Thrust apparatuses, systems, and methods

Patent metadata

Field	Value
Publication number	US-9834324-B2
Application number	US-201414533934-A
Country	US
Kind code	B2
Filing date	Nov 5, 2014
Priority date	Nov 5, 2014
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

Described herein is a thrust system for a vehicle that includes at least three electrical power controllers, at least four electrical switches each configured to receive electrical power from at least one of the at least three electrical power controllers, and at least three thrusters each configured to receive electrical power from at least one of the at least three electrical switches. The at least four electrical switches are operable to switch a supply of electrical power from any of the at least three electrical power controllers to any one of the at least three thrusters.

First claim

What is claimed is:

1. A thrust system for a vehicle, comprising:
at least three electrical power controllers;
at least four electrical switches each configured to receive electrical power from two of the at least three electrical power controllers and at least one of the at least four electrical switches comprising an output electrically connected with an input of another of the at least four electrical switches to provide electrical power to the other of the at least four electrical switches; and
at least three thrusters each configured to receive electrical power from at least one of the at least four electrical switches;
wherein the at least four electrical switches are operable to switch a supply of electrical power from any of the at least three electrical power controllers to any one of the at least three thrusters.

2. The system of claim 1 , wherein the switches are operable to allow electrical power from the at least three electrical power controllers to be concurrently supplied to the at least three thrusters, with each electrical power controller supplying power to a respective one of the at least three thrusters.

3. The system of claim 1 , wherein one of the at least three electrical power controllers is a redundant power controller, and wherein in a first mode a first of the at least three electrical power controllers supplies electrical power to a first of the at least three thrusters, a second of the at least three electrical power controllers supplies electrical power to a second of the at least three thrusters, and the redundant power controller supplies no electrical power to the first and second thrusters, and wherein in a second mode one of the first and second electrical power controllers supplies no electrical power to the first and second thrusters, respectively, and the redundant power control supplies electrical power to one of the first and second electrical power controllers.

4. The system of claim 1 , wherein:
each electrical power controller comprises a first power output and a second power output;
each electrical switch comprises a first power input, a second power input, and at least one of a first power output and a second power output;
the first power output of a first of the electrical power controllers is electrically coupled to the first power input of a first of the electrical switches, and the second power output of the first of the electrical power controllers is electrically coupled to the first power input of a second of the electrical switches;
the first power output of a second of the electrical power controllers is electrically coupled to the first power input of a third of the electrical switches, and the second power output of the second of the electrical power controllers is electrically coupled to the second power input of a fourth of the electrical switches; and
the first power output of a third of the electrical power controllers is electrically coupled to the second power input of the third of the electrical switches, and the second power output of the third of the electrical power controllers is electrically coupled to the second power input of the second of the electrical switches.

5. The system of claim 4 , wherein:
the first power output of the second of the electrical switches is electrically coupled to the first power input of the fourth of the electrical switches;
the first power output of the third of the electrical switches is electrically coupled to the second power input of the first of the electrical switches;
the first power output of the first of the electrical switches is electrically coupled to a first of the thrusters, and the second power output of the first of the electrical switches is electrically coupled to a second of the thrusters; and
the first power output of the fourth of the electrical switches is electrically coupled to a third of the thrusters, and the second power output of the fourth of the electrical switches is electrically coupled to a fourth of the thrusters.

6. The system of claim 5 , wherein:
the first of the electrical switches is actuatable to either (i) route electrical power from the first power input of the first of the electrical switches to the first power output of the first of the electrical switches and route electrical power from the second power input of the first of the electrical switches to the second power output of the first of the electrical switches, or (ii) route electrical power from the first power input of the first of the electrical switches to the second power output of the first of the electrical switches and route electrical power from the second power input of the first of the electrical switches to the first power output of the first of the electrical switches;
the second of the electrical switches is actuatable to either (i) route electrical power from the first power input of the second of the electrical switches to the first power output of the second of the electrical switches, or (ii) route electrical power from the second power input of the second of the electrical switches to the first power output of the second of the electrical switches;
the third of the electrical switches is actuatable to either (i) route electrical power from the first power input of the third of the electrical switches to the first power output of the third of the electrical switches, or (ii) route electrical power from the second power input of the third of the electrical switches to the first power output of the third of the electrical switches; and
the fourth of the electrical switches is actuatable to either (i) route electrical power from the first power input of the fourth of the electrical switches to the first power output of the fourth of the electrical switches and route electrical power from the second power input of the fourth of the electrical switches to the second power output of the fourth of the electrical switches, or (ii) route electrical power from the first power input of the fourth of the electrical switches to the second power output of the fourth of the electrical switches and route electrical power from the second power input of the fourth of the electrical switches to the first power output of the fourth of the electrical switches.

7. The system of claim 5 , wherein the switches are configured such that the first power outputs of the first, second, and third electrical power controllers supply power only to the first and second thrusters, and the second power outputs of the first, second, and third electrical power controllers supply power only to the third and fourth thrusters.

8. The system of claim 1 , wherein each of the three thrusters is an ion propulsion thruster.

9. The system of claim 1 , wherein each of the three thrusters is enabled for maximum thrust output.

10. The system of claim 1 , wherein the at least four electrical switches are configured such that each of the at least three electrical power controllers supplies electrical power to only one of the at least three thrusters at a time.

11. A thrust system for a vehicle, comprising:
at least three electrical power controllers;
at least four electrical switches each communicable in power receiving communication with two of the electrical power controllers and at least one of the at least four electrical switches comprising an output electrically connected with an input of another of the at least four electrical switches to provide electrical power to the other of the at least four electrical switches;
at least four thrusters each communicable in power receiving communication with one of the electrical switches; and
a system controller operably coupled to the electrical power controllers and four thrus

Assignees

• Boeing Co

Inventors

• Stickelmaier John F
• Perkins Julie M
• Kreiner Kurt B
• Nguyen Philip D

Classifications

• F03H1/0018

  Arrangements or adaptations of power supply systems (for cosmonautic vehicles B64G1/42) · CPC title

• B64G1/007 Primary

  Operations & Transport · mapped topic

• B64G1/428

  Power distribution and management · CPC title

• B64G1/405

  Operations & Transport · mapped topic

• B64G1/411

  Electric propulsion · CPC title