IP Library Granted Patent US 9,181,900
Granted Patent B1
US 9,181,900 · App. 13/307,954 · Granted Nov 10, 2015

Fully advanced superconducting segmented turbo-electric rotormachine (fasster)

Inventor: Richard H. Lugg (Falmouth, ME)
Assignee: Sonic Blue Aerospace, Inc.
F02K5/00F02K3/025
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Quick Facts
Patent No.
US 9,181,900
App. No.
13/307,954
Granted
Nov 10, 2015
Kind
B1
Abstract

Disclosed is a high-power, fully-superconducting electric machine and major subcomponents including a dual (twin) superconducting, counter rotating, sub-scale bypass fan machine, 13-stage switched reluctance turbo-motor, electric compressor, annular ion-plasma combustor with electromagnetic electrodes, and a five stage superconducting counter-rotating turbine power generation machine which is capable of developing 2.5 MW per stage.

Claims (13)

1. A superconducting generator turbine apparatus comprising:

a plurality of counter rotating bypass fans positioned in a hollow-core shaftless frame,

a fully segmented electric compressor,

an annular ion-plasma combustor with electromagnetic electrodes, and

a multi-stage superconducting counter-rotating turbine power generator capable of developing at least 2.0 MW per stage.

2. A superconducting generator turbine apparatus comprising:

(A) a generally cylindrical frame having an interior surface, a center and containing a fully segmented electric compressor,

(B) a plurality of counter rotating bypass fans,

(C) a turbine disposed within the cylindrical frame and configured to generate electrical power, the turbine comprising:

i) at least one arcuate blade array movably coupled relative to the interior surface of the generally cylindrical frame, and

ii) a plurality of induction coils disposed about a perimeter of the generally cylindrical frame, and

(D) an annular ion-plasma combustor configured to generate plasma exhaust comprising ionized molecules of a first polarity,

wherein a hollow-core shaftless bypass air flow tunnel is disposed at the center of the generally cylindrical frame and extends from the plurality of counter rotating bypass fans through the turbine, the fully segmented electric compressor the combustor and an exhaust nozzle.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 10, 2024
From: SONIC BLUE AEROSPACE INC.
To: HYPERSPACE PROPULSION INC.
Reel/Frame 067382/0174 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 27, 2014
From: LUGG, RICHARD H.
To: SONIC BLUE AEROSPACE, INC.
Reel/Frame 032965/0769 →
Continuity (4)
Continuation In Part 13059240
Provisional Application 61418166 · Nov 30, 2010
Provisional Application 61189365 · Aug 19, 2008
Provisional Application 61224666 · Jul 10, 2009