KR970021676A

KR970021676A - Multistage Continuous Explosion Fan Rotor Engine

Info

Publication number: KR970021676A
Application number: KR1019950039275A
Authority: KR
Inventors: 김병시
Original assignee: 김병시
Priority date: 1995-10-30
Filing date: 1995-10-30
Publication date: 1997-05-28

Abstract

본 발명은 다단 연속 폭발식 팬로터(FAN ROTOR) 엔진에 관한 것으로, 더욱 구체적으로는 엔진실을 타원형으로 구성하여 그 내부에 원통체의 회전자를 축설하고 회전자의 외주벽에 소정간격으로 탄성 돌출되게한 회전날개의 선단부를 엔진실 주벽에 밀착시켜 엔진실을 여러등분으로 분할된 격실로 구성되게한 다음 회전자를 1회전시키는 동안 타원형의 엔진실에서 기화된 연료의 흡입, 압축, 팽창, 배기를 연속적으로 행하여 동력을 발생시킬 수 있게 한 것이다.The present invention relates to a multi-stage continuous explosive fan rotor (FAN ROTOR) engine, more specifically, the engine compartment is composed of an elliptical to build a rotor of the cylindrical body therein and elastically at a predetermined interval on the outer peripheral wall of the rotor The tip of the protruding rotary blade is brought into close contact with the main wall of the engine compartment so that the engine compartment is composed of compartments divided into equal parts. Then, the suction, compression, expansion, It is possible to generate power by exhausting continuously.

즉, 엔진실(10)을 타원형으로 구성하여 그 내부에 원통체의 회전자(20)를 중심회전축(21)에 축설하고 회전자(20)의 외주벽에 소정간격으로 탄성돌출 되게한 다수의 회전날개(23) 선단부(23a)를 엔진실 내벽(10a)에 밀착시켜 엔진실(10)을 여러 등분으로 분실시킨 격실(14) 구성으로 회전자(20)를 1회전하는 동안 타원형 엔진실(10)내에서 기화된 연료의 흡입, 압축, 팽창, 배기를 연속적으로 행하여 동력을 발생시키는 다단 연속 폭발식 팬로터 엔진이다.That is, the engine chamber 10 is formed in an elliptical shape in which the rotor 20 of the cylindrical body is arranged on the central rotation shaft 21 and elastically protruded at predetermined intervals on the outer circumferential wall of the rotor 20. An elliptical engine compartment during one rotation of the rotor 20 in a compartment 14 configuration in which the tip 23a of the rotary blade 23 is in close contact with the inner wall 10a of the engine compartment and the engine compartment 10 is lost in several equal parts. 10) A multi-stage continuous explosion fan rotor engine that generates power by continuously inhaling, compressing, expanding, and evacuating vaporized fuel.

Description

Multistage Continuous Explosion Fan Rotor Engine

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.

제1도는 본 발명의 엔진장치의 작용단면 예시도,1 is an exemplary cross-sectional view of the operation of the engine device of the present invention,

제2도는 본 발명의 회전자의 일부분해 사시도,2 is a partial perspective view of the rotor of the present invention,

제3도는 본 발명에 의한 회전날개 접촉부의 확대 단면도.3 is an enlarged cross-sectional view of the rotor blade contact portion according to the present invention.

Claims

A plurality of rotor blades in which the engine chamber 10 is formed in an elliptical shape, the rotor 20 of the cylindrical body is laid on the central rotation shaft 21, and elastically protruded at predetermined intervals on the outer circumferential wall of the rotor 20. (23) The elliptical engine compartment 10 while the rotor 20 is rotated once in a compartment 14 configuration in which the tip portion 23a is in close contact with the engine compartment inner wall 10a and the engine compartment 10 is divided into equal parts. A multi-stage continuous explosive fan rotor engine that generates power by continuously inhaling, compressing, expanding, and exhausting vaporized fuel in the engine.

※ Note: The disclosure is based on the initial application.