Solid propellant additive manufacturing system

Patent metadata

Field	Value
Publication number	US-11208362-B2
Application number	US-201816226741-A
Country	US
Kind code	B2
Filing date	Dec 20, 2018
Priority date	Aug 9, 2016
Publication date	Dec 28, 2021
Grant date	Dec 28, 2021

Abstract

A system is used for additively manufacturing propellant elements, such as for rocket motors, includes partially curing a propellant mixture before extruding or otherwise dispensing the material, such that the extruded propellant material is deposited on the element in a partially-cured state. The curing process for the partially-cured extruded material may be completed shortly after the material is put into place, for example by the material being heated at or above its cure temperature, such that it finishes curing before it fully cools. The propellant material may be prepared by first mixing together, a fuel, an oxidizer, and a binder, such as in an acoustic mixer. After that mixing a curative may be added to the mixture. The propellant mixture may then be directed to an extruder (or other dispenser), in which the mixture is heated to or above a cure temperature prior to the deposition, and then deposited.

First claim

What is claimed is:

1. A system for additively manufacturing a propellant piece, the system comprising:
a first mixer;
a second mixer;
a dispenser; and
a heater having a feedback system for controlling heating from the heater;
wherein material for forming the propellant piece continuously moves from 1) the first mixer, in which fuel, oxidizer, and a binder are mixed to form a propellant mixture, to 2) the second mixer, in which a curative is added to the propellant mixture to produce a curable propellant mixture, to 3) the dispenser, with the heater used to heat and partially cure the curable propellant mixture before the curable propellant mixture is dispensed by the dispenser; and
wherein the feedback system controls the heating from the heater to heat the curable propellant mixture at or above a cure temperature of the curable propellant mixture.

2. The system of claim 1 , wherein the first mixer is an acoustic mixer.

3. The system of claim 1 , wherein the dispenser is an extruder.

4. The system of claim 1 , wherein the heater is an electrical heater.

5. The system of claim 1 , wherein the dispenser includes an array of nozzles.

6. The system of claim 5 , wherein the array of nozzles includes nozzles with different sizes and/or shapes of openings.

7. The system of claim 5 , wherein the array of nozzles is a wheel of nozzles.

8. The system of claim 5 , wherein the dispenser is an extruder that is configured to receive different of the nozzles.

9. The system of claim 1 , wherein the dispenser includes a reservoir for holding the propellent mixture.

10. The system of claim 1 , wherein the heater and the dispenser are integrated into a single device, with the heater used to heat the propellent mixture while the propellent mixture is in the dispenser.

11. A system for additively manufacturing a propellant piece, the system comprising:
a first mixer;
a second mixer;
a dispenser; and
a heater having a feedback system for controlling heating from the heater;
wherein material for forming the propellant piece continuously moves from 1) the first mixer, in which fuel, oxidizer, and a binder are mixed to form a propellant mixture, to 2) the second mixer, in which a curative is added to the propellant mixture to produce a curable propellant mixture, to 3) the dispenser, with the heater used to heat and partially cure the curable propellant mixture before the curable propellant mixture is dispensed by the dispenser, wherein the heater and the dispenser are integrated into a single device, with the heater used to heat the propellent mixture while the propellent mixture is in the dispenser, wherein the heater is an electric resistive heater wrapped around part of the dispenser, and wherein the feedback system controls the heating from the heater to heat the curable propellant mixture at or above a cure temperature of the curable propellant mixture.

12. The system of claim 11 ,
wherein the dispenser includes a reservoir for holding the propellent mixture; and
wherein the electric resistive heater is wrapped around the reservoir.

13. The system of claim 12 , wherein the heater is configured to partially cure the propellent mixture as the propellent mixture passes through the reservoir.

14. The system of claim 1 ,
further comprising a bed that is movable relative to the dispenser;
wherein the bed supports the propellant piece during dispensing of the propellent mixture from the dispenser.

15. The system of claim 14 , further comprising a controlled-environment chamber in which the dispenser and the bed are located.

16. A system for additively manufacturing a propellant piece, the system comprising:
a mixer;
a dispenser; and
a heater having a feedback system for controlling heating from the heater;
wherein material for forming the propellant piece continuously moves from 1) the mixer, in which fuel, oxidizer, binder, and curative are mixed to form a propellant mixture, to 2) the dispenser, with the heater used to heat and partially cure the curable propellant mixture before the curable propellant mixture is dispensed by the dispenser, wherein the feedback system controls the heating from the heater to heat the curable propellant mixture at or above a cure temperature of the curable propellant mixture.

17. The system of claim 11 , wherein the first mixer is an acoustic mixer.

18. The system of claim 16 , wherein the dispenser is an extruder.

19. The system of claim 16 , wherein the heater is an electrical heater wrapped around part of the dispenser.

20. The system of claim 1 , wherein the heater is in contact with the dispenser.

Assignees

• Raytheon Co

Inventors

• Summers Matthew H
• Danforth Jeremy C
• Garrett David G
• Langhenry Mark T

Classifications

• B33Y40/10

  Pre-treatment · CPC title

• B33Y70/10

  Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials · CPC title

• C06B21/0025 Primary

  the ingredient being a polymer bonded explosive or thermic component · CPC title

• C06B21/0033

  Shaping the mixture · CPC title

• B29B7/007

  for continuous mixing · CPC title