CN203362232U - Radial-flow type airflow engine - Google Patents
Radial-flow type airflow engine Download PDFInfo
- Publication number
- CN203362232U CN203362232U CN 201320307128 CN201320307128U CN203362232U CN 203362232 U CN203362232 U CN 203362232U CN 201320307128 CN201320307128 CN 201320307128 CN 201320307128 U CN201320307128 U CN 201320307128U CN 203362232 U CN203362232 U CN 203362232U
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- radial
- cylindrical shell
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- flow type
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- 230000007246 mechanism Effects 0.000 claims description 9
- 241001633942 Dais Species 0.000 claims description 6
- 230000000295 complement effect Effects 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 239000012530 fluid Substances 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000007789 sealing Methods 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000002912 waste gas Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000035922 thirst Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 235000012431 wafers Nutrition 0.000 description 1
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Abstract
The utility model discloses a radial-flow type airflow engine. The radial-flow type airflow engine comprises a second stator cylinder body provided with an airflow inlet and an airflow outlet ; an inner wall arc of the second stator cylinder body comprises a reposition segmental arc and a volume segmental arc; a second rotor cylinder body with an output shaft is arranged inside the second stator cylinder body; a plurality of second grooves are formed in the second rotor cylinder body; bayonets are arranged in the second grooves, and are pivoted with third blades through third rotating shafts; an end opposite to a connection end of the third blades and the bayonets and the inner wall of the second stator cylinder body are in sliding fit with each other in a sealing manner. According to the radial-flow type airflow engine, fluid is discharged from the airflow outlet, and the second rotor cylinder body rotates under the driving of the third blades to output mechanical energy from the output shaft; the radial-flow type airflow engine is simple in structure, low in manufacturing cost and high in energy conversion efficiency.
Description
Technical field
The utility model relates to engine technology, relates in particular to a kind of radial-flow type air-flow motor.
Background technique
A large amount of fuel be need to consume with fuel as the motor of the energy, and a large amount of waste gas, hot gas, befouling environment discharged again.For the fuel saving energy, the environment of preserving our planet, the mankind more thirst for a kind of without fuel consumption, stop waste gas, hot air discharge, free of contamination motor.At present, the employing wind power transformation that oneself is known is all more complicated of the engine structure that is utilized of mechanical kinetic energy, and manufacture cost is high, and energy conversion efficiency is low.
The model utility content
Technical problem to be solved in the utility model is: a kind of radial-flow type air-flow motor is provided, and not only simple in structure, reduced manufacture cost, and energy conversion efficiency is high.
For solving the problems of the technologies described above, the utility model proposes a kind of radial-flow type air-flow motor, comprise the second stator cylindrical shell that is provided with air-flow entry port and air-flow exhaust port, the inwall circular arc of described the second stator cylindrical shell comprises reset segmental arc and volume segmental arc; Be provided with the second rotor cylindrical shell with output shaft in described the second stator cylindrical shell, described the second rotor cylindrical shell is provided with some the second grooves, be provided with bayonet socket in the second groove, be pivoted with the 3rd blade by the 3rd rotating shaft in bayonet socket, between the opposite end of the 3rd blade and bayonet socket connecting end and the second stator cylinder inboard wall, sealed sliding movingly.
Further, described the second rotor cylindrical shell is identical with the center of circle of the segmental arc that resets, and the diameter of the second rotor cylindrical shell is less than the diameter of the segmental arc that resets.
Further, described the 3rd leaf packet bracket plate and connecting plate, arc plate be the sickle shaped shape after connecting plate is connected; The opposite end of connecting plate and arc plate connecting end is articulated in bayonet socket by the 3rd rotating shaft; The external arc radian of arc plate is complementary with the radian of the segmental arc that resets, and the diameter of the external diameter of arc plate and the second rotor cylindrical shell is isometrical.
Further, described connecting plate is provided with limited part; Be provided with limit dais in described the second groove, after described the 3rd mounted blade, limiting section support is connected on limit dais.
Further, be provided with elastic mechanism between described the second groove and the 3rd blade.
Further, described elastic mechanism comprises the single-pass hole be arranged in the second groove, and single-pass is provided with spring spindle in hole.
Further, described elastic mechanism is the torsion spring be arranged in the 3rd rotating shaft.
