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JPS5589617A - Petroleum combustor - Google Patents

Petroleum combustor

Info

Publication number
JPS5589617A
JPS5589617A JP16185678A JP16185678A JPS5589617A JP S5589617 A JPS5589617 A JP S5589617A JP 16185678 A JP16185678 A JP 16185678A JP 16185678 A JP16185678 A JP 16185678A JP S5589617 A JPS5589617 A JP S5589617A
Authority
JP
Japan
Prior art keywords
pump
turbine
flow
air
fuel
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
JP16185678A
Other languages
Japanese (ja)
Inventor
Hiroshi Nagasaka
Yutaka Suzuki
Sotohiko Watabe
Mitsuaki Sakamoto
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.)
Keihin Corp
Original Assignee
Keihin Seiki Manufacturing Co Ltd
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 Keihin Seiki Manufacturing Co Ltd filed Critical Keihin Seiki Manufacturing Co Ltd
Priority to JP16185678A priority Critical patent/JPS5589617A/en
Publication of JPS5589617A publication Critical patent/JPS5589617A/en
Pending legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE: To eliminate need for a special power source for driving a pump and enhance economy by a method wherein a metering fuel pump is composed of a device for constantly forming a predetermined liquid surface level in a fuel tank and an axial-flow pump in which a turbine is rotated by compressed air flow.
CONSTITUTION: With a motor 4 driven for operating a petroleum combustor, a suction fan 5 and an exhaust fan 8 rotate synchronously. Air compressed by the fan 5, on one hand, feeds conbustion air into a combustor 3 through a passage 7 and, on the other hand, is introduced into the air turbine chamber 25 of an axial- flow pump 12 through a passage 30, before jetted from air holes 28 to pressure receiving plates 26 for rotating a turbine 27. A turbine 20 integrally coupled with the turbine 27 by a spindle 22 rotates; the fuel in a fuel tank 16 develops a rotational flow in a pump casing 19 and converted into an axcial flow by a stator 21, then the fuel is fed from a pump chamber 31 to the combustor 3 through a passage 32.
COPYRIGHT: (C)1980,JPO&Japio
JP16185678A 1978-12-26 1978-12-26 Petroleum combustor Pending JPS5589617A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16185678A JPS5589617A (en) 1978-12-26 1978-12-26 Petroleum combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16185678A JPS5589617A (en) 1978-12-26 1978-12-26 Petroleum combustor

Publications (1)

Publication Number Publication Date
JPS5589617A true JPS5589617A (en) 1980-07-07

Family

ID=15743244

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16185678A Pending JPS5589617A (en) 1978-12-26 1978-12-26 Petroleum combustor

Country Status (1)

Country Link
JP (1) JPS5589617A (en)

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