Astron Aerospace LLC

United States of America

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        Patent 13
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New (last 4 weeks) 1
2025 October 1
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IPC Class
F02B 53/04 - Charge admission or combustion-gas discharge 10
F02B 53/02 - Methods of operating 8
F02B 53/12 - Ignition 6
F02B 55/08 - Outer members for co-operation with rotary pistonsCasings 6
F02B 55/14 - Shapes or constructions of combustion chambers 6
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NICE Class
07 - Machines and machine tools 1
12 - Land, air and water vehicles; parts of land vehicles 1
42 - Scientific, technological and industrial services, research and design 1
45 - Legal and security services; personal services for individuals. 1
Status
Pending 3
Registered / In Force 11

1.

COMBUSTION ENGINE, PARTS THEREOF, AND METHODS

      
Application Number US2025024577
Publication Number 2025/217639
Status In Force
Filing Date 2025-04-14
Publication Date 2025-10-16
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew

Abstract

The instant invention includes systems for and methods of maximizing efficiencies in an internal combustion engine while minimizing costs and weight for the same and while also minimizing maintenance requirements for the same. Such systems include a compression assembly for compressing fluid to a desired pressure for combustion (such as above 220 psi), a combustion assembly configured to receive at least a portion of the compressed volume of air for each power stroke, and an electrolyzer for separating out hydrogen from the fluid for use as additional fuel during combustion. In this way, the power stroke of the engine is independent of the compression stroke of the engine, thereby eliminating or otherwise minimizing transitional losses associated with the same.

IPC Classes  ?

  • F02M 25/028 - Adding water into the charge intakes
  • F02M 25/12 - Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding acetylene, non-waterborne hydrogen, non-airborne oxygen, or ozone the apparatus having means for generating such gases
  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/10 - Fuel supplyIntroducing fuel to combustion space
  • F02B 53/12 - Ignition

2.

ROTARY ENGINE, PARTS THEREOF, AND METHODS

      
Application Number 18974286
Status Pending
Filing Date 2024-12-09
First Publication Date 2025-06-05
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/02 - Methods of operating
  • F01C 11/00 - Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/08 - Charging, e.g. by means of rotary-piston pump
  • F02B 53/12 - Ignition
  • F02B 55/00 - Internal-combustion aspects of rotary pistonsOuter members for co-operation with rotary pistons
  • F02B 55/08 - Outer members for co-operation with rotary pistonsCasings
  • F02B 55/12 - Cooling thereof by air or other gas
  • F02B 55/14 - Shapes or constructions of combustion chambers
  • F02M 21/02 - Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
  • F02M 47/06 - Other fuel injectors peculiar thereto
  • F02M 51/00 - Fuel-injection apparatus characterised by being operated electrically
  • F02M 51/04 - Pumps peculiar thereto
  • F02M 51/06 - Injectors peculiar thereto

3.

System and method of hydrogen fuel injection

      
Application Number 17986711
Grant Number 12196162
Status In Force
Filing Date 2022-11-14
First Publication Date 2025-01-14
Grant Date 2025-01-14
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A fuel injection system is provided. The system includes a completely sealed housing surrounding the key components of the fuel injection system.

IPC Classes  ?

  • F02M 21/00 - Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
  • F02M 21/02 - Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
  • F02M 47/06 - Other fuel injectors peculiar thereto
  • F02M 51/00 - Fuel-injection apparatus characterised by being operated electrically
  • F02M 51/04 - Pumps peculiar thereto
  • F02M 51/06 - Injectors peculiar thereto

4.

Rotary engine, parts thereof, and methods

      
Application Number 18587705
Grant Number 12270331
Status In Force
Filing Date 2024-02-26
First Publication Date 2024-10-17
Grant Date 2025-04-08
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

The instant invention includes systems for and methods of maximizing efficiencies in an internal combustion engine while minimizing costs and weight for the same and while also minimizing maintenance requirements for the same. Such systems include a compression assembly for compressing fluid to a desired pressure for combustion (such as above 220 psi) and a combustion assembly configured to receive at least a portion of the compressed volume of air for each power stroke. In this way, the power stroke of the engine is independent of the compression stroke of the engine, thereby eliminating or otherwise minimizing transitional losses associated with the same.

