BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a schematic view of schematic view of the universal hyperbaric mechanism in the form of a thermal engine system with three double acting reciprocating piston assemblies and a gas turbine assembly.
FIG. 2 is a schematic view of the universal hyperbaric mechanism of FIG. 1 modified with linear power machines.
FIG. 3 is a schematic view of the universal hyperbaric mechanism of FIG. 2 with four cylinders and three double acting reciprocating piston assemblies, including linear power machines.
FIG. 4 is a schematic view of the universal hyperbaric mechanism of FIG. 3 with ultra high pressure, differential stage linear compressors and other linear power machines.
FIG. 5 is a schematic view of the universal hyperbaric mechanism in an engine system at maximum potential, forming multi symmetric synergetic engine.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
In FIG. 1, the universal hyperbaric mechanism, generally referenced by A, is an engine system with a central cylinder 1 with two opposed pistons 2 and 3, having opposed piston faces 4 and 5 acting in the opposite end cylinders 6 and 7. The pistons 2, 3, 4 and 5, are articulated with cross arms 8 and 9, provided with cross bars 10, 11, 12 and 13, that reciprocate in guides 14, 15, 16, 17. The cross arms 8 and 9 are also provided with extended connecting arms 18 and 19, which are pivotally linked with connecting rods 20 and 21 that drive the crankshaft 22. The sliding cross bars 10, 11, 12 and 13 in the guides 14, 15, 16 and 17, control the torque during operation. The engine assembly A is also associated with a thermal electric gas turbine assembly having a gas turbine 23, a compressor 24, and an electric machine 25. The exhaust gases from the linear engine subsystem are collected in the exhaust reservoir 26 drive the turbine 23 and the supercharging air is collected in the reservoir 27 for supply to the reciprocator.
The intake and exhaust for the central cylinder 1 are provided by port 28 for intake, and port 29 for combined intake and exhaust. The ports 30 and 31 are combined intake and exhaust ports for the opposite end cylinders 6 and 7. The central cylinder 1 is provided with fuel injectors 32, and the opposite end cylinders 6 and 7 are provided with fuel injectors 33 and 34. The sliding pistons 2, 3, 4 and 5 in these three cylinders are in permanent energy reciprocation with symmetric alternate cycles of compression and expansion perfectly dynamically balanced with zero inertial forces or vibrations. The combined power of the engine is produced by the totality of the actions provided by the engines' linear, and rotary members converted into mechanical and electrical power as required and as supplemented by the electrical power resulting from a positive balance of energy from the optimally operated gas turbine 23.
In FIG. 2, the engine system A described in FIG. 1 is modified and is generally indicated by B, wherein the transfer of power is made by linear links 35, 37, 39 and 41 to linear machines 36, 38, 40 and 42, which can be linear electric generators and/or any type of linear reciprocator machine that can use all the power produced.
In FIG. 3, the same engine system A described in FIG. 1 is modified and is generally indicated by C, wherein an additional engine cylinder 45 is located with a counter opposed piston 46 and double action piston 47, acting in opposite end cylinder 48, provided with combined intake-exhaust ports 49 and 50.
The articulated cross arms 51, 52, are connected with links bars 53 and 54, associated with the linear machines 55 and 56, connected by the articulation mounts 57a and 57b, with the cross arms 58a, 58b of the assembly with the double pistons 3 and 4.
The universal hyperbaric mechanism has four active engine cylinders with pistons acting two by two in double faced operations of opposed pistons in permanent dynamic balance, the two outer assemblies of double acting pistons counteracting the central assembly of double acting pistons. The central two cylinder opposed piston engine segment is working with a single flow, total intake-exhaust scavenging system, and the opposite end cylinders are working with loop scavenging total intake-exhaust system. The outer double faced pistons 3, 4, 46 and 47 are working in tandem, connected by the bars 53, 54, whereby the engine system has in totality six active piston faces.
In FIG. 4, the same engine system described in FIG. 3 is modified and generally indicated by D, wherein additional projecting end bars 61 and 62 are activating differential compressors 63, 64, 65, 67 for production of ultra high pressure gases or liquids.
In FIG. 5, the symmetric and synergetic engine system, generally indicated by E, has an engine core of the universal hyperbaric engine type described in FIG. 1 in which an additional two tandem symmetric pistons and cylinders are added and activated by two quadrilateral mechanisms shown schematically. The first quadrilateral mechanism is an assembly of articulated bars 70-71 and 72-73, connecting the assembly of double acting pistons 2 and 5 with the tandem double acting pistons 74, 75. The second quadrilateral mechanism is an assembly of articulated bars 77-78 and 79-80, connecting the assembly of double acting pistons 3 and 4 with the tandem double acting pistons 81, 82. Finally, each quadrilateral mechanism is reciprocating in the extreme opposite end cylinders 76 and 83. This engine system E with five activated engine cylinders and four assemblies of double acting pistons forms the highest level of power density with more than 1,000 hp/liter at the highest levels of pressure ratio 300/1-500/1, with a supercharging level of 10-20 and the highest thermal efficiency of 80%-90%.
Again, the energetic system of FIG. 5 is a turbo electric compound system with the integration of the basic engine assembly with an exhaust energy recovery system 26 and the associated gas turbine assembly with an ultra high pressure supercharging system of compressor 24, electric machine 25 and air reservoir 27. The quadrilateral system of FIG. 5 is the most flexible linear collector, carrier and supplier of power produced by all the engine reciprocator assemblies and cylinders available for use by linear electric power generators and other preferably linear devices. A substantial part of the power is delivered by the gas turbine with the electric machine 25 operating as a power generator on a shaft 84 co-axial with the gas turbine shaft. The driving crank shaft mechanism is reduced to the level of synchronizer with residual rotary mechanical power for starting the engine.
Patent Application
20080083328
