CN1173584A - Disk type pulse combustion turbine - Google Patents

Disk type pulse combustion turbine Download PDF

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Publication number
CN1173584A
CN1173584A CN 97112527 CN97112527A CN1173584A CN 1173584 A CN1173584 A CN 1173584A CN 97112527 CN97112527 CN 97112527 CN 97112527 A CN97112527 A CN 97112527A CN 1173584 A CN1173584 A CN 1173584A
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CN
China
Prior art keywords
combustion turbine
disk type
pulse combustion
type pulse
pulse
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.)
Granted
Application number
CN 97112527
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Chinese (zh)
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CN1079135C (en
Inventor
王大可
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
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to CN97112527A priority Critical patent/CN1079135C/en
Publication of CN1173584A publication Critical patent/CN1173584A/en
Application granted granted Critical
Publication of CN1079135C publication Critical patent/CN1079135C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

A pulse gas turbine is disclosed, which featrues that the pulse jet part is reformed into a coiled disk and overlapped with blade wheel for small size.

Description

Disk type pulse combustion turbine
Belong to the motor class
Pulse combustion turbine in the most approaching existing document, its pulse jet part is long straight, and it is bigger to take up space.
The present invention seeks to propose a kind of disk type pulse combustion turbine of smaller length
Technical solution of the present invention is partly to change long straight pulse jet into the coiling shape, and superimposed with the impeller plate.
Because long straight pulse jet part can be superimposed with impeller after coiling, so length is less.There is finished product to prove.
Advantage of the present invention is that volume is less, is convenient to less space and uses.
Figure of description is structure and relative position relation.
The specific embodiments of invention is: pulse jet is partly used coiling shape structure, and become superimposed position relation with the impeller plate.

Claims (1)

  1. The present invention with belong to pulse combustion turbine together near prior art.
    The invention is characterized in: pulse jet partly is the coiling shape, and superimposed with the impeller plate.
CN97112527A 1997-07-14 1997-07-14 Disk type pulse combustion turbine Expired - Fee Related CN1079135C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN97112527A CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN97112527A CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Publications (2)

Publication Number Publication Date
CN1173584A true CN1173584A (en) 1998-02-18
CN1079135C CN1079135C (en) 2002-02-13

Family

ID=5172324

Family Applications (1)

Application Number Title Priority Date Filing Date
CN97112527A Expired - Fee Related CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Country Status (1)

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CN (1) CN1079135C (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4708159A (en) * 1986-04-16 1987-11-24 Nea Technologies, Inc. Pulse combustion energy system
CN2119600U (en) * 1992-02-24 1992-10-21 南京热水器总厂 Air heater using gaseous fuel

Also Published As

Publication number Publication date
CN1079135C (en) 2002-02-13

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