1. Field of Invention
This invention pertains generally to engines and generators and, more particularly, to an internal explosion engine and generator using non-combustible gases.
2. Related Art
An internal explosion engine is generally similar in principle to an internal combustion engine except that it uses non-combustible gases such as air, oxygen, nitrogen or inert gas(es) instead of the combustible gases which are used in internal combustion engines.
Prior to operation, the gas for operating an internal explosion engine is placed in the explosion chamber of the engine, and the chamber is sealed. During operation, the gas in the explosion chamber is repeatedly compressed, ionized, explosively expanded and contracted to move a piston or rotor or other movable device to convert kinetic energy to mechanical or electrical energy.
Once the gas has been loaded into the explosion chamber, the engine can operate for extended periods of time without additional fuel. There is no need for fuel intake on each cycle of operation, as in an internal combustion engine, and there is no exhaust.
Examples of internal explosion engines of the prior art are found in U.S. Pat. Nos. 3,670,494 and 4,428,193.
It is, in general, an object of the invention to provide a new and improved internal explosion engine and generator.
Another object of the invention is to provide an internal explosion engine and generator of above character which overcomes the limitations and disadvantages of the engines and generators heretofore provided.
These and other objects are achieved in accordance with the invention by providing an internal explosion engine and generator which has an explosion chamber, a movable member forming one wall of the chamber, a charge of non-explosive gas sealed inside the chamber, means for repeatedly igniting the gas in an explosive manner to drive the movable member from a position of minimum volume to a position of maximum volume, means for returning the movable member from the position of maximum volume to the position of minimum volume, and means coupled to the movable member for providing electrical energy in response to explosion of the gas.
In one disclosed embodiment, the movable member is a piston connected to a crankshaft, and it is returned to the position of minimum volume by a flywheel on the crankshaft. In another, two pistons are connected back-to-back in a hermetically sealed chamber to prevent loss of the explosive gas. In one embodiment, the electrical energy is produced by a generator connected to the crankshaft, and in the other it is produced by a coil positioned near a magnet which moves with the pistons.
As illustrated in
An inlet port 18 is formed in the cylinder head for introducing a charge of gas into the explosion chamber, and the admission of gas through the port is controlled by a valve assembly 19.
The piston is connected to a crankshaft 21 by a connecting rod 22, and the crankshaft includes a counterweight or flywheel 23. In operation, the piston is driven in a downward direction by the explosion of the gas in the chamber and returned to the firing position by energy stored in the flywheel. The lower end of cylinder 13 is closed by a crankcase housing 24.
The crankshaft is connected to the shaft 26 of a generator 27 located outside the crankcase housing by a coupling 28. As discussed more fully hereinafter, the generator can also be driven as a motor for use in starting the engine.
In the embodiment illustrated, valve assembly 19 is a one-way check valve which allows gas to pass into but not out of the explosion chamber through inlet port 18. The valve assembly is shown in greater detail in
Electrodes are mounted in the head for igniting the gas in the chamber. A high frequency electrode 43 is positioned axially of the chamber and connected to a radio frequency generator 44 for ionizing the gas to form a plasma. Electrodes 46–49 are spaced about electrode 43, with electrode 46 being connected to the secondary winding 50 of a spark coil 51 and electrodes 47–49 being connected to a capacitor 52. A contact pin 53 projects from the face of the piston in alignment with electrode 43.
Piston 12 and end plate or head 16 are fabricated of a ferro-magnetic material such as Grade 416 stainless steel, and cylinder 13 is fabricated of a non-ferrous material such Grade 303 stainless steel. A coil 54 is disposed about the outer portion of the cylinder and coupled magnetically with the piston to form a reluctance generator.
Means is provided for detecting when the piston is in its top dead center (TDC) or minimum volume position. This means includes a magnet 56 which is mounted on the counterweight or flywheel portion 23 of crankshaft 21 and a Hall switch 57 which is mounted in a stationary position in the crankcase and actuated by the magnet when it comes into proximity to the switch.
