US2016201464A1PendingUtilityA1

Intake/outlet pipe optimization method for rotary engine

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Assignee: NAT INST CHUNG SHAN SCIENCE & TECHNOLOGYPriority: Mar 14, 2014Filed: Mar 22, 2016Published: Jul 14, 2016
Est. expiryMar 14, 2034(~7.7 yrs left)· nominal 20-yr term from priority
F01C 1/22F01C 21/186F01C 20/28F02B 53/04Y02T10/12F02B 55/02F01C 21/18F04C 15/06F02B 55/08
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Claims

Abstract

An intake/outlet pipe optimization method includes the steps of providing a rotary engine, measuring the pressure in an operation of the engine, designing the appearance of the intake/outlet pipes, adjusting the pressure wave in an air pipe and the pressure in an air chamber of the engine to increase the air intake and improve the output horsepower of the engine. The intake pipe is a tapered pipe having the pipe diameter on an intake side greater than the pipe diameter on the engine side; and the outlet pipe is an inversely tapered pipe having the pipe diameter on the engine side smaller than the pipe diameter on the outlet side.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . An intake/outlet pipe optimization method for a rotary engine, comprising the steps of:
 (A) providing a rotary engine body;   (B) running the rotary engine, and measuring the pressure of an air pipe and the pressure of an air chamber of the engine;   (C) controlling a pipe shape of the intake pipe by pipe length, such that the pipe diameter on an intake side is greater than the pipe diameter on an engine side, and controlling the pipe shape of an outlet pipe by a pipe length, such that the pipe diameter on the engine side is smaller than the pipe diameter on an outlet side; and   (D) performing a series of power output performance tests of the engine according to different combinations of the pipe length, pipe diameter, pipe shape and pipe angle, and determining an optimal combination of the pipe length, pipe diameter and pipe shape by an engine performance test result.   
     
     
         2 . The method of  claim 1 , wherein the pipe shape of the intake pipe is a tapered pipe shape, and the airflow direction is from the intake side with a relatively larger cross-sectional area to the engine side with a relatively smaller cross-sectional area. 
     
     
         3 . The method of  claim 1 , wherein the pipe shape of the outlet pipe is a tapered pipe shape, and the airflow direction is from the engine side with a relatively larger cross-sectional area to the outlet side with a relatively smaller cross-sectional area. 
     
     
         4 . The method of  claim 1 , wherein the pipe shape of the intake pipe and the pipe shape of the outlet pipe control the taper angle of the air pipe, and the angle is an included angle between an open end of the air pipe and the engine side. 
     
     
         5 . The method of  claim 4 , wherein the pipe angle control range is from 0 degree to 50 degrees, and the angles have values with an interval from one another. 
     
     
         6 . The method of  claim 1 , wherein the pipe length control range is from 100 mm to 1500 mm, and the pipe lengths have values with an interval from one another. 
     
     
         7 . The method of  claim 1 , wherein different combinations of the pipe length, pipe diameter, and pipe shape described in the step (D) together with the pressure of the air chamber of the rotary engine are provided for adjusting the amplitude and frequency of the pressure wave in the intake pipe, so that when the engine is situated at an air intake status, the pressure of the intake pipe is greater than the pressure of the air chamber.

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