Stirling engine for an emission-free aircraft

Patent metadata

Field	Value
Publication number	US-9945361-B2
Application number	US-201514877102-A
Country	US
Kind code	B2
Filing date	Oct 7, 2015
Priority date	Dec 22, 2011
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes a drive device structured and arranged to generate thrust, a lift device structured and arranged to generate lift, and a heat engine structured and arranged to convert thermal energy into kinetic energy to drive the drive device. The heat engine includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

First claim

What is claimed:

1. An aircraft with at least one heat engine, the aircraft comprising:
a wing and a fuselage;
a working chamber of the at least one heat engine, having a top and an underside filled with a working gas, being located in at least one of the wing and fuselage;
a displacer of the at least one heat engine being structured and arranged for pivoting movement between the top and the underside of the working chamber to a define a first and a second chamber region; and
a heating region of the at least one heat engine being located in a region of the top of the working chamber to receive solar thermal radiation through the at least one of the wing and fuselage to heat the working gas,
wherein the at least one of the wing and fuselage has an external skin that forms a wall of the working chamber.

2. The aircraft according to claim 1 , the heat engine comprising a flat-plate Stirling engine.

3. The aircraft according to claim 1 , further comprising:
a regenerator of the at least one heat engine being structured and arranged in the working chamber to collect and deliver thermal energy contained in the working gas;
a rotatable inertia element of the at least one heat engine comprising at least one of a propeller or a flywheel; and
a driver of the at least one heat engine being structured and arranged to be connectable to the rotatable inertia element to drive a thrust drive.

4. The aircraft according to claim 1 , further comprising an electric storage structured and arranged to store and deliver electric energy generated by a power-generator coupled to the heat engine to convert kinetic energy into electric energy.

5. An aircraft with an emission-free drive, comprising:
an aircraft thruster structured and arranged to generate thrust force on the aircraft;
a wing structured and arranged to impart lift on the aircraft;
a fuselage; and
a heat engine, which is structured and arranged to convert thermal energy into kinetic energy to drive the aircraft thruster, comprising at least one flat-plate Stirling engine drivable by solar thermal radiation,
wherein the at least one flat-plate Stirling engine comprises:
a working chamber having a top and an underside; and
a displacer structured and arranged for pivoting movement between the top and the underside of the working chamber to a define a first and a second chamber region,

wherein at least one of the wing and the fuselage has an external skin that forms a wall of the working chamber.

Assignees

• Eads Deutschland Gmbh

Inventors

• Seifert Jost

Classifications

• B64D27/06

  within, or attached to, wings · CPC title

• B64D27/04

  of piston type · CPC title

• F03G6/068 Primary

  having other power cycles, e.g. Stirling or transcritical, supercritical cycles; combined with other power sources, e.g. wind, gas or nuclear · CPC title

• F02G1/043 Primary

  the engine being operated by expansion and contraction of a mass of working gas which is heated and cooled in one of a plurality of constantly communicating expansible chambers, e.g. Stirling cycle type engines · CPC title

• B64C1/16

  specially adapted for mounting power plant · CPC title