Battery powered vehicle propulsion system

Patent metadata

Field	Value
Publication number	US-10060419-B2
Application number	US-201414550372-A
Country	US
Kind code	B2
Filing date	Nov 21, 2014
Priority date	Nov 21, 2014
Publication date	Aug 28, 2018
Grant date	Aug 28, 2018

Abstract

A vehicle propulsion system includes an air heating chamber that receives inlet air from an air intake chamber and provides thrust through an exhaust chamber. A battery powered pulse generator generates a pulsed electrical output signal. An amplifier amplifies the pulsed electrical output signal to provide an amplified pulsed power output signal to the air heating chamber. The amplified pulsed power output signal directly heats the inlet air to generate thrust through the exhaust chamber.

First claim

What is claimed is:

1. A vehicle propulsion system, comprising:
an air heating chamber that receives inlet air from an air intake chamber and provides thrust through an exhaust chamber;
a battery powered pulse generator to generate a pulsed electrical output signal; and
a traveling wave tube amplifier to amplify the pulsed electrical output signal to provide an amplified pulsed power output signal to the air heating chamber, wherein the amplified pulsed power output signal directly heats the inlet air, without use of a fuel, to generate thrust through exiting of the directly heated inlet air from the exhaust chamber.

2. The system of claim 1 , further comprising an electrode that is driven by the traveling wave tube amplifier to provide the pulsed power output signal to the air heating chamber.

3. The system of claim 1 , further comprising a valve disposed between the air intake chamber and the air heating chamber, wherein the valve closes to shut off the inlet air after the amplified pulsed power output signal heats the inlet air in the air heating chamber.

4. The system of claim 3 , wherein the valve opens to enable the inlet air to be received by the air inlet chamber a period of time after the thrust is generated though the exhaust chamber.

5. The system of claim 4 , wherein the battery powered pulse generator generates the pulsed electrical output signal according to a frequency and duty cycle to open and close the valve according to a resonant engine cycle.

6. The system of claim 1 , wherein the air intake chamber and the exhaust chamber are tuned such that at least two pressure wavefronts are generated when the amplified pulsed power output signal directly heats the inlet air in the air heating chamber.

7. The system of claim 6 , wherein one of the at least two pressure wavefronts exits the exhaust chamber and the other of the at least two pressure wavefronts exits the intake chamber, the tuning of the air intake chamber and the exhaust chamber causes the pressure wavefront exiting the exhaust chamber to be greater than the pressure wavefront exiting the intake chamber to generate the thrust.

8. The system of claim 7 , wherein the battery powered pulse generator generates the pulsed electrical output signal according to a frequency and duty cycle to generate the at least two pressure wavefronts.

9. The system of claim 1 , wherein the vehicle propulsion system is employed as a jet engine to power a drone air craft or a land vehicle.

10. A method comprising:
initiating, by a controller, an air inlet phase to provide inlet air from an air intake chamber to an air heating chamber of a resonant engine;
amplifying, by a traveling wave tube amplifier, a pulsed electrical output signal to provide an amplified pulsed power output signal to the air heating chamber, wherein the amplified pulsed power output signal directly heats the inlet air, without use of a fuel, to generate thrust through exiting of the directly heated inlet air from the exhaust chamber;
enabling a battery powered energy pulse to directly heat the inlet air, without use of a fuel, in the air heating chamber during a pulsed energy phase after the air inlet phase; and
disabling the battery powered energy pulse after heating the inlet air in the air heating chamber during a thrust phase to generate the thrust after the pulsed energy phase.

11. The method of claim 10 , further comprising repeating the air inlet phase, the pulsed energy phase, and the thrust phase according to a frequency and duty cycle of the battery powered energy pulse to complete a resonant cycle of phases for the resonant engine.

12. The method of claim 10 , further comprising closing a valve disposed between the air intake chamber and the air heating chamber during the pulsed energy phase, wherein the valve closes to shut off the inlet air after the battery powered energy pulse heats the inlet air in the air heating chamber.

13. The method of claim 12 , further comprising opening the valve to enable the inlet air to be received by the air inlet chamber a period of time after the thrust exits though the exhaust chamber during the thrust phase.

14. The method of claim 10 , further comprising generating at least one pressure wavefront in the air intake chamber and at least one other pressure wavefront in the exhaust chamber when the battery powered energy pulse heats the inlet air in the air heating chamber.

15. The method of claim 14 , further comprising tuning the air intake chamber and the exhaust chamber such that the at least one pressure wavefront exiting the air intake chamber is less than the at least one other pressure wavefront exiting the exhaust chamber to generate the thrust during the thrust phase.

16. A system comprising:
a resonant engine comprising:
an intake chamber to receive inlet air for the resonant engine;
an air heating chamber to directly heat the inlet air, without use of a fuel, received from the intake chamber; and
an exhaust chamber to generate thrust through exiting of the directly heated air from the exhaust chamber after the inlet air is heated in the air heating chamber;

a battery powered pulse generator to generate a pulsed electrical output signal;
a controller to control a frequency and a duty cycle of the pulsed electrical output signal, wherein the frequency and duty cycle control a resonant operating cycle of the resonant engine; and
a traveling wave tube amplifier to amplify the pulsed electrical output signal to provide an amplified pulsed power output signal to the air heating chamber, wherein the amplified pulsed power output signal directly heats the inlet air to generate thrust through the exhaust chamber.

17. The system of claim 16 , further comprising a valve disposed between the intake chamber and the air heating chamber, wherein the valve closes to shut off the inlet air after the amplified pulsed power output signal heats the inlet air in the air heating chamber.

18. The system of claim 16 , wherein the intake chamber and the exhaust chamber are tuned such that at least two pressure wavefronts are generated when the amplified pulsed power output signal directly heats the inlet air in the air heating chamber.

19. The system of claim 16 , wherein the controller dynamically adjusts the frequency or duty cycle of the pulsed electrical output signal based on monitored conditions of the resonant engine.

Assignees

• Rudd Lael
• Parker Robert W
• Tajirian Edmond K
• Northrop Grumman Systems Corp

Inventors

• Rudd Lael
• Parker Robert W
• Tajirian Edmond K

Classifications

• F02K7/04

  with resonant combustion chambers · CPC title

• B60L50/60

  using power supplied by batteries (in combination with fuel cells B60L50/75) · CPC title

• B60L2200/10

  Air crafts · CPC title

• Y02T10/7005

  Cross-Sectional Technologies · mapped topic

• B64G1/406

  Operations & Transport · mapped topic