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Title:
TURBINE ENGINE
Document Type and Number:
Japanese Patent JPH04101025
Kind Code:
A
Abstract:

PURPOSE: To secure an engine which can be used conveniently as a small power supply for houshold use and can be manufactured and assembled simply at a low cost by manufacturing an axial flow gas turbine, and a generator of combustion gas used therefor separately, and connecting them together before using them.

CONSTITUTION: A turbine engine is composed of an axial flow gas turbine A, and a generator B for generating a gas used as actuation gas for this turbine. In the axial flow gas turbine A, a turbine shaft 4 provided with a vane 5 on the circular face is rotatably supported inside a casing 1 whose one end acts as an injection port 2 of combustion gas, and other end acts as a discharge port 3. Meanwhile, in the generator B for generating a gas used as actuation gas, a compression chamber 18 is formed by sealing the tip end part of a cylinder 17 provided with a piston 16 which reciprocates by a crank mechanism 15, and a rotationally moving valve 19 which has an air port 20 is provided by being incribed on the inside of the compression chamber 18. An intake port communicated to a fuel carburetor and an injection port communicated to the turbine A are formed in the compression chamber 18.


Inventors:
NAKATSU HIROMICHI
NAKATSU MASANOBU
Application Number:
JP21499190A
Publication Date:
April 02, 1992
Filing Date:
August 16, 1990
Export Citation:
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Assignee:
NAKATSU HIROMICHI
NAKATSU MASANOBU
International Classes:
F02B41/10; F02C5/06; F02C5/12; (IPC1-7): F02B41/10; F02C5/06; F02C5/12
Domestic Patent References:
JPS62243930A1987-10-24
JPS63268938A1988-11-07
Attorney, Agent or Firm:
Kinichi Kitamura (3 others)