CN104633445A - Free gyroscope structure for allowing fluid to pass - Google Patents
Free gyroscope structure for allowing fluid to pass Download PDFInfo
- Publication number
- CN104633445A CN104633445A CN201510008113.0A CN201510008113A CN104633445A CN 104633445 A CN104633445 A CN 104633445A CN 201510008113 A CN201510008113 A CN 201510008113A CN 104633445 A CN104633445 A CN 104633445A
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- China
- Prior art keywords
- support channel
- inner ring
- outer shroud
- passage
- fluid
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- 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.)
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- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Gyroscopes (AREA)
Abstract
The invention relates to a novel flowing mechanism form, in particular to a free gyroscope structure for allowing fluid to pass. All parts of a free gyroscope are communicated, a communicated flowing mechanism is formed, and the structure can be used for rotary work tests of a structure with a spinning novel manned craft on the outer portion and the inner portion needing to be stable and a flowing structure needing to convey fluid outside. The free gyroscope communicating mechanism can guarantee that the inner structure and the outer structure are in the independent rotary state, and meanwhile the communication performance of all the parts is guaranteed.
Description
Technical field
The invention belongs to field of fluid machinery, relate to a kind of for the device of mechanism to be supplied accommodating fluid rotated.
Background technique
Gyroscopic effect adds flight stability, and Magnus effect may be used for promoting flight performance, and these use more at empty sky weapon, but people, other biological or some equipment can not adapt to this High Rotation Speed, but need extraneous delivering fluids simultaneously.In addition in order to examine the working state of some fluid machineries under various rotation status, and under whole fluid operating test stand is placed in rotation status, difficulty is very large.
Summary of the invention
The present invention is the fluid flow mechanism of free gyro form.This mechanism of free gyro UNICOM can ensure that external and internal compositions is in independently rotation status, ensures the connectedness of each several part simultaneously.People in such as high speed self-rotating flight vehicle etc. need externally to carry out fluid communication for a long time, ensure that inside has more stable direction Directivity simultaneously; In addition, aircraft fluid flow apparatus is rotated freely for entirety this gyro mechanism can be used to carry out ground handling test, except this gyroscope, follow running without the need to other supplementary equipment, thus decrease the carrying of its ground-testing plant and saved test space.
For the free gyro structure that fluid passes through, comprise inner ring and outer shroud, the Support Channel one of two inside and outside nested encryptions, Support Channel two, passage one, passage two, Support Channel three and Support Channel four; Inner ring is connected with Support Channel three by Support Channel two with outer shroud, be equipped with Support Channel one and Support Channel four outward, Support Channel one and Support Channel four ensure that outer shroud can rotate at the axle at Support Channel one and Support Channel four place, and Support Channel two and Support Channel three ensure that inner ring can rotate at the inner axle around Support Channel and Support Channel three place of outer shroud; Inner ring rotate envelope and outer shroud non-intersect, inner ring is provided with passage one and passage two, for connecting mechanism to be supplied; Inner ring and outer shroud offer the pipeline passed through for fluid, after ensureing that fluid enters from the Support Channel one of outer shroud, is entered the pipeline of inner ring by Support Channel two, flow out from the passage one of inner ring, enter mechanism to be supplied.
Fluid flows out into Support Channel two from described mechanism to be supplied, is entered the pipeline of inner ring by Support Channel two, flows out, enters the pipeline of outer shroud, flowed out subsequently by Support Channel four from the passage two of inner ring.
There is barbed portion in inner ring and outer shroud, lays electrode or magnet steel in gap portions, and this gyro can be made under the effect of electromagnetic force to carry out rotary work.
Accompanying drawing explanation
Fig. 1 is the structural drawing of device;
Fig. 2 is the sectional view of Support Channel;
Fig. 3 is Support Channel side view;
Fig. 4 is ring generalized section;
Fig. 5 is in the second embodiment, has the ring generalized section of local breach;
Fig. 6 is in the second embodiment, has the free gyro structural scheme of mechanism of local landolsring.
1 is Support Channel one, 2 be Support Channel two, 3 for passage one, 4 be inner ring, 5 be outer shroud, 6 for passage two, 7 be Support Channel three, 8 is Support Channel four, and 9 is Support Channel import, and 10 is Support Channel outlet, 11 is ring import A, 12 is ring internal channel A, and 13 is ring outlet A, and 14 is ring outlet B, 15 is ring internal channel B, and 16 is ring outlet B
Embodiment
As Fig. 1-4, delivering fluids enters from the Support Channel import 9 of Support Channel 1, then flowed out by the duct of its Support Channel outlet 10 and enter outer shroud 5, then by outer shroud 5 upper bracket passage 1, ring import A11 between Support Channel 22, ring internal channel A12, the Support Channel import 9 of ring outlet A13 structure and Support Channel 22, Support Channel outlet 10 enters inner ring 4, again by the import A11 in inner ring 4, ring internal channel A12, ring outlet A13 structure inlet passage 1, passage 1 and passage 26 UNICOM support the equipment needing supply and exhaust fluid, fluid is crossed and is entered 26, by passage 26, ring outlet B14 between Support Channel 37, ring internal channel B15 and ring outlet B16 structure flow into outer shroud 5, then by the ring outlet B14 between outer shroud 5, the structure of ring internal channel B15 and ring outlet B16, discharged by Support Channel 48.
