Variable geometry toroidal engine

Internal-combustion engines – Rotary – With fuel injection means

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C123S206000, C123S289000

Reexamination Certificate

active

06546908

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a rotary engine, and more particularly to an internal combustion engine in which a piston assembly orbits continuously within a toroidal chamber.
2. Description of the Prior Art
The conventional technology for internal combustion engines is the reciprocating piston engine which has evolved and been refined over a period of some 125 years. That kind of engine is, however, subject to a number of widely recognized, severe limitations and constraints in power generation efficiency.
The reciprocating piston engine does not produce rotary motion with a constant torque arm but, rather, uses a crankshaft to convert reciprocating motion of a piston into rotary motion, with the attendant disadvantage of a variable torque arm that is drastically reduced in the top dead centre region of the piston when combustion is initiated. The result is a lack of torque and power and a reduction of engine efficiency.
Many attempts have been made to produce a workable “toroidal piston engine” which provides revolving pistons mounted to a central disk to produce the desired constant torque arm, Examples of this kind are to be found in U.S. Pat. No. 4,035,111 (Cronen, Sr.); U.S. Pat. No. 4,242,591 (Harville); U.S. Pat. No. 4,683,852 (Kypreos-Pantazis); U.S. Pat. No. 4,753,073 (Chandler); U.S. Pat. No. 5,046,465 (Yi); U.S. Pat. No. 5,203,297 (Iversen); and U.S. Pat. No. 5,645,027 (Esmailzadeh).
In common with all positive displacement combustion engines, the toroidal engine must incorporate means both for compressing the intake charge and for containing the hot expanding gasses that are generated by combustion. In keeping with this principle, previous inventors of toroidal engines have usually made provision for some sort of “valve” to intercept the path of the advancing piston, to retract and so allow the piston to pass by, then to close behind the piston.
In this manner, the intake charge is compressed between the advancing piston and the valve blocking its path. The compressed charge is then diverted into a combustion chamber, the valve is briefly opened to allow the piston to pass by, the valve closes and the ignited combustion gases, released from the combustion chamber, expand between the closed valve and the retreating rear face of the piston. Accordingly, each piston is propelled on a circular orbit as it passes through the valve aperture.
My study of the prior art, experiments which I have conducted and computer-assisted thermodynamic modelling results have led me to conclude that the reason none of these approaches has achieved commercial success stems from general failure to address a fundamental problem inherent in the operation of toroidal engines, namely, the loss in compression potential and the loss in air mass which occurs between the front face of a piston and a valve intersecting the toroidal chamber in advance of that piston and, likewise, the pressure loss which occurs between the rear face of the piston and the intersecting valve behind that piston. Thus, that air mass between the advancing face of a piston and the intersecting valve which is not diverted into the combustion chamber, but escapes into the toroidal chamber, is “lost” to the useful generation of work.
In a toroidal piston engine of this general kind, some mechanism is required for opening and closing a valve seat in advance of and then behind a moving piston to gain the mechanical energy resulting from compression, ignition and expansion. Any such mechanism will take a certain amount of time to open or close and, to that extent, the piston will have travelled further in its angular rotary motion, creating and enlarging a “residual volume” (or, equivalently, “dead volume”). This effect can lead to a loss in compression ratio, a loss in air mass, and concomitant loss of expansion pressure, in turn resulting in significant inefficiency and loss of power.
Hitherto, the designers of toroidal engines have apparently acted on the assumption that merely to block the path of the advancing piston with a valve and to trap the intake charge will generate adequate compression, with no loss of air mass, and adequate pressurization of the toroidal chamber. Prior known engines of this kind have never achieved this desired result, however, as each employs one or another intersecting valve opening-and-closing mechanism which is too slow. This results in unacceptably large residual volumes produced ahead of and behind the valve by the rapidly moving pistons.
As a specific example, the aforementioned patent to Kypreos-Pantazis discloses a rotating piston internal combustion engine in which the mechanism for opening and closing the toroidal chamber in advance of and behind a piston comprises separating walls adapted to move radially inwardly and outwardly to divide the toroid inner space into sub-chambers. The means to withdraw the separating walls to allow the passage of a piston and thereafter reinsert it is typically a cam coupled mechanically to the central output shaft of the engine to withdraw the walls periodically from the toroid chamber as the shaft and piston assembly rotates, and return springs for reinserting the walls into the toroid chamber.
A practical problem with that and with other prior art toroidal engines is that their opening-and-closing mechanisms create significant residual volume between the front and rear of the piston, resulting in entirely unsatisfactory performance. I have employed thermodynamic mathematical modelling to demonstrate the inevitability of the practical failure of toroidal engines using such mechanisms. All of the prior art exemplified in the patent literature employs either planar sliding valves or planar rotating valves, which are required to move in reciprocating fashion owing to the configuration of the toroid. At the high rotational speeds required by an engine cycle, reciprocating mechanisms are very difficult to seal and to maintain.
The same thermodynamic mathematical modelling and analysis also revealed a surprisingly drastic improvement in the performance of toroidal piston engines where the residual volumes are contrived to be made as small as possible. Indeed, the dead volume would ideally be zero but as a practical matter, of course, the moving piston and the valve in its closed position must never physically contact each other.
The practical conclusion of my analysis is that a toroidal engine of this general kind becomes usefully workable only where the volume in the compression phase of the cycle (between the piston and valve) is physically reduced sufficiently to generate a compression ratio approximating the value achieved in conventional reciprocating piston engines and the loss of air mass is minimized to achieve an efficiency comparable to conventional engine technology. That ratio, in an SI engine, typically lies in the range of between 8:1 and 12:1 or, in the case of the Diesel engine, approximately 18:1.
The fundamentally different approach I have taken to improving the performance of toroidal piston engines of this kind is to alter the geometry of the chamber section formed between valve and piston to minimize the residual volumes and thereby attain the very significant improvement in performance which was predicted by the analysis of models. For that reason, I refer to my invention as the “variable geometry toroidal engine” or VGT engine. As discussed below, the aforementioned geometry can be varied by employing a rotating disk valve with an aperture that periodically intersects the toroidal chamber and minimizing the residual volumes between piston and valve.
In a first principal embodiment the reduction in the residual volumes is achieved by matching the three-dimensional shape of the piston to the valve opening. According to a second principal embodiment, it is achieved by providing a piston which is mechanically expandible and contractible, to minimize the residual volumes between the piston and the valve just prior to opening of the valve and just following shutting of the valve.
SU

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Variable geometry toroidal engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Variable geometry toroidal engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Variable geometry toroidal engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3070361

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.