CN106704033A - Method for constructing power system and device thereof - Google Patents
Method for constructing power system and device thereof Download PDFInfo
- Publication number
- CN106704033A CN106704033A CN201610986672.3A CN201610986672A CN106704033A CN 106704033 A CN106704033 A CN 106704033A CN 201610986672 A CN201610986672 A CN 201610986672A CN 106704033 A CN106704033 A CN 106704033A
- Authority
- CN
- China
- Prior art keywords
- turning
- punching press
- line shaft
- described pair
- force system
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/30—Wind power
Abstract
The invention discloses a method for constructing a power system; and a pneumatic turbine or an opposite rotating pneumatic turbine is used for driving an opposite rotating punching compressor. The method for constructing the power system can efficiently improve the propelling efficiency of the power system. The invention further discloses a device for applying the method for constructing the power system. The device has the advantages of simple structure and high thrust efficiency.
Description
Technical field
The present invention relates to heat energy and dynamic field, more particularly to construction force system method and its device.
Background technology
Air is entered using Atmospheric Flow (such as the air-flow flowed backward relative to aircraft that aircraft flight is produced)
Row produces propulsive force to have great importance after compressing or being compressed to air through combustion chamber.Accordingly, it would be desirable to invent a kind of new
Construction force system method and its device.
The content of the invention
In order to solve the above problems, technical scheme proposed by the present invention is as follows：
A kind of method of construction force system of the invention, is driven to turning punching press compressor with pneumatic turbine.
Further optionally, the compressed gas outlet for turning punching press compressor by described pair and combustion chamber.
A kind of method of construction force system of the invention, is driven to turning punching press compressor with to turning pneumatic turbine.
Further optionally, the compressed gas outlet for turning punching press compressor by described pair and combustion chamber.
Further optionally, the combustion chamber is connected with jet pipe.
Using the device of the method for foregoing construction force system, N number of line shaft coaxial line is set, and adjacent two are described dynamic
Turn transmission through gear mesh between power axle to set, the pneumatic turbine is arranged on the line shaft；Described pair turns punching press compressor
Impeller be arranged on the line shaft.
Using the device of the method for foregoing construction force system, N number of line shaft be set with centrally disposed line shaft and with
The center power axle is rotatably assorted setting, and turning transmission through gear mesh between two adjacent line shafts is set, the tooth
The rotating shaft of wheel is arranged on the center power axle, the described pair of a part of rotary blade for turning pneumatic turbine and the center power
Axle connect setting, the described pair of another part rotary blade for turning pneumatic turbine and the line shaft connect setting；Described pair turns punching
The impeller of compressor is pressed to be arranged on the line shaft.
Further optionally, the described pair of compressed gas outlet for turning punching press compressor and combustion chamber are made.
Further optionally, the combustion chamber is made to be connected with jet pipe.
In the present invention, " N " is nonzero integer, and is selectively chosen that to be set to 2,3,4,5,6,7,8,9,10 etc. non-
Zero integer.
In the present invention, necessary part, list should be set in necessary place according to heat energy and the known technology of dynamic field
Unit or system etc..
Beneficial effects of the present invention are as follows:The method of construction force system disclosed in this invention can efficiently be lifted dynamic
The propulsive efficiency of Force system；Device disclosed in this invention has the advantages that simple structure, thrust efficiency are high.
Brief description of the drawings
Fig. 1：The structural representation of the embodiment of the present invention 1；
Fig. 2：The structural representation of the embodiment of the present invention 2；
Fig. 3：The structural representation of the embodiment of the present invention 3；
Fig. 4：The structural representation of the embodiment of the present invention 4；
Fig. 5：The structural representation of the embodiment of the present invention 5；
Fig. 6：The structural representation of the embodiment of the present invention 6.
Specific embodiment
The invention also discloses a kind of method of construction force system, driven to turning with pneumatic turbine or to turning pneumatic turbine
Punching press compressor.And the compressed gas that further can turn punching press compressor by described pair are exported and combustion chamber；Can also more enter
One step connects the combustion chamber with jet pipe.
The method of above-mentioned construction force system is described further with specific embodiment below in conjunction with the accompanying drawings：
Embodiment 1
Using the device of the method for foregoing construction force system, as shown in figure 1, including pneumatic turbine 3 and to turning punching press pressure
Mechanism of qi 5, the coaxial line of N number of line shaft 1 is set, and is set through 2 pairs turns of transmissions of gear between two adjacent line shafts 1, described
Pneumatic turbine 3 is arranged on the line shaft 1；The described pair of impeller for turning punching press compressor 5 is arranged on the line shaft 1.
