Astron Systems Ltd

United Kingdom

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        United States 1
        World 1
Date
2025 August 1
2025 (YTD) 1
2024 1
IPC Class
F01D 15/10 - Adaptations for driving, or combinations with, electric generators 2
F01D 25/12 - Cooling 2
F01D 25/22 - Lubricating arrangements using working fluid or other gaseous fluid as lubricant 2
F02K 9/46 - Feeding propellants using pumps 2
F02K 9/48 - Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases 2
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Status
Pending 1
Registered / In Force 1
Found results for  patents

1.

Rocket Engine

      
Application Number 19119570
Status Pending
Filing Date 2023-10-11
First Publication Date 2025-08-07
Owner Astron Systems Ltd (United Kingdom)
Inventor
  • Sokolowski, Rafal
  • Brown, Eddie
  • Jones-Tett, Kieran

Abstract

There is disclosed a rocket engine arranged to deliver one or more propellants to a combustion chamber of the rocket engine for generating motive thrust. The rocket engine comprises an electrical transmission system, a turbine generator unit arranged to receive a propellant flow through the turbine generator unit and to generate electrical power and to pass the generated electrical power to the electrical transmission system, and a motor pump unit arranged to receive electrical power from the electrical transmission system and to use the received electrical power to pump a propellant flow though the motor pump unit.

IPC Classes  ?

  • F02K 9/48 - Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases
  • F01D 15/10 - Adaptations for driving, or combinations with, electric generators
  • F01D 25/12 - Cooling
  • F01D 25/22 - Lubricating arrangements using working fluid or other gaseous fluid as lubricant
  • F02K 9/46 - Feeding propellants using pumps
  • F02K 9/56 - Control
  • F04D 13/06 - Units comprising pumps and their driving means the pump being electrically driven

2.

ROCKET ENGINE

      
Application Number GB2023052635
Publication Number 2024/079461
Status In Force
Filing Date 2023-10-11
Publication Date 2024-04-18
Owner ASTRON SYSTEMS LTD (United Kingdom)
Inventor
  • Sokolowski, Rafal
  • Brown, Eddie
  • Jones-Tett, Kieran

Abstract

There is disclosed a rocket engine arranged to deliver one or more propellants to a combustion chamber of the rocket engine for generating motive thrust. The rocket engine comprises an electrical transmission system, a turbine generator unit arranged to receive a propellant flow through the turbine generator unit and to generate electrical power and to pass the generated electrical power to the electrical transmission system, and a motor pump unit arranged to receive electrical power from the electrical transmission system and to use the received electrical power to pump a propellant flow though the motor pump unit.

IPC Classes  ?

  • F02K 9/46 - Feeding propellants using pumps
  • F02K 9/48 - Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases
  • F01D 15/10 - Adaptations for driving, or combinations with, electric generators
  • F01D 25/12 - Cooling
  • F01D 25/22 - Lubricating arrangements using working fluid or other gaseous fluid as lubricant
  • F02K 9/56 - Control
  • F04D 13/06 - Units comprising pumps and their driving means the pump being electrically driven