, MERNA E.; PINNEY, THOMAS R.; EMBLER, JONATHAN D.; DRIEMEYER, DAN E.
To: THE BOEING COMPANY
Reel/Frame 041204/0137 →
Continuity (1)
Related Publication 20180222157A1 · Aug 9, 2018
Cited By (1)
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