JPS5644425A - Constant-volume heated working gas turbine - Google Patents

Constant-volume heated working gas turbine

Info

Publication number
JPS5644425A
JPS5644425A JP12027079A JP12027079A JPS5644425A JP S5644425 A JPS5644425 A JP S5644425A JP 12027079 A JP12027079 A JP 12027079A JP 12027079 A JP12027079 A JP 12027079A JP S5644425 A JPS5644425 A JP S5644425A
Authority
JP
Japan
Prior art keywords
gas
constant
combustion
volume
mixture
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP12027079A
Other languages
Japanese (ja)
Inventor
Yoshito Oba
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP12027079A priority Critical patent/JPS5644425A/en
Publication of JPS5644425A publication Critical patent/JPS5644425A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE: To increase the flowing quantity of gas based on constant-volume combustion, generate a large amount of constant-volume heated working gas and heighten output, by combining a turbine running gas generator with a rotation chamber combustion mechanism for continuously performing constant-volume heating combustion.
CONSTITUTION: Gas introduced through a gas intake port is compressed by a compressor 2. Fuel is injected from a fuel injection valve 3 into the compressed gas while it flows through a compression passage 4. The gas and the fuel are thus mixed with each other. The mixture is introduced into the rotation chamber 11 of a feed rotor 9 which rotates in a casing 7. The introduced mixture is moved as the rotor 9 rotates. When the mixture is burned and exploded under the pressure of high- temperature gas from a combustion assisting chamber 12, heated and expanded high-pressure gas gushes to heighten the pressure of the combustion assisting chamber 12. At that time, high-speed gas ejection is caused from a working gas ejection passage 14 to drive a turbine 15. Some gas remaining in the rotation chamber 11 is discharged into the atmosphere through an exhaust port 6.
COPYRIGHT: (C)1981,JPO&Japio
JP12027079A 1979-09-19 1979-09-19 Constant-volume heated working gas turbine Pending JPS5644425A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12027079A JPS5644425A (en) 1979-09-19 1979-09-19 Constant-volume heated working gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12027079A JPS5644425A (en) 1979-09-19 1979-09-19 Constant-volume heated working gas turbine

Publications (1)

Publication Number Publication Date
JPS5644425A true JPS5644425A (en) 1981-04-23

Family

ID=14782058

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12027079A Pending JPS5644425A (en) 1979-09-19 1979-09-19 Constant-volume heated working gas turbine

Country Status (1)

Country Link
JP (1) JPS5644425A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2859206A1 (en) * 2012-06-07 2015-04-15 Michel Aguilar Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2859206A1 (en) * 2012-06-07 2015-04-15 Michel Aguilar Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle
JP2015522741A (en) * 2012-06-07 2015-08-06 アギラール, ミシェルAGUILAR, Michel Method and thermal reactor for single valve propulsion with multiple injections and combustion per revolution cycle

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