CN203242217U - Barrel-type gravitational field interference unit - Google Patents
Barrel-type gravitational field interference unit Download PDFInfo
- Publication number
- CN203242217U CN203242217U CN 201320275392 CN201320275392U CN203242217U CN 203242217 U CN203242217 U CN 203242217U CN 201320275392 CN201320275392 CN 201320275392 CN 201320275392 U CN201320275392 U CN 201320275392U CN 203242217 U CN203242217 U CN 203242217U
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- CN
- China
- Prior art keywords
- drum
- magnetic patch
- strip
- barrel
- yoke
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a barrel-type gravitational field interference unit, which comprises a plurality of long-strip-shaped magnets which are closely adhered and arranged to form a barrel, the cross sections of the magnets can be circular, fan-shaped or rectangular, each long-strip-shaped magnet is respectively provided with an inner magnetic yoke and an outer magnetic yoke on the inner side and outer side of the barrel, the inner magnetic yoke and the outer magnetic yoke of each long-strip-shaped magnet are connected at two ends of each long-strip-shaped magnet, and are respectively provided with a magnetic yoke end head half shaft at the two ends; and the magnetic yoke end head half shafts are clamped in supporting plate inner arc grooves on the inner sides of supporting plates at two ends of the barrel which is formed by the long-strip-shaped magnets. The barrel-type gravitational field interference unit is characterized in that the inner side of the supporting plates at two ends of the barrel are symmetrically provided with a plurality of motors at positions close to the long-strip-shaped magnets, one end, which is far away from the supporting plates at two ends of the barrel, of a motor central shaft of each motor is provided with a gear, and the barrel is driven to rotate around a central axis of the barrel through the rotation of the gears.
Description
Technical field
The present invention relates to cylindrical gravity field interference unit, belong to gravity and disturb sciemtifec and technical sphere.
Background technology
Gravity is ubiquitous at the earth's surface;on the face of the globe, people study antigravity for many years, but failed breakthrough achievement always, the weightlessness of human simulation space is by applying one to object perpendicular to earth surface and towards the acceleration of earth surface, to reduce or to offset acceleration of gravity, thereby realize reducing the effect of gravity field, human also not in the phenomenon of laboratory observation to the interference gravity field.
Summary of the invention
The purpose of this invention is to provide a kind of cylindrical gravity field interference unit that can affect by the high-strength magnetic line of force of High Rotation Speed cutting gravity field.
Cylindrical gravity field interference unit, comprise that the polylith cross section is that circular fan-shaped or rectangular strip magnetic patch is close to drum of discharging composition mutually, every the strip magnetic patch is equipped with respectively an inner yoke and an outer yoke in drum inboard and the outside, yoke is good magnetic conductor, such as iron block etc., the inner yoke of every strip magnetic patch links to each other with the two ends of outer yoke at the strip magnetic patch, and at two ends a yoke termination semiaxis is arranged respectively; Yoke termination semiaxis is stuck in the support plate lnner arced slot of drum two supports plate inboard at the drum two ends that the strip magnetic patch forms, and makes yoke termination semiaxis do at a high speed circular the rotation along the support plate lnner arced slot in the support plate lnner arced slot; The drum two supports plate at two ends is installed on the drum base that is positioned at ground; It is characterized in that:
1, the inboard of drum two supports plate is symmetrically installed with a plurality of motors near the strip magnetic patch, the motor center axle of each motor is equipped with a gear away from drum two supports plate one end, yoke inner tines on the inner yoke of the gear teeth of gear and strip magnetic patch inboard is complementary, and when the motor high-speed rotation, the drum that can drive strip magnetic patch composition is done high-speed rotation, the rotation of drum is that the yoke termination semiaxis with the drum two ends is stuck in the support plate lnner arced slot of drum two supports plate and does high-speed rotation, and drum is done high-speed rotation around the central shaft of drum.
2, the magnetic direction of strip magnetic patch is that an end is the N utmost point, and the other end is the S utmost point, and all strip magnetic patch all are to arrange shoulder to shoulder in the in the same way magnetic field of the other end at same end, the S utmost point by the N utmost point, and drum one end of composition is that the N utmost point, the other end are the S utmost point; Inner yoke and the outer yoke that install in the interior outside of strip magnetic patch, its effect are that the back-shaped magnetic field magnetic line of guiding strip magnetic patch returns via yoke, and not via space in the drum or the drum external space.
When the rotational speed V that 3, reaches the drum that 10000 Gausses and strip magnetic patch form as the magnetic field intensity T of strip magnetic patch reached 6000 revolutions per seconds, the gravity field strength of center had significantly and reduces in its drum of drum that the strip magnetic patch forms; And the product TV value of the magnetic field intensity T of the speed V of the drum rotation of strip magnetic patch composition and strip magnetic patch is larger, and the gravity field strength of center reduces larger in its drum.
The present invention compared with prior art has the following advantages:
1, do not have to find to have similar approach to realize affecting the patent documentation report of gravity field effect.
Description of drawings
Fig. 1 is the diagrammatic cross-section of the embodiment of the invention;
Fig. 2 is middle A-A diagrammatic cross-section embodiment illustrated in fig. 1;
Fig. 3 is middle P enlarged diagram embodiment illustrated in fig. 1.
Among Fig. 1-3: 1, space 8, ground 9, drum base 10, the interior center 11 of drum, drum two supports plate 12, support plate lnner arced slot 13, yoke termination semiaxis 14, motor strap 15, the gear teeth 16, motor center axle 17, yoke inner tines in motor 2, gear 3, strip magnetic patch 4, outer yoke 5, inner yoke 6, gravity field and direction 7 thereof, the drum.
