This application relates to a gas controlled engine and more particularly to a closed loop air pressure regulated force generating system that uses air to generate engine propulsion.
Conventionally, engines, or simply just motors, are controlled by gas combustion. Also, presently there are many electric motors in existence as well especially with the advent of electric cars which continue to grow in popularity. However, there remains many other uses for engines other than motor vehicles, such as power generators, small engine devices, factory machinery, household and yard devices, etc., which could afford to have less torque and power and could be run efficiently without high power combustion engines.
One embodiment of the present application may include an apparatus that has a plurality of pressurized air tanks controlled by a compressor. Also, an engine is coupled to the tanks via air piping which permits the changes in pressure to cause the air to operate the pistons and create movement within the engine in a continuous state of operation.
It will be readily understood that the components of the present application, as generally described and illustrated in the figures herein, may, be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of an apparatus, and system configuration, as represented in the attached figures, is not intended to limit the scope of the application as claimed, but is merely representative of selected embodiments of the application.
The features, structures, or characteristics of the application described throughout this specification may be combined in any suitable manner in one or more embodiments. For example, the usage of the phrases “example embodiments”, “some embodiments”, or other similar language, throughout this specification refers to the fact that a particular feature, structure, or characteristic described in connection with the embodiment may be included in at least one embodiment of the present application. Thus, appearances of the phrases “example embodiments”, “in some embodiments”, “in other embodiments”, or other similar language, throughout this specification do not necessarily all refer to the same group of embodiments, and the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments.
Additionally, to increase torque, each cylinder can be fired singularly or in a double/quadruple capacity depending on the needed torque. During retraction, more air can be generated by using the hydraulic piston over air cylinder 106, chamber B of the cylinder can compress new air into the system. As the exhaust air is captured into the low pressure tank 101, air compressor 103 moves the low pressure air up into the high pressure tank 102. The system repeats the process autonomously without requiring additional energy sources.
This engine configuration can be many different designs including a 90 degree ‘V’ design, an in-line design, a flat engine design, a radial engine design, and a scissoring engine design. The compressor 103 can be operated electrically in a standalone system as well as it can be incorporated within the system. It could run with or without air tanks, only with compressor. The compressor may be a piston type compressor and/or a screw type compressor. To increase rpm, the transmission 125 is attached to the rear of the engine, or to the front of the engine, or front and rear of the engine simultaneously. The transmission will adjust the number of RPMs.
The hydraulic ram cylinder head adapter 108 receives the 107 cylinder. The air cylinder control valve 109 controls pressurizing the hydraulic piston over air cylinder 106 and depressurizing item 106 and 107. The hydraulic control valve 110 permits the oil to return to a home position freely. The air check valve permits the air to travel in one direction. Crank shaft 112 is the main rotating shaft of the engine 400. Connecting rods 113 connect the crank shaft 112 to the ram cylinder rod adapter 114, which connects the ram cylinder 107 to the connecting rods 113.
The timing gear assembly with chain 115 synchronizes the crank shaft 112 to the cam shaft 116, which controls the firing order and the duration of the air and hydraulic valves. Solid lifters 117 roll over the cam to lift the push rods to an up and down type of movement. Push rod and spring assembly 118 connects to the cam shaft. The linear bearing 119 maintains the push rods into position.
At an initial time #1 and #6 ram cylinders are in top dead center (TDC) position. 109 provides air to the #1 cylinder and the #6 cylinder, 2 cylinders are energized with 100 psi air pressure from item 109 air control valve to 106 (AHU) chamber A. This action boosts the air pressure to hydraulic pressure and intensifies it by 10 times or more. This hydraulic pressure is sent by high pressure hydraulic hose to ram cylinder 107 chamber A this action moves the ram cylinder rod in a downward movement. As the rod moved the connecting rod, item 114 is connected to crankshaft 112 from T.D.C. to a 90 degree position, then 2 sets of cylinders are energized including the #8 and the #5 cylinder, this action will move the crank shaft item number 112 an additional 90 degrees clockwise, at this time the #1 and #2 cylinders reach the 180 degree mark on the crank shaft. At the end of the stroke (180 degrees) after top dead center (ATDC), the 112 crank shaft is connected with the timing chain and sprocket assembly 115 to camshaft 116, this chain and sprocket assembly could operate as a 1-to-1 ratio and the camshaft and 116 is a 90 degree design and the lobes are 180 degrees on and 180 degrees off on the cam lobes set of lifters 117. The lifters are rolling around the lobes causing the lifters to ascend and descend around the lobes. On the lifters there are a set of lifting rods spring assemble item 118 the spring presses the lifters to rotate on the lobes continuously. And the lifting rod assemble item 118 runs through a set of linear bearing items 119 which are mounted on item 108, this bearing will keep the rod in a true and accurate position all the way to connect hydraulic valve 110 and 109, which are mounted on top of each other in a single action ascending and descending movement. This will activate both valves simultaneously permitting the air in the hydraulic oil to change direction as the #1 and #6 cylinders are in a 180 degree location, the cam 116 reverses the air and hydraulic valves to switch directions. At this time, 106 chamber A is de-energized. By de-energizing 106, chamber A permits the piston inside the 106 to be free and return home position without restriction.
