CN106628198A - Centrifugal force driving device - Google Patents
Centrifugal force driving device Download PDFInfo
- Publication number
- CN106628198A CN106628198A CN201611059990.1A CN201611059990A CN106628198A CN 106628198 A CN106628198 A CN 106628198A CN 201611059990 A CN201611059990 A CN 201611059990A CN 106628198 A CN106628198 A CN 106628198A
- Authority
- CN
- China
- Prior art keywords
- spiral arm
- rotating shaft
- fixing structure
- slidably
- ring
- 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
- 238000007789 sealing Methods 0.000 claims description 10
- 238000005119 centrifugation Methods 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/409—Unconventional spacecraft propulsion systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention relates to a device for driving an object to move directionally through centrifugal force. The device comprises a sealed shell (1), a limiting ring (2), a rotating arm set (3), centrifugal columns (4), slidable rotating arms (5), a gear motor (6), a high-rotating-speed high-power motor (7), a rotating shaft (8) and a limiting ring fixing structure (9). When the centrifugal columns (4) move along the inner wall of the limiting ring (2), the frequencies of the centrifugal columns (4) moving on the semicircle and two quadrants of the inner wall of the limiting ring (2) are consistent, according to the formula that F=m[omega]2r=4m[pi]2f2r, the centrifugal force on the semicircle of the inner wall of the limiting ring is twice the centrifugal force on the quadrants when the centrifugal columns move around the rotating shaft and along the inner wall of the limiting ring, the ratio of the centrifugal force of the slidable rotating arms in corresponding positions is close to 2:1, the acting time of the force is the same, and thus the formed force difference can drive the object to move directionally.
Description
Technical field
The present invention relates to a kind of utilization centrifugal force drives object movement, flight, the device of hovering, especially can be in space ring
Object is expeditiously driven to move in border.
Background technology
Its complex structure of current aero-engine and can fail in the environment without air or rarefaction of air.Spacecraft
Driving mainly by airspace engine, its power consumption is high, needs to carry substantial amounts of fuel, it is difficult to long-time high-efficiency operation.
The content of the invention
In order to overcome existing aero-engine complex structure, can not work under without air or rarefaction of air environment, it is existing
There is the deficiency that space transportation is costly and inefficient, the present invention provides a kind of centrifugation force driving device, and the device can realize empty day
One drives and simple structure, low cost, efficiency high.
The technical solution adopted for the present invention to solve the technical problems is：Vacuumize in a sealing shell, have in it
Limit ring, spiral arm group, centrifugal column, slidably spiral arm. reducing motor, high rotating speed heavy-duty motor. rotating shaft, limit ring fixed knot
Structure.
The two ends of restriction ring fixing structure respectively have a hollow shaft and axle center is on the same line, in sealing shell
And can rotate along hollow shaft, two opposing parallel restriction rings are fixed inside it, limit ring place plane and limit ring and consolidate
The hollow rotating shaft of fixed structure is vertical, limits ring and is used for limiting the movement locus of centrifugal column.In the hollow shaft for limiting ring fixing structure
Interior installation rotating shaft.Two groups of spiral arm groups are fixed in rotating shaft, the spiral arm of spiral arm group is vertical with rotating shaft, consolidated positioned at limiting ring and limiting ring
Between the hollow rotating shaft of fixed structure, each spiral arm group has eight spiral arms, each on every spiral arm to cover a slidably spiral arm, between the two
Slidably.Centrifugal column has eight, and a circular hole perpendicular to the post heart is opened at every two ends, and sliding for different group is inserted in respectively
Dynamic cantilever, slidably between cantilever and centrifugal column also slidably.High rotating speed heavy-duty motor is fixed on sealing shell inwall, its
Rotor and rotating shaft connect, and drive rotating shaft, slidably spiral arm group, spiral arm and centrifugal column.Reducing motor is arranged on sealing shell inwall
On, drive and limit ring fixing structure rotation, control the direction of tractive force.
The invention has the beneficial effects as follows：Can efficiently at low cost from ground using the transport facility of the driving means
Empty day flight is realized to space is arrived again in the air, it is also possible to for spaceship and detector, particularly with nuclear energy energy supply in face
When, can preferably carry out longer-distance universe exploration.
Description of the drawings
In appended figure, in nonrestrictive citing form, one embodiment of the present of invention is illustrated.
Fig. 1 is the sectional side elevation of the embodiment of the present invention.
Fig. 2 is the cross sectional view of the embodiment of the present invention.
1. sealing shell in figure, 2. limits ring, 3. spiral arm group, 4. centrifugal column, 5. slidably spiral arm, 6. reducing motor, 7.