Power for operating generator 27 as a motor to start the engine is provided by batteries 59 which, in the embodiment illustrated, are mounted inside the housing of a controller 61 for the generator. The batteries are connected to the motor by a normally open starting switch 62.
The batteries also provide power for RF generator 44 and for the electrodes 46–49 which ignite the gas in the chamber, with energization of those electrodes being controlled by a relay 63. The application of power to the RF generator is controlled by an on/off switch 64, and energization of relay coil 65 is controlled by the on/off switch and by Hall switch 57 which is connected between the on/off switch and the relay coil.
The relay has a first set of contacts 66 which switch capacitor 52 between the power source and electrodes 47–49, and a second set of contacts 67 which connect the primary winding 68 of spark coil 51 to the power source.
The batteries are charged with the current produced in coil 54 by the reluctance generator. That coil is connected to the input of a power rectifier 69, and the output of the rectifier is connected to the batteries.
Prior to operation, a charge of air is introduced into explosion chamber through check valve 19 and inlet port 18. To start the engine, on/off switch 64 is closed, thereby energizing RF generator 44 and the primary winding of spark coil 51 and applying charging current to capacitor 52, and starter switch 62 is closed to energize generator 27 as a starting motor. The gas in the chamber is ionized by the RF power applied to electrode 43 to form a plasma.
As the piston makes its upward stroke, the air is compressed and heated, and toward top dead center, the air is ionized by the. RF power applied to electrode 43 to form a plasma. When the piston is at or near top dead center, Hall switch 57 closes, energizing relay coil 65. When the relay coil is energized, contacts 66 apply the charge which has built up on capacitor 52 to electrodes 47–49, and contacts 67 open to interrupt the current in the primary winding of spark coil 51, producing a high voltage discharge between spark electrode 46 and the contact pin 53 on the piston.
The spark from electrode 46 and the current from electrodes 47–49 flowing through the ionized air ignite the air, causing it to explode and produce a lightning-like pressure wave, with ultraviolet light, ozone and heat. That pressure wave drives the piston in a downward direction, turning crankshaft 21 and generator 27, storing mechanical energy in the flywheel and producing electrical energy from the generator.
After the piston reaches its maximum volume or bottom dead center (BDC) position the mechanical energy stored in the flywheel causes the crankshaft to continue rotating, thereby driving the piston back toward top dead center.
The same charge of air is ignited over and over again for an extended period of time, and to the extent that any of the air is lost past the piston rings, it is automatically replenished by air entering the chamber through the check valve. Thus, with the piston on its down stroke, if the pressure in the chamber drops below the level set by spring 38, ball 36 moves away from its seat, allowing air to enter the chamber through the inlet port. During the upstroke, the pressure in the chamber holds the bail tightly against the seat, sealing the air in the chamber.
The embodiment of
The piston assembly includes a pair of pistons 12 which are connected together in back-to-back fashion by a sleeve 77, with rings 14 providing a seal between the pistons and the cylinder. The pistons have central contact pins 53, and each of the explosion chambers has an inlet port 18 and electrodes 43, 46–49 for ionizing and igniting the gas.
As in the embodiment of
Sleeve 77 carries magnets 56 which actuate Hall switches 57 mounted outside cylinder 74 to determine when the pistons are at or near their top dead center (TDC) positions. A grounding contact 78 carried sleeve 77 makes sliding contact with the wall of the cylinder to maintain the pistons and contact pins 53 at ground potential.
The piston assembly also includes a relatively large permanent magnet 81 which is carried by sleeve 77 midway between the pistons. A ferro-magnetic core structure 82 provides flux coupling between magnet 81 and stator coils 83, 84 which are located outside the cylinder.