Embodiment
In the embodiment one shown in Fig. 1-3: cylindrical gravity field interference unit, comprise that the polylith cross section is that circular fan-shaped or rectangular strip magnetic patch 3 is close to drum of discharging composition mutually, every strip magnetic patch 3 is equipped with respectively an inner yoke 5 and an outer yoke 4 in drum inboard and the outside, the inner yoke 5 of every strip magnetic patch 3 links to each other with the two ends of outer yoke 4 at strip magnetic patch 3, and at two ends a yoke termination semiaxis 13 is arranged respectively; Yoke termination semiaxis 13 is stuck in the support plate lnner arced slot 12 of drum two supports plate 11 inboards at the drum two ends that strip magnetic patch 3 forms, and makes yoke termination semiaxis 13 do at a high speed circular the rotation along support plate lnner arced slot 12 support plate lnner arced slot 12 is interior; The drum two supports plate 11 at two ends is installed on the drum base 9 that is positioned at ground 8; It is characterized in that: the inboard of drum two supports plate 11 is symmetrically installed with a plurality of motors 1 near strip magnetic patch 3, the motor center axle 16 of each motor 1 is equipped with a gear 2 away from drum two supports plate 11 1 ends, yoke inner tines 17 on the gear teeth 15 of gear 2 and the inner yoke 5 of strip magnetic patch 3 inboards is complementary, and when motor 1 high-speed rotation, the drum that can drive strip magnetic patch 3 compositions is done high-speed rotation, the rotation of drum is that the yoke termination semiaxis 13 with the drum two ends is stuck in the support plate lnner arced slot 12 of drum two supports plate 11 and does high-speed rotation, and drum is done high-speed rotation around the central shaft of drum.
The magnetic direction of strip magnetic patch 3 is that an end is the N utmost point, and the other end is the S utmost point, and all strip magnetic patch 3 all are to arrange shoulder to shoulder in the in the same way magnetic field of the other end at same end, the S utmost point by the N utmost point, and drum one end of composition is that the N utmost point, the other end are the S utmost point; Inner yoke 5 and the outer yoke 4 that install in the interior outside of strip magnetic patch 3, its effect are that the back-shaped magnetic field magnetic line of guiding strip magnetic patch 3 returns via yoke, and not via space in the drum 7 or the drum external space.
When the rotational speed V that reaches the drum that 10000 Gausses and strip magnetic patch 3 form as the magnetic field intensity T of strip magnetic patch 3 reached 6000 revolutions per seconds, the gravity field strength of center had significantly and reduces in its drum of drum that strip magnetic patch 3 forms; And the product TV value of the magnetic field intensity T of the speed V of the drum rotation of strip magnetic patch 3 compositions and strip magnetic patch 3 is larger, and the gravity field strength of center 10 reduces larger in its drum.
Claims (2)
1. cylindrical gravity field interference unit, comprise that the polylith cross section is that circular fan-shaped or rectangular strip magnetic patch (3) is close to drum of discharging composition mutually, every strip magnetic patch (3) is equipped with respectively an inner yoke (5) and an outer yoke (4) in drum inboard and the outside, the inner yoke (5) of every strip magnetic patch (3) links to each other with the two ends of outer yoke (4) at strip magnetic patch (3), and at two ends a yoke termination semiaxis (13) is arranged respectively; Yoke termination semiaxis (13) is stuck in the inboard support plate lnner arced slot (12) of the drum two supports plate (11) at the drum two ends that strip magnetic patch (3) forms; The drum two supports plate (11) at two ends is installed on the drum base (9) that is positioned at ground (8); It is characterized in that: the inboard of drum two supports plate (11) is symmetrically installed with a plurality of motors (1) near strip magnetic patch (3), the motor center axle (16) of each motor (1) is equipped with a gear (2) away from drum two supports plate (11) one ends, and the yoke inner tines (17) on the inner yoke (5) of the gear teeth (15) of gear (2) and strip magnetic patch (3) inboard is complementary.
2. cylindrical gravity field interference unit as claimed in claim 1, it is characterized in that: the magnetic direction of strip magnetic patch (3) is that an end is the N utmost point, the other end is the S utmost point, and all strip magnetic patch (3) all are to arrange shoulder to shoulder in the in the same way magnetic field of the other end at same end, the S utmost point by the N utmost point, and drum one end of composition is that the N utmost point, the other end are the S utmost point; Inner yoke (5) and the outer yoke (4) that install in the interior outside of strip magnetic patch (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320275392 CN203242217U (en) | 2013-05-20 | 2013-05-20 | Barrel-type gravitational field interference unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320275392 CN203242217U (en) | 2013-05-20 | 2013-05-20 | Barrel-type gravitational field interference unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203242217U true CN203242217U (en) | 2013-10-16 |
Family
ID=49319489
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320275392 Expired - Fee Related CN203242217U (en) | 2013-05-20 | 2013-05-20 | Barrel-type gravitational field interference unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203242217U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103247205A (en) * | 2013-05-20 | 2013-08-14 | 魏伯卿 | Drum type gravitational field interfering device |
-
2013
- 2013-05-20 CN CN 201320275392 patent/CN203242217U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103247205A (en) * | 2013-05-20 | 2013-08-14 | 魏伯卿 | Drum type gravitational field interfering device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131016 Termination date: 20150520 |
|
| EXPY | Termination of patent right or utility model |