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Title:
COMBUSTION CHAMBER ROTARY TYPE GAS TURBINE ENGINE
Document Type and Number:
Japanese Patent JPS60164626
Kind Code:
A
Abstract:

PURPOSE: To make an output variation ever so easy, by regulating the number of combustion times and a speed of rotation in a compression fan and an output turbine by means of rotation in a combustion chamber rotor.

CONSTITUTION: A turbine shaft 9 is connected to a combustion chamber rotor 2 by a turbine shaft gear 10, while compressed gas out of a compression fan 1 is inhaled in a combustion chamber 6 of the combustion chamber rotor 2 from a suction port 7 and, after being ignited by a spark plug, led into an output turbine 3 from an exhaust port 8. A difference between output by the output turbine 3 and such force as being necessary to rotate the combustion fan 1 and the combustion chamber rotor 2 is taken out of a driving shaft 5. Thus, since the number of combustion times and a speed of rotation in the combustion fan and the output turbine are regulated by rotation in the combustion chamber rotor, an output variation is attainable in an easy manner.


Inventors:
TAKAMOTO TATEO
Application Number:
JP2003884A
Publication Date:
August 27, 1985
Filing Date:
February 08, 1984
Export Citation:
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Assignee:
TAKAMOTO TATEO
International Classes:
F02C3/073; F02C3/14; F02C5/04; F02C7/00; (IPC1-7): F02C3/073; F02C3/14; F02C7/00



 
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