IPC Classes  ?

  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F01C 11/00 - Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
  • F01C 21/08 - Rotary pistons
  • F02M 25/028 - Adding water into the charge intakes
  • F02M 26/04 - EGR systems specially adapted for supercharged engines with a single turbocharger
  • F02M 27/04 - Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sonic waves, or the like by electric means or magnetism

5.

ROTARY ENGINE, PARTS THEREOF, AND METHODS

      
Application Number US2024017341
Publication Number 2024/191587
Status In Force
Filing Date 2024-02-26
Publication Date 2024-09-19
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew

Abstract

The instant invention includes systems for and methods of maximizing efficiencies in an internal combustion engine while minimizing costs and weight for the same and while also minimizing maintenance requirements for the same. Such systems include a compression assembly for compressing fluid to a desired pressure for combustion (such as above 220 psi) and a combustion assembly configured to receive at least a portion of the compressed volume of air for each power stroke. In this way, the power stroke of the engine is independent of the compression stroke of the engine, thereby eliminating or otherwise minimizing transitional losses associated with the same.

IPC Classes  ?

6.

SYSTEMS AND METHODS FOR PRODUCTION OF HYDROGEN AND OXYGEN

      
Application Number 18229879
Status Pending
Filing Date 2023-08-03
First Publication Date 2024-02-29
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A hydrogen and oxygen gas production system, parts thereof, and methods associated therewith is provided. The system utilizes naturally occurring fissures on the ocean floor which expel superheated water at a high pressure. The system includes a bell shaped device attached to a tube, included within the bell is an electrolysis device, including a cathode/anode combination. The bell shaped device catches water expelled from the fissure and the electrolysis device pulls the water molecules apart into their individual components in their gaseous form, hydrogen and oxygen. The gasses then travel up the tube to an end of the tube located above sea level, wherein the gasses are separated from one another utilizing either their natural properties or a selectively permeable membrane. The system further provides a method for collecting the separated gasses from the tube and storing them in compressed tanks in a usable form.

IPC Classes  ?

  • C25B 15/08 - Supplying or removing reactants or electrolytesRegeneration of electrolytes
  • C25B 1/04 - Hydrogen or oxygen by electrolysis of water
  • C25B 9/015 - Cylindrical cells
  • C25B 9/05 - Pressure cells
  • C25B 9/17 - Cells comprising dimensionally-stable non-movable electrodesAssemblies of constructional parts thereof

7.

SYSTEMS AND METHODS FOR PRODUCTION OF HYDROGEN AND OXYGEN

      
Application Number US2023029395
Publication Number 2024/030542
Status In Force
Filing Date 2023-08-03
Publication Date 2024-02-08
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew

Abstract

A hydrogen and oxygen gas production system, parts thereof, and methods associated therewith is provided. The system utilizes naturally occurring fissures on the ocean floor which expel superheated water at a high pressure. The system includes a bell shaped device attached to a tube, included within the bell is an electrolysis device, including a cathode/anode combination. The bell shaped device catches water expelled from the fissure and the electrolysis device pulls the water molecules apart into their individual components in their gaseous form, hydrogen and oxygen. The gasses then travel up the tube to an end of the tube located above sea level, wherein the gasses are separated from one another utilizing either their natural properties or a selectively permeable membrane. The system further provides a method for collecting the separated gasses from the tube and storing them in compressed tanks in a usable form.

IPC Classes  ?

  • C25B 15/08 - Supplying or removing reactants or electrolytesRegeneration of electrolytes
  • C25B 1/04 - Hydrogen or oxygen by electrolysis of water
  • C25B 15/023 - Measuring, analysing or testing during electrolytic production

8.

H2 STARFIRE

      
Serial Number 97872125
Status Pending
Filing Date 2023-04-04
Owner Astron Aerospace LLC ()
NICE Classes  ?
  • 07 - Machines and machine tools
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 42 - Scientific, technological and industrial services, research and design
  • 45 - Legal and security services; personal services for individuals.

Goods & Services

Engines, other than for land vehicles Engines for land vehicles Engine technology design and development Offering of licenses, namely, granting of licenses to others of intellectual property relating to engine technology

9.

