公开(公告)号：US20220056802A1

公开(公告)日：2022-02-24

申请号：US17389239

申请日：2021-07-29

申请人： ASTRON AEROSPACE LLC

发明人： MATTHEW T. RILEY

IPC分类号： F01C21/04 ,  F01M13/00 ,  F02B53/02 ,  F01C1/08

摘要： 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.

公开(公告)号：US20230092617A1

公开(公告)日：2023-03-23

申请号：US17862172

申请日：2022-07-11

申请人： ASTRON AEROSPACE LLC

发明人： Matthew T. RILEY

IPC分类号： F02B53/02 ,  F01C11/00 ,  F02B53/08 ,  F02B55/08 ,  F02B55/00

摘要： 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.

公开(公告)号：US11788462B2

公开(公告)日：2023-10-17

申请号：US17389239

申请日：2021-07-29

申请人： ASTRON AEROSPACE LLC

发明人： Matthew T. Riley

IPC分类号： F02B53/04 ,  F01C1/08 ,  F02B53/02 ,  F01M13/00 ,  F02B55/14 ,  F02B55/02 ,  F02B55/08 ,  F02B53/08

CPC分类号： F02B53/04 ,  F01C1/08 ,  F01M13/00 ,  F02B53/02 ,  F02B53/08 ,  F02B55/02 ,  F02B55/08 ,  F02B55/14

摘要： 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.

公开(公告)号：US11384684B2

公开(公告)日：2022-07-12

申请号：US16732318

申请日：2020-01-01

申请人： ASTRON AEROSPACE LLC

发明人： Matthew T. Riley

IPC分类号： F02B53/02 ,  F02B53/04 ,  F02B53/08 ,  F02B53/12 ,  F02B55/00 ,  F02B55/08 ,  F02B55/12 ,  F02B55/14 ,  F01C11/00

摘要： 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.

公开(公告)号：US20210040885A1

公开(公告)日：2021-02-11

申请号：US16732318

申请日：2020-01-01

申请人： ASTRON AEROSPACE LLC

发明人： Matthew T. RILEY

IPC分类号： F02B53/08 ,  F02B55/14 ,  F02B53/12

摘要： 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.

公开(公告)号：US20240344480A1

公开(公告)日：2024-10-17

申请号：US18587705

申请日：2024-02-26

申请人： ASTRON AEROSPACE LLC

发明人： MATTHEW T. RILEY

IPC分类号： F02B53/04 ,  F02M25/028 ,  F02M27/04

CPC分类号： F02B53/04 ,  F01C11/004 ,  F01C21/08 ,  F02M25/028 ,  F02M26/04 ,  F02M27/04

摘要： 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.

公开(公告)号：US20240068118A1

公开(公告)日：2024-02-29

申请号：US18229879

申请日：2023-08-03

申请人： ASTRON AEROSPACE LLC

发明人： MATTHEW T. RILEY

IPC分类号： C25B15/08 ,  C25B1/04 ,  C25B9/015 ,  C25B9/05 ,  C25B9/17

CPC分类号： C25B15/083 ,  C25B1/04 ,  C25B9/015 ,  C25B9/05 ,  C25B9/17

摘要： 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.