Embodiment 2
Using the device of the method for foregoing construction force system, as shown in Fig. 2 including pneumatic turbine 3 and to turning punching press pressure
Mechanism of qi 5, the coaxial line of N number of line shaft 1 is set, and is set through 2 pairs turns of transmissions of gear between two adjacent line shafts 1, described
Pneumatic turbine 3 is arranged on the line shaft 1；The described pair of impeller for turning punching press compressor 5 is arranged on the line shaft 1, institute
State the compressed gas outlet to turning punching press compressor 5 to be connected with combustion chamber 6, the combustion chamber 6 connects with jet pipe 7.
Embodiment 3
Using the device of the method for foregoing construction force system, as shown in figure 3, including pneumatic turbine 3 and to turning punching press pressure
Mechanism of qi 5, the coaxial line of N number of line shaft 1 is set, and is set through 2 pairs turns of transmissions of gear between two adjacent line shafts 1, described
Pneumatic turbine 3 is arranged on the line shaft 1；The described pair of impeller for turning punching press compressor 5 is arranged on the line shaft 1, institute
State the compressed gas outlet to turning punching press compressor 5 to be connected with combustion chamber 6, the combustion chamber 6 connects with jet pipe 7.
Used as disposable implementation method, the embodiment of the present invention 1 to embodiment 3 and its disposable implementation method can be entered
One step optionally selects to make the pneumatic turbine 3 be arranged on the line shaft 1 by gear, and can further select
Select to selecting property to make the gear be set to speed increasing mechanism.
Embodiment 4
Using the device of the method for foregoing construction force system, as shown in figure 4, including to turn pneumatic turbine 31 and to turn punching
Pressure compressor 5, N number of line shaft 1 is set with centrally disposed line shaft 11 and is rotatably assorted setting with the center power axle 11,
Turn transmission through gear 2 pairs between two adjacent line shafts 1 to set, the rotating shaft of the gear 2 be arranged on it is described in it is aroused in interest
On power axle 1, the described pair of a part of rotary blade for turning pneumatic turbine 31 and the connect setting of center power axle 1, described pair turns
Another part rotary blade of pneumatic turbine 31 and the connect setting of the line shaft 1；The described pair of impeller for turning punching press compressor 5 sets
Put on the line shaft 1.
Embodiment 5
Using the device of the method for foregoing construction force system, as shown in figure 5, including to turn pneumatic turbine 31 and to turn punching
Pressure compressor 5, N number of line shaft 1 is set with centrally disposed line shaft 11 and is rotatably assorted setting with the center power axle 11,
Turn transmission through gear 2 pairs between two adjacent line shafts 1 to set, the rotating shaft of the gear 2 be arranged on it is described in it is aroused in interest
On power axle 1, the described pair of a part of rotary blade for turning pneumatic turbine 31 and the connect setting of center power axle 1, described pair turns
Another part rotary blade of pneumatic turbine 31 and the connect setting of the line shaft 1；The described pair of impeller for turning punching press compressor 5 sets
Put on the line shaft 1, the described pair of compressed gas outlet for turning punching press compressor 5 is connected with combustion chamber 6.
Embodiment 6
Using the device of the method for foregoing construction force system, as shown in fig. 6, including to turn pneumatic turbine 31 and to turn punching
Pressure compressor 5, N number of line shaft 1 is set with centrally disposed line shaft 11 and is rotatably assorted setting with the center power axle 11,
Turn transmission through gear 2 pairs between two adjacent line shafts 1 to set, the rotating shaft of the gear 2 be arranged on it is described in it is aroused in interest
On power axle 1, the described pair of a part of rotary blade for turning pneumatic turbine 31 and the connect setting of center power axle 1, described pair turns
Another part rotary blade of pneumatic turbine 31 and the connect setting of the line shaft 1；The described pair of impeller for turning punching press compressor 5 sets
Put on the line shaft 1, the described pair of compressed gas outlet for turning punching press compressor 5 is connected with combustion chamber 6, the combustion chamber 6
Connected with jet pipe 7.
Used as disposable implementation method, the embodiment of the present invention 4 to embodiment 6 and its disposable implementation method can be entered
One step optionally selects to make described pair to turn pneumatic turbine 31 to be arranged on the line shaft 1 by gear, and can enter again
One step optionally selects to make the gear be set to speed increasing mechanism.
Used as disposable implementation method, N is optional described in embodiment 1 to embodiment 6 and its disposable implementation method
Select to selecting property to be set to certain of 2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21 or more than 21
Individual nonzero integer.
It is clear that the invention is not restricted to above example, according to techniques known and technology disclosed in this invention
Scheme, can derive or association goes out many flexible programs, all these flexible programs, and it is protection model of the invention also to be regarded as
Enclose.