Technique scheme at least has following beneficial effect: the utility model by being provided with some the second grooves on the second rotor cylindrical shell, be provided with bayonet socket in the second groove, be pivoted with the 3rd blade by the 3rd rotating shaft in bayonet socket, between the opposite end of the 3rd blade and bayonet socket connecting end and the second stator cylinder inboard wall, sealed sliding movingly, by fluid is discharged from the air-flow exhaust port, the second rotor cylindrical shell rotates under three-vaned drive, from the output shaft output mechanical energy, not only simple in structure, reduced manufacture cost, and energy conversion efficiency is high.
The accompanying drawing explanation
Fig. 1 is the transverse sectional view of the structural representation of the utility model radial-flow type air-flow motor.
Fig. 2 is the cross-sectional view of the structural representation of the second rotor cylindrical shell in the utility model radial-flow type air-flow motor.
Fig. 3 is the longitudinal sectional view of the structural representation of the utility model radial-flow type air-flow motor.
Embodiment
It should be noted that, in the situation that do not conflict, embodiment and the feature in embodiment in the application can combine mutually.Below in conjunction with accompanying drawing, the utility model is described further.
As shown in Figure 1 to Figure 3, radial-flow type air-flow motor of the present utility model comprises the second stator cylindrical shell 71, the second rotor cylindrical shell 72, the 3rd blade 73, the 3rd rotating shaft 74, output shaft 75.Wherein, the second stator cylindrical shell 71 is for being provided with the circular cylindrical cavity of air-flow entry port 711 and air-flow exhaust port 712, the inwall circular arc of the second stator cylindrical shell 71 comprises two sections concentric and waney segmental arc 713 and volume segmental arcs 714 of resetting, the volume segmental arc 714 that reset segmental arc 713 and the C point that to be respectively the A point order to B ordered to D, the second rotor cylindrical shell 72 is arranged in the second stator cylindrical shell 71, and the second rotor cylindrical shell 72 is identical with the center of circle of the segmental arc 713 that resets, and the diameter of the second rotor cylindrical shell 72 is slightly less than the diameter of the segmental arc 713 that resets, output shaft 75 is arranged on the second rotor cylindrical shell 72, for output mechanical energy, the second rotor cylindrical shell 72 is provided with in 3 the second groove 76, the second grooves 76 and is respectively equipped with bayonet socket 77, the 3rd blade 73 comprises arc plate 731 and connecting plate 732, arc plate 731 be the sickle shaped shape after connecting plate 732 is connected, connecting plate 732 is articulated in bayonet socket 77 by the 3rd rotating shaft 74 with the opposite end of arc plate 731 connecting ends, guarantee sickle shaped the 3rd blade 73 dehisce to meet to air-flow entry port 711, the external arc radian of arc plate 731 is complementary with the radian of the segmental arc 713 that resets, and the diameter of the external diameter of arc plate 731 and the second rotor cylindrical shell 72 is isometrical, close up while resetting when the 3rd blade 73 and the second rotor cylindrical shell 72 like this, the 3rd blade 73 full wafers embed in the second groove 76 of the second rotor cylindrical shell 72, now the external arc of the 3rd blade 73 coordinates with segmental arc 713 inscribes that reset, can reduce friction, prevent the 3rd blade 73 wearing and tearing, be provided with limited part 733 on connecting plate 732, be provided with limit dais 761 in described the second groove 76, after described the 3rd blade 73 launches, limited part 733 is connected on limit dais 761, like this can be when the 3rd blade 73 be opened, the 3rd blade 73 is played to position-limiting action, guarantee that the 3rd blade 73 and the second stator cylindrical shell 71 inner wall sealings are slidably matched and are unlikely to produce friction with inwall, elastic mechanism 78 is arranged between the second groove 76 and the 3rd blade 73, particularly, elastic mechanism 78 comprises the single-pass hole 781 be arranged in the second groove 76, be provided with spring spindle 782 in single-pass hole 781, when the 3rd blade 73 rotation is left the segmental arc 713 that resets and entered volume segmental arc 714,, when the end of the 3rd blade 73 forwards A point to, spring spindle 782 promotion the 3rd blades 73 are opened rapidly like this, so that the high velocity air flowed into from air-flow entry port 711 impacts the 3rd blade 73, raise the efficiency, as another kind of mode of execution, elastic mechanism 78 also can, for being arranged on the torsion spring in the 3rd rotating shaft 74, can be obtained above-mentioned effect equally.
