CN1064130A - Turbine-type heat engino - Google Patents
Turbine-type heat engino Download PDFInfo
- Publication number
- CN1064130A CN1064130A CN 91100846 CN91100846A CN1064130A CN 1064130 A CN1064130 A CN 1064130A CN 91100846 CN91100846 CN 91100846 CN 91100846 A CN91100846 A CN 91100846A CN 1064130 A CN1064130 A CN 1064130A
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- CN
- China
- Prior art keywords
- impeller
- explosion chamber
- explosion
- turbine
- engino
- 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
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Abstract
Turbine-type heat engino is a kind of hot machine of existing turbine formula that is different from, and it can be applicable to fields such as generating, boats and ships.
Turbine-type heat engino is by base, impeller housing, impeller, explosion chamber, gas injection apparatus, compositions such as ignition mechanism.
During turbine-type heat engino work, at first make gas injection apparatus that fuel is injected explosion chamber, ignition device makes the combustion explosion that injects explosion chamber impact impeller then, makes the rotation of impeller impeller axle, and impeller shaft is exactly the power output shaft of this hot machine.
Description
The present invention is a kind of turbine-type heat engino.
The hot machine of turbine formula is used for generating.Boats and ships, aircraft etc., but because the steam turbine in the hot machine of turbine formula is working medium with the high compressed steam.This just needs huge affiliated facilities such as boiler.Though the gas turbine volume is little, needs air compressor, recuperating device etc.Thereby the hot machine complex structure of existing turbine formula, bring very big difficulty for manufacturing and use.
The purpose of this invention is to provide a kind of simple in structurely, do not need the turbine-type heat engino of boiler, air compressor, recuperating device etc.
The object of the present invention is achieved like this: the gas injection apparatus of this turbine-type heat engino injects the inflammable gas of some in the fuel tank explosion chamber of this turbine-type heat engino, the ignition mechanism sparking makes in the explosion chamber and the combustible gas explosion of air mixing, the impact generated by explosion ripple is gone out by explosion chamber, pour impeller housing and impact impeller simultaneously, make the impeller shaft rotation, impeller shaft is the power shaft.
The present invention just is made up of impeller housing, impeller, explosion chamber, gas injection apparatus etc., so structure is simple especially.
Concrete structure of the present invention is provided by following embodiment and accompanying drawing thereof.
Fig. 1 is the structure diagram of the turbine-type heat engino of proposition according to the present invention.
Describe the details and the working condition of the turbine-type heat engino that proposes according to the present invention in detail below in conjunction with Fig. 1.
This turbine-type heat engino comprises: base (1), impeller housing (2), impeller shaft (3), impeller (4), air outlet (5), suction port (6), explosion chamber (8), gas injection apparatus (being made up of part 9,10,11,12,13,14,15,16).Ignition mechanism (forming) by part 7,17.
Gas injection apparatus comprises: piston (9), piston cylinder (10), valve (11), pipe (12), connecting rod (13), eccentric wheel (14), support (15), motor (16).
Ignition mechanism comprises: spark plug (7), contact (17)
During this turbine-type heat engino work: at first connect power supply (not drawing among the figure) motor (16) the drive eccentric wheel (14) of gas injection apparatus is rotated, the eccentric wheel of rotation (14) drives piston (9) by connecting rod (13) and moves up and down.Open the valve (11) of gas injection apparatus then, when piston (9) moves upward above the position of valve (11), inflammable gas in the fuel tank (not drawing among the figure) is by pipe (12), valve (11) enters piston cylinder (10), piston (9) move downward immediately with the inflammable gas in the piston cylinder (10) be pressed into explosion chamber (8) and with explosion chamber (8) in air mixing, the contact (17) that while eccentric wheel (14) touches on the support (15) is struck sparks the spark plug (7) in the explosion chamber (8), the combustible gas explosion of the air mixing of being lighted by spark plug (7) in the explosion chamber (8), the impact generated by explosion ripple is gone out by explosion chamber (8), pour impeller housing (2) and impact impeller (4) simultaneously, make its impeller axle (3) rotation, the gas that impact kinetic energy weakens is by air outlet (5) row mouth, suck fresh air by suction port (6) simultaneously, in in explosion chamber (8) and combustible gas explosion air mixing, the eccentric wheel (14) that rotates with motor (16) moves upward again by connecting rod (13) drive piston (9), inflammable gas in the fuel tank (not drawing among the figure) is again by pipe (12), valve (11) enters piston cylinder (10), piston (9) moves downward immediately, again inflammable gas is pressed into explosion chamber (8), eccentric wheel (14) touches the contact (17) on the support (15) again simultaneously, make spark plug (7) sparking in the explosion chamber (8), impact the interior impeller (4) of impeller housing (2) again with the combustible gas explosion of air mixing, impeller shaft (3) is rotated further, and this turbine-type heat engino just constantly rotates like this.Quit work and cut off the electricity supply (not drawing among the figure) or cut-off valve (11) gets final product.