Rotary engine, parts thereof, and methods

      
Application Number 17862172
Grant Number 12163461
Status In Force
Filing Date 2022-07-11
First Publication Date 2023-03-23
Grant Date 2024-12-10
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/02 - Methods of operating
  • F01C 11/00 - Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/08 - Charging, e.g. by means of rotary-piston pump
  • F02B 53/12 - Ignition
  • F02B 55/00 - Internal-combustion aspects of rotary pistonsOuter members for co-operation with rotary pistons
  • F02B 55/08 - Outer members for co-operation with rotary pistonsCasings
  • F02B 55/12 - Cooling thereof by air or other gas
  • F02B 55/14 - Shapes or constructions of combustion chambers

10.

Rotary engine, parts thereof, and methods

      
Application Number 17389239
Grant Number 11788462
Status In Force
Filing Date 2021-07-29
First Publication Date 2022-02-24
Grant Date 2023-10-17
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F01C 1/08 - Rotary-piston machines or engines of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
  • F02B 53/02 - Methods of operating
  • F01M 13/00 - Crankcase ventilating or breathing
  • F02B 55/14 - Shapes or constructions of combustion chambers
  • F02B 55/02 - Pistons
  • F02B 55/08 - Outer members for co-operation with rotary pistonsCasings
  • F02B 53/08 - Charging, e.g. by means of rotary-piston pump

11.

ROTARY ENGINE, PARTS THEREOF, AND METHODS

      
Application Number US2021043801
Publication Number 2022/026777
Status In Force
Filing Date 2021-07-29
Publication Date 2022-02-03
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accomodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the begining of each combustion process through the end of each exhaust process. The system aslo includes a compression assembly linked to the combustion assembly such that the compassion rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/02 - Methods of operating
  • F02B 55/14 - Shapes or constructions of combustion chambers
  • F02B 55/08 - Outer members for co-operation with rotary pistonsCasings

12.

ROTARY ENGINE, PARTS THEREOF, AND METHODS

      
Application Number US2020013933
Publication Number 2021/029906
Status In Force
Filing Date 2020-01-16
Publication Date 2021-02-18
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

13.

Rotary engine, parts thereof, and methods

      
Application Number 16732318
Grant Number 11384684
Status In Force
Filing Date 2020-01-01
First Publication Date 2021-02-11
Grant Date 2022-07-12
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/02 - Methods of operating
  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/08 - Charging, e.g. by means of rotary-piston pump
  • F02B 53/12 - Ignition
  • F02B 55/00 - Internal-combustion aspects of rotary pistonsOuter members for co-operation with rotary pistons
  • F02B 55/08 - Outer members for co-operation with rotary pistonsCasings
  • F02B 55/12 - Cooling thereof by air or other gas
  • F02B 55/14 - Shapes or constructions of combustion chambers
  • F01C 11/00 - Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type

14.

Rotary engine, parts thereof, and methods

      
Application Number 16745184
Grant Number 10844782
Status In Force
Filing Date 2020-01-16
First Publication Date 2020-11-24
Grant Date 2020-11-24
Owner ASTRON AEROSPACE LLC (USA)
Inventor Riley, Matthew T.

Abstract

A rotary engine, parts thereof, and methods associated therewith is provided. The engine is modular and adjustable to accommodate a variety of requirements and preferences. The system includes a combustion assembly having a housing and a power rotor positioned therein. The power rotor rotates in a first direction from the beginning of each combustion process through the end of each exhaust process. The system also includes a compression assembly linked to the combustion assembly such that the compression rotor rotates in the first direction from the beginning of each intake process through the end of each compression process. A tank assembly in fluid communication with the compression assembly and the combustion assembly provides stability to the system while eliminating or otherwise reducing transitional loses.

IPC Classes  ?

  • F02B 53/02 - Methods of operating
  • F02B 53/04 - Charge admission or combustion-gas discharge
  • F02B 53/08 - Charging, e.g. by means of rotary-piston pump
  • F02B 53/12 - Ignition
  • F02B 55/14 - Shapes or constructions of combustion chambers
  • F01C 11/00 - Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type