IP Library Granted Patent US 12,692,824
Granted Patent B2
US 12,692,824 · App. 18/085,919 · Granted Jul 28, 2026

Catalytic decomposition reactors

Inventors: Ronald D. Jones (Melbourne, FL); Michael Joseph Baier (Garland, TX); Justin Otto Karl (Titusville, FL)
Assignee: Firehawk Aerospace, Inc.
F02K9/50B01J8/008B01J8/02B01J35/56B01J37/0215B22F10/28B33Y10/00C01B13/0203C01B21/02F02K9/425F02K9/68F23C10/01F23C13/00F23C13/02F23C13/04F23C13/06F23C13/08B01J2208/00884B01J2208/00938B22F2301/00
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,692,824
App. No.
18/085,919
Filed
Dec 21, 2022
Granted
Jul 28, 2026
Kind
B2
Art Unit
1732
USPC
502/150
Abstract

A catalyst bed includes a structure defining a plurality of channels configured to receive flow of fluid to be chemically catalyzed. The plurality of channels are oriented at least partially non-parallel to an overall flow direction of the flow from inputs of the plurality of channels to outputs of the plurality of channels. A catalyst is exposed at an exterior of the structure.

Claims (38)

1 . A catalyst bed comprising:

a monolithic support defining a plurality of channels configured to receive flow of fluid to be chemically catalyzed, wherein the plurality of channels are oriented at least partially non-parallel to an overall flow direction of the flow from inputs of the plurality of channels to outputs of the plurality of channels,

wherein a catalyst coats the monolithic support and is exposed at an exterior of the monolithic support, and

wherein a composition of the monolithic support is different at different portions of the monolithic support.

2 . The catalyst bed of claim 1 , wherein the monolithic support comprises a first section composed of a first material and a second section composed of a second material different from the first material,

wherein the first section adjoins the second section.

3 . The catalyst bed of claim 1 , wherein the composition of the monolithic support is graded.

4 . The catalyst bed of claim 1 , wherein a composition of the catalyst is different at different portions of the catalyst bed.

5 . The catalyst bed of claim 1 , wherein the plurality of channels twist circumferentially with respect to the overall flow direction.

6 . The catalyst bed of claim 5 , wherein the plurality of channels are arranged annularly around a port extending through the monolithic support.

7 . The catalyst bed of claim 1 , wherein the monolithic support has an open cell shape in which gaps are oriented both axially along the overall flow direction and radially transverse to the overall flow direction.

8 . The catalyst bed of claim 1 , wherein cross-sections along a length of the monolithic support include progressively-rotated versions of a template cross-section.

9 . The catalyst bed of claim 1 , wherein the plurality of channels have a plurality of first ports arrayed at a first plane and a plurality of second ports arrayed at a second plane, and

wherein a density of the first ports at the first plane is different from a density of the second ports at the second plane.

10 . The catalyst bed of claim 9 , wherein the plurality of channels fan out from the plurality of first ports to the plurality of second ports.

11 . The catalyst bed of claim 1 , wherein the monolithic support is formed by additive manufacturing.

12 . The catalyst bed of claim 1 , wherein the monolithic support comprises a first portion composed of a first material and a second portion composed of a second material, wherein the first material has a lower high-temperature limit than the second material.

13 . The catalyst bed of claim 1 , wherein different portions of the monolithic support differ in at least one of wall thickness or channel width.

14 . The catalyst bed of claim 1 , wherein a density of the plurality of channels is different at different cross-sections of the monolithic support in planes perpendicular to the overall flow direction.

15 . The catalyst bed of claim 1 , wherein an extension direction of at least one of the plurality of channels is different at different portions of the monolithic support.

16 . The catalyst bed of claim 1 , wherein the monolithic support comprises repeating unit cells forming a lattice, and wherein a type of lattice formed by the repeating unit cells is different at different portions of the monolithic support.

17 . The catalyst bed of claim 1 , wherein the monolithic support has a stochastic lattice geometry.

18 . The catalyst bed of claim 1 , wherein the monolithic support has a triply periodic minimal surface geometry.

19 . The catalyst bed of claim 1 , wherein the monolithic support comprises at least one of a refractory metal or a ceramic.

20 . A catalyst bed comprising:

a structure defining a plurality of channels configured to receive flow of fluid to be chemically catalyzed, wherein the plurality of channels are oriented at least partially non-parallel to an overall flow direction of the flow from inputs of the plurality of channels to outputs of the plurality of channels, and

wherein a catalyst is exposed at an exterior of the structure,

wherein the plurality of channels have a plurality of first ports arrayed at a first plane and a plurality of second ports arrayed at a second plane, the plurality of first ports being connected to respective ones of the plurality of second ports by respective ones of the plurality of channels, such that a number of the plurality of first ports matches a number of the plurality of second ports, and

wherein a number density of the plurality of first ports at the first plane is different from a number density of the plurality of second ports at the second plane.

21 . The catalyst bed of claim 20 , wherein the plurality of channels fan out from the plurality of first ports to the plurality of second ports.

22 . The catalyst bed of claim 20 , wherein the structure comprises a monolithic support, and wherein the monolithic support has a dome shape.