The core structure includes a pair of generally C-shaped cores 86, 87, each of which has pair of relatively short inner arms 86a, 87a which abut against the upper and lower surfaces of cylinder 74 and an outer arm 86b, 87b which is spaced laterally from the cylinder. The ends of the inner arms which abut against the cylinder have a concave curvature which matches the convex curvature of the outer wall of the cylinder, and coils 83, 84 are wound about outer arms of the cores. The cores are formed in two sections, with a split 88 across the outer arms to facilitate assembly.
Steel laminations 89 are embedded in the cylinder wall in contact with the short arms of the cores to complete the magnetic circuit. The laminations are hermetically sealed into the cylinder wall, and in one presently preferred embodiment they are stacks of silicon steel laminations with a thickness of 0.005 inch and a layer of nickel plating less than 0.001 inch thick sealing the stacks.
The stator coils can be utilized both as the windings of a motor for starting the engine and thereafter as the windings of a generator in which an electric current is produced as the piston assembly oscillates back and forth within the cylinder.
Since the cylinder is hermetically sealed, any gas leaking past the rings of the pistons will remain within the engine, rather than being lost to the outside environment as in the embodiment of
In addition to air, suitable gases for use in the embodiment of
With the gas hermetically sealed within the engine, it is not necessary to replenish the gas as often as it would be if the engine were not sealed, and inlet port 18 can be closed with the plug assembly 91 of
Plug assembly 91 includes a body or bushing 92 with a hollow interior 93 which is filled with a rubber insert 94. The inner end of the valve body is threaded into the port, and a cap 96 is threaded onto the enlarged outer end of the body to retain the insert in the plug. A gasket 97 provides a seal between the enlarged portion of the plug body and the end plate or head 16.
Operation and use of the embodiment of
As the magnet carried by the piston assembly moves back and forth within the gap in the core structure, the alternating flux it produces is coupled to coils 83, 84 to produce the output current in the generator windings.
The invention has a number of important features and advantages. It can use explosive fuel mixtures such as air, inert gases and other non-combustible gases which can be rapidly expanded and contracted multiple times to convert kinetic energy into electrical and/or mechanical power. The engine can have one or more explosion chambers with a piston forming a movable wall for changing the volume of each.
The operating gas is preloaded into the chambers, the inlet ports are sealed, and the engine an be operated with the same gas load over long periods of time and multiple explosive expansions and contractions at various frequencies, e.g. 30–60 cycles per second or more, without adding gas to the chambers.
In one disclosed embodiment, the loss of gas due to leakage is prevented by enclosing the engine in a hermetically sealed enclosure. In another, a check valve in the inlet port allows the gas in the chambers to be automatically replenished when the pressure in the chambers drops below a predetermined level. The hermetic sealing is particularly important and desirable if the engine is operated in environments such as outer space or underseas where replenishment gases may not be readily available.
The invention permits a wide range of design flexibility and can provide compact power supplies ranging in capacity from a few kilowatts to multiple megawatts, and it can be utilized in a wide variety of applications.
It is apparent from the foregoing that a new and improved internal explosion engine and generator has been provided. While only certain presently preferred embodiments have been described in detail, as will be apparent to those familiar with the art, certain changes and modifications can be made without departing from the scope of the invention as defined by the following claims.
This application is based upon Provisional Application No. 60/462,993, filed Apr. 14, 2003, the priority of which is claimed.
Number | Name | Date | Kind |
---|---|---|---|
2984067 | Morris | May 1961 | A |
3237847 | Wilson | Mar 1966 | A |
3670494 | Papp | Jun 1972 | A |
3680431 | Papp | Aug 1972 | A |
4306414 | Kuhns | Dec 1981 | A |
4416113 | Portillo | Nov 1983 | A |
4428193 | Papp | Jan 1984 | A |
5899071 | Stone et al. | May 1999 | A |
6272855 | Leonardi | Aug 2001 | B1 |
6739131 | Kershaw | May 2004 | B1 |
Number | Date | Country | |
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20040200216 A1 | Oct 2004 | US |
Number | Date | Country | |
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60462993 | Apr 2003 | US |