Claims (2)
1, this turbine-type heat engino is to be it is characterized in that explosion chamber (8) is housed on impeller housing (2) by base (1), impeller housing (2), impeller shaft (3), impeller (4), air outlet (5), suction port (6), and gas injection apparatus (being made up of part 9,10,11,12,13,14,15,16) and ignition mechanism (being made up of part 7,17) are housed on explosion chamber (8).
2, turbine-type heat engino according to claim 1 is characterized in that: after power supply (not drawing among the figure) is connected, the motor of gas injection apparatus (16) drives eccentric wheel (14) and rotates, and the eccentric wheel of rotation (14) drives piston (9) by connecting rod (13) and moves up and down.Open the valve (11) of gas injection apparatus then, when piston (9) moves upward above the position of valve (11), inflammable gas in the fuel tank (not drawing among the figure) enters piston cylinder (10) by pipe (12) valve (11), piston (9) move downward immediately with the inflammable gas in the piston cylinder (10) be pressed into explosion chamber (8) and with explosion chamber (8) in air mixing, eccentric wheel (14) touches the contact (17) on the support (15) simultaneously, make spark plug (7) sparking in the explosion chamber (8), in the explosion chamber (8) by spark plug (7) that light with combustible gas explosion air mixing, the impact generated by explosion ripple is gone out by explosion chamber (8), pour impeller housing (2) and make its impeller axle (3) rotation towards impeller (4) simultaneously, the gas that impact kinetic energy weakens is discharged by air outlet (5), suck fresh air by suction port (6) simultaneously, in in explosion chamber (8) and combustible gas explosion air mixing, the eccentric wheel (14) that rotates with motor (16) moves upward again by connecting rod (13) drive piston (9), inflammable gas in the fuel tank (not drawing among the figure) enters piston cylinder (10) by pipe (12) valve (11) again, piston (9) moves downward immediately and again inflammable gas is pressed into explosion chamber (8), eccentric wheel (14) touches the contact (17) on the support (15) again simultaneously, make the combustible gas explosion of interior spark plug (7) sparking of explosion chamber (8) and air mixing impact the interior impeller (4) of impeller housing (2) again, impeller shaft (3) is rotated further, this turbine-type heat engino just constantly rotates like this, and quitting work cuts off the electricity supply (not drawing among the figure) or close valve (11) gets final product.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 91100846 CN1064130A (en) | 1991-02-08 | 1991-02-08 | Turbine-type heat engino |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 91100846 CN1064130A (en) | 1991-02-08 | 1991-02-08 | Turbine-type heat engino |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1064130A true CN1064130A (en) | 1992-09-02 |
Family
ID=4904865
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 91100846 Pending CN1064130A (en) | 1991-02-08 | 1991-02-08 | Turbine-type heat engino |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1064130A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1124404C (en) * | 1999-09-03 | 2003-10-15 | 张胜利 | Retroacting engine |
| CN102052153A (en) * | 2010-11-19 | 2011-05-11 | 北京工业大学 | Shock power machine adopting knocking combustion mode |
| CN106141650A (en) * | 2016-08-26 | 2016-11-23 | 重庆新钰立金属科技有限公司 | Screw mounting device |
-
1991
- 1991-02-08 CN CN 91100846 patent/CN1064130A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1124404C (en) * | 1999-09-03 | 2003-10-15 | 张胜利 | Retroacting engine |
| CN102052153A (en) * | 2010-11-19 | 2011-05-11 | 北京工业大学 | Shock power machine adopting knocking combustion mode |
| CN106141650A (en) * | 2016-08-26 | 2016-11-23 | 重庆新钰立金属科技有限公司 | Screw mounting device |
| CN106141650B (en) * | 2016-08-26 | 2018-02-13 | 重庆新钰立金属科技有限公司 | Screw mounting device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C06 | Publication | ||
| PB01 | Publication | ||
| C01 | Deemed withdrawal of patent application (patent law 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |