IP Library Granted Patent US 7,810,325
Granted Patent B2
US 7,810,325 · App. 11/710,391 · Granted Oct 12, 2010

Self-pressurizing Stirling engine

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,810,325
App. No.
11/710,391
Granted
Oct 12, 2010
Kind
B2
Abstract

A solar thermal powered aircraft powered by heat energy from the sun. A heat engine, such as a Stirling engine, is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller. The heat engine has a thermal battery in thermal contact with it so that heat is supplied from the thermal battery. A solar concentrator, such as reflective parabolic trough, is movably connected to an optically transparent section of the aircraft body for receiving and concentrating solar energy from within the aircraft. Concentrated solar energy is collected by a heat collection and transport conduit, and heat transported to the thermal battery. A solar tracker includes a heliostat for determining optimal alignment with the sun, and a drive motor actuating the solar concentrator into optimal alignment with the sun based on a determination by the heliostat.

Claims (14)

1. An improved Stirling engine of a type having a crankcase with opposing hot and cold heat exchanging ends, a piston capable of reciprocating within said crankcase between the hot and cold heat exchanging ends, a crankshaft coupled to said piston and extending out from said crankcase so that reciprocation of said piston rotates said crankshaft, and a journal surrounding said crankshaft, the improvement comprising:

a working fluid within an hermetically sealed crankcase;

a crankcase pressure relief valve for controlling the crankcase pressure and the power output of said Stirling engine;

a closed reservoir for receiving working fluid released from said crankcase pressure relief valve; and

at least one helical groove on a surface of one of said crankshaft and said journal and bounded by a surface of the other one of said crankshaft and said journal, said helical groove(s) communicating between an inner crankcase volume and said closed reservoir so that the relative motion between the rotating crankshaft and said journal pumps the working fluid into said

crankcase to self-pressurize the same, whereby the working fluid released from said crankcase is recycled back into said crankcase.

2. The improvement of claim 1 ,

wherein the working fluid is helium.

3. The improvement of claim 1 ,

wherein the working fluid is hydrogen.

4. The improvement of claim 3 , further comprising:

a hydrogen permeable cap capping the hot end of the Stirling engine; and

a lithium-hydride based thermal storage medium in contact with said hydrogen permeable cap and the hot side of said Stirling engine;

wherein the slow loss of hydrogen from the lithium-hydride is balanced by a slow gain from the Stirling engine hydrogen working fluid through said hydrogen permeable cap, whereby the hydrogen containment of the thermal battery is extended.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 7, 2016
From: THE REGENTS OF THE UNIVERSITY OF CALIFORNIA
To: LAWRENCE LIVERMORE NATIONAL SECURITY, LLC
Reel/Frame 038223/0097 →
CONFIRMATORY LICENSE Recorded Sep 24, 2014
From: LAWRENCE LIVERMORE NATIONAL SECURITY, LLC
To: U.S. DEPARTMENT OF ENERGY
Reel/Frame 033804/0719 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 4, 2007
From: REGENTS OF THE UNIVERSITY OF CALIFORNIA, THE
To: LAWRENCE LIVERMORE NATIONAL SECURITY, LLC
Reel/Frame 020012/0032 →