The working procedure of radial-flow type air-flow motor is as follows:
There is the fluid of certain pressure to enter in the cavity of the second stator cylindrical shell 71 from air-flow entry port 711, promote the 3rd blade 73 and move; When the 3rd blade 73 moves to blade while resetting segmental arc 713, under the effect of the cambered surface 713 that resets, the 3rd blade 73 resets and embeds in the second groove 76, and fluid is discharged from air-flow exhaust port 712, the second rotor cylindrical shell 72 rotates under the drive of the 3rd blade 73, from output shaft 75 output mechanical energies.
The above is embodiment of the present utility model; it should be pointed out that for those skilled in the art, under the prerequisite that does not break away from the utility model principle; can also make some improvements and modifications, these improvements and modifications also are considered as protection domain of the present utility model.
Claims (7)
1. a radial-flow type air-flow motor, comprise the second stator cylindrical shell that is provided with air-flow entry port and air-flow exhaust port, and the inwall circular arc of described the second stator cylindrical shell comprises reset segmental arc and volume segmental arc; Be provided with the second rotor cylindrical shell with output shaft in described the second stator cylindrical shell, it is characterized in that, described the second rotor cylindrical shell is provided with some the second grooves, be provided with bayonet socket in the second groove, be pivoted with the 3rd blade by the 3rd rotating shaft in bayonet socket, between the opposite end of the 3rd blade and bayonet socket connecting end and the second stator cylinder inboard wall, sealed sliding movingly.
2. radial-flow type air-flow motor as claimed in claim 1, is characterized in that, described the second rotor cylindrical shell is identical with the center of circle of the segmental arc that resets, and the diameter of the second rotor cylindrical shell is less than the diameter of the segmental arc that resets.
3. radial-flow type air-flow motor as claimed in claim 1, is characterized in that, described the 3rd leaf packet bracket plate and connecting plate, arc plate be the sickle shaped shape after connecting plate is connected; The opposite end of connecting plate and arc plate connecting end is articulated in bayonet socket by the 3rd rotating shaft; The external arc radian of arc plate is complementary with the radian of the segmental arc that resets, and the diameter of the external diameter of arc plate and the second rotor cylindrical shell is isometrical.
4. radial-flow type air-flow motor as claimed in claim 3, is characterized in that, described connecting plate is provided with limited part; Be provided with limit dais in described the second groove, after described the 3rd mounted blade, limiting section support is connected on limit dais.
5. radial-flow type air-flow motor as claimed in claim 1, is characterized in that, between described the second groove and the 3rd blade, is provided with elastic mechanism.
6. radial-flow type air-flow motor as claimed in claim 5, is characterized in that, described elastic mechanism comprises the single-pass hole be arranged in the second groove, and single-pass is provided with spring spindle in hole.
7. radial-flow type air-flow motor as claimed in claim 5, is characterized in that, described elastic mechanism is the torsion spring be arranged in the 3rd rotating shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320307128 CN203362232U (en) | 2013-05-30 | 2013-05-30 | Radial-flow type airflow engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320307128 CN203362232U (en) | 2013-05-30 | 2013-05-30 | Radial-flow type airflow engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203362232U true CN203362232U (en) | 2013-12-25 |
Family
ID=49810018
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320307128 Expired - Fee Related CN203362232U (en) | 2013-05-30 | 2013-05-30 | Radial-flow type airflow engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203362232U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104454020A (en) * | 2014-12-16 | 2015-03-25 | 周觉明 | Fluid power machine with runner rotary vane whirling mechanism |
-
2013
- 2013-05-30 CN CN 201320307128 patent/CN203362232U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104454020A (en) * | 2014-12-16 | 2015-03-25 | 周觉明 | Fluid power machine with runner rotary vane whirling mechanism |
| CN104454020B (en) * | 2014-12-16 | 2019-10-18 | 南通金鼎天轮动力科技有限公司 | Fluid dynamic with runner vane cyclotron mechanism is mechanical |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: SHENZHEN JINWANFU ENERGY TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: DENG YUANMING Effective date: 20150731 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150731 Address after: The streets of Shenzhen city in Guangdong province 518000 Keyuan Road Nanshan District Guangdong No. 11 Financial Technology Building A block 10 building A Patentee after: Shenzhen Jin Wanfu Energy Technology Co., Ltd. Address before: 516300, No. 4, No. five, Lane 301, Village North Road, Pingshan golden residential committee, Pingshan County, Huizhou, Guangdong, Huidong Patentee before: Deng Yuanming |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131225 Termination date: 20160530 |