23 . The catalyst bed of claim 20 , wherein the structure comprises a monolithic support,

wherein the plurality of first ports are entrance ports of the monolithic support, and

wherein the plurality of second ports are exit ports of the monolithic support.

24 . The catalyst bed of claim 20 , wherein a first channel of the plurality of channels comprises:

a first section extending away from a central axis of the structure along the overall flow direction, and

a second section extending toward the central axis of the structure.

25 . The catalyst bed of claim 24 , wherein the first section is between an entrance port of the first channel and the second section.

Assignments (2)
SECURITY INTEREST Recorded Sep 1, 2026
From: FIREHAWK AEROSPACE INC.
To: ACQUIOM AGENCY SERVICES LLC
Reel/Frame 075859/0015 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 28, 2024
From: JONES, RONALD D.; BAIER, MICHAEL JOSEPH; KARL, JUSTIN OTTO
To: FIREHAWK AEROSPACE, INC.
Reel/Frame 066583/0733 →
Continuity (2)
Provisional Application 63292215 · Dec 21, 2021
Related Publication 20230191351A1 · Jun 22, 2023
References Cited (35)
US 3695041A · Eggers et al. · 1972 [cited by applicant]
US 4385489A · Abbott · 1983 [cited by applicant]
US 6302683B1 · Vestin et al. · 2001 [cited by applicant]
US 9453479B1 · Jones · 2016 [cited by applicant]
US 9567875B2 · Chaen et al. · 2017 [cited by applicant]
US 10286599B2 · Jones · 2019 [cited by applicant]
US 10309346B2 · Jones · 2019 [cited by applicant]
US 20050181939A1 · Xu et al. · 2005 [cited by applicant]
US 20090007541A1 · Kawaguchi et al. · 2009 [cited by applicant]
US 20090120060A1 · Coste · 2009 [cited by applicant]
US 20090215911A1 · Wang et al. · 2009 [cited by applicant]
US 20130230721A1 · Coupland · 2013 [cited by applicant]
US 20170120335A1 · DeMuth et al. · 2017 [cited by applicant]
US 20170175609A1 · Masoudi · 2017 [cited by applicant]
US 20180036945A1 · Lereboullet et al. · 2018 [cited by applicant]
US 20180169937A1 · Jones · 2018 [cited by applicant]
US 20180171933A1 · Besnard · 2018 [cited by applicant]
US 20200215480A1 · Roy · 2020 [cited by examiner]
US 20200240365A1 · Elzein et al. · 2020 [cited by applicant]
EP 2979752A1 · 2016 [cited by examiner]
WO WO0049671A1 · 2000 [cited by examiner]
Gibbon et al., “Energetic Green Propulsion for Small Spacecraft,” Presented at the 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, UT, Jul. 8-11, 2011, 9 pages. [cited by applicant]
Hendley et al., “Catalytic Decomposition of Nitrous Oxide for Use in Hybrid Rocket Motors,” JPP, May 2021, 37(3):1-5. [cited by applicant]
Invitation to Pay Additional Fees and, Where Applicable, Protest Fees in International Application No. PCT/US2022/53643, mailed on Mar. 14, 2023, 3 pages. [cited by applicant]
Lohner et al., “Nitrous Oxide Monopropellant Gas Generator Development,” Stanford University, 2008, 13 pages. [cited by applicant]
Wilson et al., “Catalytic Decomposition of Nitrous Oxide Monopropellant for Hybrid Motor Re-Ignition,” Presented at the 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Jul. 30-Aug. 1, 2012, Atlanta, GA,… [cited by applicant]
Wilson, “Catalytic Decomposition of Nitrous Oxide Monopropellant for Hybrid Motor Ignition,” Thesis, Utah State University, 2013, 131 pages. [cited by applicant]
Zakirov et al., “An Update on Surrey Nitrous Oxide Catalytic Decomposition Research,” Proceedings of the 15th AIAA/USU Conference on Small Satellites, Orbital Maneuvering, SSC01-XI-2, 2001, 9 pages. [cited by applicant]
Zakirov et al., “N2O Propulsion Research at Tsinghua: 2003,” Presented at the 2nd Int. Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, Jun. 7-8, 2004, 6 pages. [cited by applicant]
Zakirov et al., “Restart able Hybrid Rocket Motor Using Nitrous Oxide,” Proceedings of the 57th International Astronautical Congress, Oct. 2-6, 2006, Valencia, Spain, 6 pages. [cited by applicant]
Zakirov et al., “Surrey Research on Nitrous Oxide Catalytic Decomposition for Space Applications,” Proceedings of the 14th AIAA/USU Conference on Small Satellites, Advanced Subsystems and Components II, SSC00-XI-6, Jan.… [cited by applicant]
Zakirov, “Investigation into Nitrous Oxide Propulsion Option for Small Satellite Applications,” Dissertation, University of Surrey, Aug. 2001, 312 pages. [cited by applicant]
International Search Report and Written Opinion in International Appln. No. PCT/US2022/053643, mailed on May 15, 2023, 24 pages. [cited by applicant]
Price et al., “The Status of Monopropellant Hydrazine Technology,” NASA, Feb. 15, 1968, Technical Report 32-7227, 30 pages. [cited by applicant]
International Preliminary Report on Patentability in International Application No. PCT/US0222/053643, mailed on Jul. 4, 2024, 15 pages. [cited by applicant]