Patent ID: 11867137
Assignee: nan
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 4:
5. The jet engine of claim 1, wherein:
a. the engine further comprises:
i. a front compression stage for pressurizing intake air;
ii. a central superheating section for further increasing the temperature and pressure of the pressurized intake air from the front compression stage; and
iii. a rear exhaust nozzle stage recovering energy from a discharge of the superheating section and creating thrust;

b. the central superheating section is at least partially electrically powered by the electrical power source; and
c. the central superheating section is connected to said first inverter via an inverter system output to alter the electric current traveling from said first inverter such that the current feeding into the central superheating section is not purely inductive.