Preceramic resin formulations, ceramic materials comprising the preceramic resin formulations,and related articles and methods

Patent metadata

Field	Value
Publication number	US-10731036-B2
Application number	US-201715651970-A
Country	US
Kind code	B2
Filing date	Jul 17, 2017
Priority date	Jul 17, 2017
Publication date	Aug 4, 2020
Grant date	Aug 4, 2020

Abstract

A preceramic resin formulation comprising a polycarbosilane preceramic polymer and an organically modified silicon dioxide preceramic polymer. A ceramic material comprising a reaction product of the polycarbosilane preceramic polymer and organically modified silicon dioxide preceramic polymer is also described. Articles comprising the ceramic material are also described, as are methods of forming the preceramic resin formulation and the ceramic material.

First claim

What is claimed is:

1. A preceramic resin formulation comprising a polycarbosilane preceramic polymer and an organically modified silicon dioxide preceramic polymer, the organically modified silicon dioxide preceramic polymer comprising quaternary coordinated oxygen to silicon atoms of the organically modified silicon dioxide preceramic polymer.

2. The preceramic resin formulation of claim 1 , wherein a viscosity of the polycarbosilane preceramic polymer is less than or equal to about 250 cP at a temperature of about 25° C. and a viscosity of the organically modified silicon dioxide preceramic polymer is greater than or equal to about 2,500 cP at a temperature of about 25° C.

3. The preceramic resin formulation of claim 1 , wherein the polycarbosilane preceramic polymer comprises monomers having the chemical structure of

where R 1 and R 2 of each monomer is independently a hydrogen (H) group, a methyl (CH 3 ) group, a vinyl group (CH 2 ═CH) directly bonded to the silicon atom, or a vinyl group (CH 2 ═CH) bonded to the silicon atom by an alkyl linker, and n is an integer from 2 to 10,000.

4. The preceramic resin formulation of claim 1 , wherein the polycarbosilane preceramic polymer is formulated to exhibit a viscosity of from about 40 cP to about 120 cP at about 25° C.

5. The preceramic resin formulation of claim 1 , wherein the polycarbosilane preceramic polymer is formulated to exhibit a viscosity of from about 40 cP to about 100 cP at about 25° C.

6. The preceramic resin formulation of claim 1 , wherein the organically modified silicon dioxide preceramic polymer comprises monomers having the chemical structure of

where each of R 3 and R 4 is independently a methyl (CH 3 ) group, a vinyl group (CH 2 ═CH) directly bonded to the silicon atom, or a vinyl group (CH 2 ═CH) bonded to the silicon atom by an alkyl linker, and n is an integer from 2 to 10,000.

7. The preceramic resin formulation of claim 1 , wherein the organically modified silicon dioxide preceramic polymer is formulated to exhibit a viscosity of from about 50,000 cP at 25° C. to about 60,000 cP at 25° C.

8. The preceramic resin formulation of claim 1 , wherein the organically modified silicon dioxide preceramic polymer is formulated to exhibit a viscosity of from about 4,500 cP at 25° C. to about 7,000 cP at 25° C.

9. The preceramic resin formulation of claim 1 , wherein the polycarbosilane preceramic polymer comprises from about 10% by weight to about 90% by weight of the preceramic resin formulation.

10. The preceramic resin formulation of claim 1 , wherein the organically modified silicon dioxide preceramic polymer comprises from about 10% by weight to about 90% by weight of the preceramic resin formulation.

11. The preceramic resin formulation of claim 1 , further comprising a crosslinking agent.

12. The preceramic resin formulation of claim 1 , wherein the preceramic resin formulation is formulated to exhibit a viscosity of from about 1,000 cP at about 25° C. to about 5,000 cP at about 25° C.

13. A method of forming a preceramic resin formulation, comprising:
combining a polycarbosilane preceramic polymer and an organically modified silicon dioxide preceramic polymer with a crosslinking agent, the organically modified silicon dioxide preceramic polymer comprising quaternary coordinated oxygen to silicon atoms of the organically modified silicon dioxide preceramic polymer.

14. A method of forming a ceramic material, comprising:
forming a preceramic resin formulation comprising a polycarbosilane preceramic polymer, an organically modified silicon dioxide preceramic polymer, and a crosslinking agent, the organically modified silicon dioxide preceramic polymer comprising quaternary coordinated oxygen to silicon atoms of the organically modified silicon dioxide preceramic polymer;
curing the preceramic resin formulation to form a cured preceramic resin formulation; and
ceramifying the cured preceramic resin formulation to form a ceramic material.

15. The method of claim 14 , wherein curing the preceramic resin formulation to form a cured preceramic resin formulation comprises reacting vinyl groups of the polycarbosilane preceramic polymer with silicon-hydrogen bonds of the organically modified silicon dioxide preceramic polymer.

16. The method of claim 14 , wherein curing the preceramic resin formulation to form a cured preceramic resin formulation comprises exposing the preceramic resin formulation to a temperature of from about 0° C. to about 400° C.

17. The method of claim 14 , wherein ceramifying the cured preceramic resin formulation to form a ceramic material comprises forming the ceramic material at a ceramic yield of greater than about 70%.

18. The method of claim 14 , further comprising forming the preceramic resin formulation into a shape before curing the preceramic resin formulation.

19. The method of claim 18 , wherein forming the preceramic resin formulation into a shape before curing the preceramic resin formulation comprises forming the preceramic resin formulation into at least a portion of a component of a rocket motor nozzle or a rocket motor casing before curing.

20. The method of claim 18 , wherein forming the preceramic resin formulation into a shape before curing the preceramic resin formulation comprises forming the preceramic resin formulation into at least a portion of a turbine, a turbine blade, a turbine housing, a turbine engine vane, and insulating tile, a rotor blade, an insulation blanket, a compressor blade, a wing component, a fuselage skin, a landing gear, an exhaust nozzle, an engine exhaust duct, a nose cone, a re-entry shield or a heat shield before curing.

21. The method of claim 18 , wherein forming the preceramic resin formulation into a shape before curing the preceramic resin formulation comprises forming an oxidative resistant coating on a rocket motor nozzle or other high temperature aerostructure, a high temperature adhesive, a mortar material, an insulation, a thermal protection material, a thermal ablation material, or a matrix material of a ceramic matrix composite.

Assignees

• Northrop Grumman Innovation Systems Inc

Inventors

• Garcia Benjamin W C

Classifications

• C04B35/80

  Fibres, filaments, whiskers, platelets, or the like · CPC title

• C04B35/515

  based on non-oxide ceramics · CPC title

• F05D2300/226

  Carbides · CPC title

• C08G77/60

  in which all the silicon atoms are connected by linkages other than oxygen atoms · CPC title

• F05D2230/20

  essentially without removing material · CPC title