The invention relates to air compressors and more particularly to a pistonless rotary motor for air compressor, the pistonless rotary motor having grooves for flowing pressurized air to a compression stroke of a next compression chamber to that pressure of the incoming air can be increased.
The Wankel engine is a type of internal combustion engine using an eccentric rotary design to convert pressure into rotating motion. Compared to the reciprocating piston engine, the Wankel engine has more uniform torque, less vibration, and is more compact and weighs less. Wankel engines deliver three power pulses per revolution of the rotor. The output shaft uses toothed gearing to turn three times faster giving one power pulse per revolution. In one revolution, the rotor experiences power pulses and exhausts gas simultaneously. For comparison, in a two-stroke piston engine there is one power pulse for each crankshaft revolution and, in a four-stroke piston engine, one power pulse for every two revolutions.
In a typical pistonless rotary motor for air compressor, at a compression stroke when the rotor reaches a top dead center, exhausts are closed and volume of a compression chamber is decreased to a minimum. Air resistance of a next intake stroke can be increased greatly if there is no means to release the remained pressurized air. As a result, performance of the air compressor is significantly decreased. Thus, the need for improvement still exists.
It is therefore one object of the invention to provide a pistonless rotary motor comprising a housing including two axially spaced end walls, a peripheral wall extending between the end walls together with the end walls to form a rotor cavity, two opposite, radially spaced intakes, and two opposite radially spaced exhausts; and a triangular rotor rotatably disposed in the rotor cavity and including three peripheral faces with an apex portion formed between any two adjacent peripheral faces, the apex portions being in sealing engagement with an inner surface of the peripheral wall to form three moving compression chambers in the rotor cavity, volumes of the compression chambers being configured to change as the rotor rotates eccentrically; wherein the housing further comprises two opposite, radially spaced first grooves in the peripheral wall and two opposite, radially spaced second grooves in the peripheral wall; wherein the first groove is proximate the intake and the second groove is proximate the exhaust; wherein the first grooves are disposed at a top dead center of the rotor relative to the rotor cavity and configured to release air having a first pressure when the rotor revolves eccentrically; and wherein the second grooves are disposed the top dead center of the rotor relative to the rotor cavity when the rotor revolves eccentrically and configured to release air having a second pressure.
Preferably, the first pressure is greater than the second pressure.
The above and other objects, features and advantages of the invention will become apparent from the following detailed description taken with the accompanying drawings.
Referring to
Characteristics of the invention are detailed below. Two opposite, radially spaced first grooves 161 and two opposite, radially spaced second grooves 162 are provided in the peripheral wall 11. The first groove 161 is proximate the intake 141 and the second groove 162 is proximate the exhaust 142. Specifically, the first grooves 161 are provided at a top dead center of the rotor 20 relative to the rotor cavity 13 and configured to release pressurized air. The second grooves 162 are provided at the top dead center of the rotor 20 relative to the rotor cavity 13 and configured to release exhaust.
In a revolving operation of the rotor 20, air flows into the compression chambers 15 via the intakes 141. At a first stage of an exhaust stroke, the first grooves 161 are open and pressurized air remained in the first grooves 161 flows to a compression stroke of a next compression chamber 15 for increasing pressure of the incoming air (see
At a second stage of the exhaust stroke, the first grooves 161 are closed and air remained in the second grooves 162 flows to an intake stroke of a previous compression chamber 15 for release (see
It is envisaged by the invention that exhaust is prevented from being disadvantageously pressurized in the exhaust stroke to decrease compression performance.
While the invention has been described in terms of preferred embodiments, those skilled in the art will recognize that the invention can be practiced with modifications within the spirit and scope of the appended claims.
Number | Name | Date | Kind |
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3452643 | Pratt | Jul 1969 | A |
4297090 | Hoffmann | Oct 1981 | A |
6575719 | Manner | Jun 2003 | B2 |
8978618 | Davis | Mar 2015 | B2 |
Number | Date | Country | |
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20220282622 A1 | Sep 2022 | US |