As cylinders 1 and 6 are de-energized and start to retreat to a home position simultaneously, new sets of cylinders are energized including the #4 cylinder and the #7 cylinder. Energized cylinders rotate the crankshaft 112 an additional 90 degrees from a current position. At this time, the #8 and #5 cylinders start to retreat to a home position. At the same time, new sets of cylinders are energized including the #2 and #3 cylinders as they rotate the crankshaft an additional 90 degrees, the #1 and #6 cylinders are back to a TDC position and the cycle begins to repeat.
At all times, 4 cylinders are in force and 4 cylinders are in retreat. Every 90 degrees, a set of 2 cylinders are in rotation, including on in force and off in retreat.
Retreating of the cylinders works as the engine rotates the #1 cylinder and the #6 cylinder are 180 degrees after TDC. Each designated set of cylinders will return to a home position by connecting rod item 114, which forces the ramrod to retreat to a home position on item 107. In operation, oil in the ram cylinder in chamber A is forced back to a hydraulic piston over air cylinder 106. This action will retreat the air piston to a return to home position as well. At this point, air cylinder 106 is ready to be re-energized for another cycle. Another way to retract the cylinders to a home position is to energize the B chamber of 106 and 107.
One example of how the exhaust is captured provides that after de-energizing the air cylinder 106, chamber A, the exhaust is captured back by returning the pressurized air to the exhaust manifold item 104. On top of each returning exhaust line, there is an air check valve 111. This will not permit the exhaust air to return into the system. As the exhaust enters into 104, the exhaust manifold, the pressurized air returns to the low PSI tank 101. At that time, the air compressor 103 will move the low pressure air from the 101 tank to the high pressure tank 102, which concludes the cycle which then repeats.
It will be readily understood that the components of the application, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations. Thus, the detailed description of the embodiments is not intended to limit the scope of the application as claimed, but is merely representative of selected embodiments of the application.
Therefore, although the application has been described based upon these preferred embodiments, it would be apparent to those of skill in the art that certain modifications, variations, and alternative constructions would be apparent, while remaining within the spirit and scope of the application. In order to determine the metes and bounds of the application, therefore, reference should be made to the appended claims.
This application claims the benefit of PCT Ser. No. PCT/US16/36412 filed on Jun. 8, 2016 and entitled PRESSURE CONTROLLED HYDRAULIC ENGINE, which claims the benefit of U.S. Provisional Patent Application No. 62/172,526, filed on Jun. 8, 2015 and entitled PRESSURE CONTROLLED HYDRAULIC ENGINE. The subject matter of these applications are hereby incorporated by reference herein in their entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/US2016/036412 | 6/8/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2016/200912 | 12/15/2016 | WO | A |
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4052850 | Mohaupt | Oct 1977 | A |
4769988 | Clark, Jr. | Sep 1988 | A |
4896505 | Holleyman | Jan 1990 | A |
5515675 | Bindschatel | May 1996 | A |
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6065945 | Zamzow | May 2000 | A |
6629573 | Perry | Oct 2003 | B1 |
8360743 | Walters | Jan 2013 | B2 |
9470110 | Stroganov | Oct 2016 | B2 |
Number | Date | Country | |
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20180202292 A1 | Jul 2018 | US |
Number | Date | Country | |
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62172526 | Jun 2015 | US |