Claims (10)
1. a kind of method of construction force system, it is characterised in that：Driven to turning punching press compressor with pneumatic turbine.
2. the method for construction force system as claimed in claim 1, it is characterised in that：The compression for turning punching press compressor by described pair
Gas vent and combustion chamber.
3. a kind of method of construction force system, it is characterised in that：Driven to turning punching press compressor with to turning pneumatic turbine.
4. the method for construction force system as claimed in claim 3, it is characterised in that：The compression for turning punching press compressor by described pair
Gas vent and combustion chamber.
5. as described in claim 2 or 4 construction force system method, it is characterised in that：The combustion chamber is connected with jet pipe.
6. the device of the method for construction force system as claimed in claim 1 or 2 is applied, it is characterised in that：N number of line shaft (1)
Coaxial line is set, and is set to turning transmission through gear (2) between two adjacent line shafts (1), and the pneumatic turbine (3) sets
Put on the line shaft (1)；The described pair of impeller for turning punching press compressor (5) is arranged on the line shaft (1).
7. using the device of the method for construction force system as described in claim 3 or 4, it is characterised in that：N number of line shaft (1)
It is set with centrally disposed line shaft (11) and is rotatably assorted setting with the center power axle (11), adjacent two is described dynamic
Set to turning transmission through gear (2) between power axle (1), the rotating shaft of the gear (2) is arranged on the center power axle (11),
The described pair of a part of rotary blade for turning pneumatic turbine (31) and center power axle (11) connect setting, described pair turns pneumatic
Another part rotary blade of turbine (31) and the line shaft (1) connect setting；The described pair of impeller for turning punching press compressor (5)
It is arranged on the line shaft (1).
8. device as claimed in claim 6, it is characterised in that：The described pair of compressed gas outlet and combustion for turning punching press compressor (5)
Burn room (6) connection.
9. device as claimed in claim 7, it is characterised in that：The described pair of compressed gas outlet and combustion for turning punching press compressor (5)
Burn room (6) connection.
10. such as the described device of claim 8 or 9, it is characterised in that：The combustion chamber (6) connects with jet pipe (7).
Applications Claiming Priority (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2015107815099 | 2015-11-14 | ||
| CN201510781410 | 2015-11-14 | ||
| CN201510780804 | 2015-11-14 | ||
| CN2015107814109 | 2015-11-14 | ||
| CN201510781509 | 2015-11-14 | ||
| CN2015107808042 | 2015-11-14 | ||
| CN201510781440 | 2015-11-15 | ||
| CN201510781440X | 2015-11-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106704033A true CN106704033A (en) | 2017-05-24 |
Family
ID=58940442
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610986672.3A Pending CN106704033A (en) | 2015-11-14 | 2016-11-09 | Method for constructing power system and device thereof |
| CN201610986676.1A Pending CN106704034A (en) | 2015-11-14 | 2016-11-09 | Method for constructing power system and device for method |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610986676.1A Pending CN106704034A (en) | 2015-11-14 | 2016-11-09 | Method for constructing power system and device for method |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN106704033A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1048439A (en) * | 1989-06-26 | 1991-01-09 | 川波春平 | To changeing the double rotor centrifugal fluid-charger |
| US5692372A (en) * | 1995-03-18 | 1997-12-02 | Rolls-Royce Plc | Aircraft compound cycle propulsion engine |
| CA2183378A1 (en) * | 1996-08-15 | 1998-02-16 | Michael J. Baxter | Turbine booster |
| CN102146858A (en) * | 2010-08-12 | 2011-08-10 | 靳北彪 | Stamping engine for pneumatic turbine |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2294445C2 (en) * | 2004-08-18 | 2007-02-27 | Открытое Акционерное Общество Центральная Компания Финансово-Промышленной Группы "Российский Авиационный Консорциум" | Double-flow jet engine |
-
2016
- 2016-11-09 CN CN201610986672.3A patent/CN106704033A/en active Pending
- 2016-11-09 CN CN201610986676.1A patent/CN106704034A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1048439A (en) * | 1989-06-26 | 1991-01-09 | 川波春平 | To changeing the double rotor centrifugal fluid-charger |
| US5692372A (en) * | 1995-03-18 | 1997-12-02 | Rolls-Royce Plc | Aircraft compound cycle propulsion engine |
| CA2183378A1 (en) * | 1996-08-15 | 1998-02-16 | Michael J. Baxter | Turbine booster |
| CN102146858A (en) * | 2010-08-12 | 2011-08-10 | 靳北彪 | Stamping engine for pneumatic turbine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106704034A (en) | 2017-05-24 |
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| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170524 |
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| WD01 | Invention patent application deemed withdrawn after publication |