In addition, also can there is barbed portion, as seen in figs. 5-6, lay electrode in gap portions, or magnet steel, this gyro can be made under the effect of electromagnetic force to carry out rotary work.
Claims (3)
1. the free gyro structure passed through for fluid, it is characterized in that: the inner ring (4) and outer shroud (5), the Support Channel one (1) that comprise two inside and outside nested encryptions, Support Channel two (2), passage one (3), passage two (6), Support Channel three (7) and Support Channel four (8); Inner ring (4) is connected with Support Channel three (7) by Support Channel two (2) with outer shroud (5), outer shroud (5) is provided with Support Channel one (1) and Support Channel four (8), Support Channel one (1) and Support Channel four (8) ensure that outer shroud can rotate at the axle at Support Channel one (1) and Support Channel four (8) place, and Support Channel two (2) and Support Channel three (7) ensure that inner ring (4) can rotate at the inner axle around Support Channel (2) and Support Channel three (7) place of outer shroud (5); Inner ring (4) rotate envelope and outer shroud (5) non-intersect, inner ring (4) is provided with passage one (3) and passage two (6), for connecting mechanism to be supplied; Inner ring (4) and outer shroud (5) offer the pipeline passed through for fluid, after ensureing that fluid enters from the Support Channel one (1) of outer shroud (5), the pipeline of inner ring (4) is entered by Support Channel two (2), flow out from the passage one (3) of inner ring, enter mechanism to be supplied.
2. the free gyro structure passed through for fluid according to claim 1, it is characterized in that: fluid flows out into Support Channel two (2) from described mechanism to be supplied, the pipeline of inner ring (4) is entered by Support Channel two (2), flow out from the passage two (3) of inner ring (4), enter the pipeline of outer shroud (5), flowed out by Support Channel four (8) subsequently.
3. the free gyro structure passed through for fluid according to claim 1, it is characterized in that: inner ring (4) and outer shroud (5) exist barbed portion, lay electrode or magnet steel in gap portions, this gyro can be made under the effect of electromagnetic force to carry out rotary work.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510008113.0A CN104633445B (en) | 2015-01-07 | 2015-01-07 | Free gyroscope structure for allowing fluid to pass |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510008113.0A CN104633445B (en) | 2015-01-07 | 2015-01-07 | Free gyroscope structure for allowing fluid to pass |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104633445A true CN104633445A (en) | 2015-05-20 |
| CN104633445B CN104633445B (en) | 2017-05-03 |
Family
ID=53212508
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510008113.0A Active CN104633445B (en) | 2015-01-07 | 2015-01-07 | Free gyroscope structure for allowing fluid to pass |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104633445B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1114279A (en) * | 1995-04-04 | 1996-01-03 | 符策政 | Flying saucer |
| EP1863706A2 (en) * | 2005-03-23 | 2007-12-12 | GFS Projects Limited | A craft having a rotatable fluid propulsion device |
| EP1863705A2 (en) * | 2005-03-23 | 2007-12-12 | GFS Projects Limited | Aerofoil surface for controlling spin |
| KR20120038713A (en) * | 2010-10-14 | 2012-04-24 | 한국표준과학연구원 | A gyroscopic aircraft with vertical takeoff and landing |
| CN104139858A (en) * | 2014-07-03 | 2014-11-12 | 余彩仙 | Disc type aircraft |
-
2015
- 2015-01-07 CN CN201510008113.0A patent/CN104633445B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1114279A (en) * | 1995-04-04 | 1996-01-03 | 符策政 | Flying saucer |
| EP1863706A2 (en) * | 2005-03-23 | 2007-12-12 | GFS Projects Limited | A craft having a rotatable fluid propulsion device |
| EP1863705A2 (en) * | 2005-03-23 | 2007-12-12 | GFS Projects Limited | Aerofoil surface for controlling spin |
| KR20120038713A (en) * | 2010-10-14 | 2012-04-24 | 한국표준과학연구원 | A gyroscopic aircraft with vertical takeoff and landing |
| CN104139858A (en) * | 2014-07-03 | 2014-11-12 | 余彩仙 | Disc type aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104633445B (en) | 2017-05-03 |
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