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Gerotor apparatus for a quasi-isothermal brayton cycle engine

a cycle engine and quasi-isothermal technology, applied in the direction of machines/engines, rotary/oscillating piston pump components, liquid fuel engines, etc., can solve the problems of difficult to achieve perfect erickson cycle, low power density, difficult to achieve internal combustion, etc., to achieve simple gas flow paths, reduce power consumption, and reduce the effect of bearing load

Inactive Publication Date: 2010-01-07
STARROTOR CORPORATION +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The invention is a gerotor apparatus that includes two gerotors and a synchronizing system to synchronize their rotation. The synchronizing system includes a cam plate and an alignment plate, which interact to synchronize the rotation of the two gerotors. The technical effects of the invention include a more compact and lightweight engine with simplified gas flow paths, less loads on bearings, and lower power consumption. The invention also introduces a simpler method for regulating leakage from gaps and prevents heat transfer from the gas to the oil, or entrainment of oil into the gas. Additionally, the drive mechanisms have small backlash and low wear.

Problems solved by technology

The Otto Cycle engine is an inexpensive, internal combustion, low-compression engine with a fairly low efficiency.
In practice, a perfect Erickson cycle is difficult to achieve because isothermal expansion and compression are not readily attained in large, industrial equipment.
It features low power density, mechanical complexity, and difficult-to-achieve constant-temperature compressor and expander.
It has a higher power density than the Carnot cycle, but it is difficult to perform the heat exchange, and it is difficult to achieve constant-temperature compression and expansion.
In practice, real engines have “irreversibilities,” or losses, associated with friction and temperature / pressure gradients.
These devices are generally suitable for aviation in which aircraft operate at fairly constant speeds; they are generally not suitable for most transportation applications, such as automobiles, buses, trucks, and trains, which must operate over widely varying speeds.
Further, the Otto and Diesel cycle engines lose efficiency because they do not completely expand high-pressure gases, and simply throttle the waste gases to the atmosphere.

Method used

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  • Gerotor apparatus for a quasi-isothermal brayton cycle engine
  • Gerotor apparatus for a quasi-isothermal brayton cycle engine
  • Gerotor apparatus for a quasi-isothermal brayton cycle engine

Examples

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first embodiment

[0051]FIG. 10 illustrates example cross-sections of outlet valve plate 40f taken along line C of FIG. 9 according to two embodiments of the invention. In the first embodiment, C1, outlet valve plate 40f includes an outlet opening 224f allowing fluids to exit fluid flow passageways 32f into second chamber portion 204f. In some embodiments in which gerotor apparatus 10f is a compressor, the area of outlet opening 224f is smaller than the total area of inlet opening(s) 214f formed in inlet valve plate 41f (see FIG. 11, discussed below).

second embodiment

[0052]In the second embodiment, C2, outlet valve plate 40f includes an outlet opening 224f, as well as one or more check valves 230f, allowing fluids to exit fluid flow passageways 32f into second chamber portion 204f. Providing one or more check valves 230f allows various types of fluids 192f to be run through gerotor apparatus 10f, such as gasses, liquids (e.g., water), and gas-liquid mixtures. The area of outlet opening 224f may be smaller than the total area of inlet opening(s) 214f formed in inlet valve plate 41f (see FIG. 11, discussed below). The total area of outlet opening 224f and check valves 230f may be approximately equal to the total area of inlet opening(s) 214f formed in inlet valve plate 41f. The appropriate check valves 230f may open to discharge the particular fluid 192f running through gerotor apparatus 10f. For example, if a low compression ratio is required for the application, all of the check valves 230f may open. If a high compression ratio is required, none...

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PUM

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Abstract

According to one embodiment of the invention, a gerotor apparatus includes a first gerotor, a second gerotor, and a synchronizing system operable to synchronize a rotation of the first gerotor with a rotation of the second gerotor. The synchronizing system includes a cam plate coupled to the first gerotor, wherein the cam plate includes a plurality of cams, and an alignment plate coupled to the second gerotor. The alignment plate includes at least one alignment member, wherein the plurality of cams and the at least one alignment member interact to synchronize a rotation of the first gerotor with a rotation of the second gerotor.

Description

RELATED APPLICATIONS[0001]This application claims benefit under 35 U.S.C. § 119(e) of U.S. Provisional Application Ser. No. 60 / 538,747, entitled “QUASI-ISOTHERMAL BRAYTON CYCLE ENGINE,” filed Jan. 23, 2004.TECHNICAL FIELD OF THE INVENTION[0002]The present invention relates to a gerotor apparatus that functions as a compressor or expander. The gerotor apparatus may be applied generally to Brayton cycle engines and, more particularly, to a quasi-isothermal Brayton cycle engine.BACKGROUND OF THE INVENTION[0003]For mobile applications, such as an automobile or truck, it is generally desirable to use a heat engine that has the following characteristics: internal combustion to reduce the need for heat exchangers; complete expansion for improved efficiency; isothermal compression and expansion; high power density; high-temperature expansion for high efficiency; ability to efficiently “throttle” the engine for part-load conditions; high turn-down ratio (i.e., the ability to operate at widel...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): F01C1/10F01C11/00F01C17/04F01C17/06F01C19/08F01C21/00F01C21/04F01C21/06F02G3/00
CPCF01C1/104F01C11/004F01C17/04F01C17/06F01C19/085F04C15/0003F01C21/04F01C21/06F04C2/10F04C11/003F01C21/008F01C1/10F01C21/00
Inventor HOLTZAPPLE, MARK T.RABROKER, GEORGE A.ROSS, MICHAEL K.
Owner STARROTOR CORPORATION
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