High rotating speed heavy-duty motor, 8. rotating shaft 9. limits ring fixing structure.
Specific embodiment
It is presented herein below in conjunction with the accompanying drawings and embodiments that the present invention will be further described.
In the embodiment shown in fig. 1, sealing shell (1) vacuumizes process in outermost layer inside it, to guarantee that air hinders
Power reaches minimum, while preventing dust to be poured into.Restriction ring fixing structure (9) is a cylindrical grid birdcage shaped configuration, up and down
Respectively there is a hollow shaft at two ends, and axle center on the same line, in sealing shell (1), can rotate along hollow shaft.Limiting
The two ends of close hollow rotating shaft are each in ring fixing structure (9) fixes restriction ring (2), limits ring (2) for limiting centrifugal column
(4) movement locus, limits ring (2) high hardness wear-resisting material manufacture, and the flat shape for limiting ring (2) inwall is left one
Semicircle (center of circle is in semicircle front-right), two ends respectively connect to the right length, and equal to semicircle radius line segment, (line segment is located in tie point
Tangent line on), the two lines section other end respectively connects in the same plane a quadrant (center of circle is in inner side), two four/
The radius of one circle is equal to 1/2nd of semicircle radius, and the distance between other end of two quadrants is equal to semicircle radius
And connected with straight line, the midpoint for limiting the circle center line connecting of two quadrants of ring (2) inwall is located at restriction ring fixing structure
(9) on the axle center of hollow shaft, it is vertical with the hollow shaft for limiting ring fixing structure (9) to limit ring (2) place plane.Rotating shaft (8)
In the hollow shaft for limiting ring fixing structure (9), between the two rotatably.It is located at rotating shaft (8) two ends and limits ring (2) and limit
Each between the hollow shaft of ring fixing structure (9) processed to fix a spiral arm group (3), spiral arm group (3) has two, and each has eight rotations
Arm, spiral arm and rotating shaft (8) are vertical.Slidably spiral arm (5) is open tubular column, is enclosed within the spiral arm of spiral arm group (3) and between the two may be used
Slide, at the same guarantee rotate when spiral arm group (3) spiral arm and slidably spiral arm (5) launch after will not touch limit ring fix
Structure (9).Centrifugal column (4) is cylindrical-shaped structure, there is eight, uses glass hard steel iron, it is ensured that while it has sufficient intensity
There are enough quality again, a hole perpendicular to the post heart is opened at every two ends, and the distance of holes is equal to upper two spiral arms of rotating shaft (8)
Distance between group (3), will not respectively be inserted in two of same centrifugal column (4) in the slidably spiral arm (5) on same spiral arm group (3)
In hole and between the two slidably, guarantee the post heart of every centrifugal column (4) respectively with the axle center of rotating shaft (8) in same flat during installation
It is in face and parallel, it is ensured that two can be allowed to limit ring (2) uniform stresseds when centrifugal column (4) is moved.High rotating speed heavy-duty motor
(6) in capsul (1), its rotor is connected with rotating shaft (8), for driving spiral arm group (3) to rotate, so as to drive centrifugal column
(4) along the inwall motion for limiting ring (2).Reducing motor (7) drives and limits ring fixing structure (9) in capsul (1)
Rotate with ring (2) is limited, to control to draw force direction.
Above structure can make centrifugal column (4) do circumference along the semicircle and two quadrants for limiting ring (2) inwall
Frequency during motion is identical.
To sum up told, by formula F=m ω2R=4m π2f2R understands, when centrifugal column (4) around rotating shaft (8) along restriction ring
(2) when inwall is moved, the centrifugal force on ring (2) inwall semicircle is limited is the twice on quadrant, slidably cantilever
(5) the centrifugal force ratio in relevant position can also be close to two-to-one, and the action time of power is identical, and the power difference for so being formed can
To drive object orientation motion.
Claims (4)
1. a kind of centrifugation force driving device, including sealing shell, restriction ring, spiral arm group, slidably centrifugal column, spiral arm, deceleration electricity
Machine, high rotating speed heavy-duty motor, rotating shaft, restriction ring fixing structure, it is characterised in that：Restriction ring is installed in sealing shell to fix
Structure, limits fixed restriction ring in ring fixing structure, limits and install in the hollow rotating shaft of ring fixing structure rotating shaft, fixed in rotating shaft
Spiral arm group, installs slidably spiral arm on the spiral arm of spiral arm group, centrifugal column, high rotating speed heavy-duty motor band are slidably installed on spiral arm
Dynamic rotating shaft, slidably spiral arm group, spiral arm and centrifugal column, reducing motor drives and limits ring fixing structure and restriction ring.
2. a kind of centrifugation force driving device told according to claim 1, it is characterised in that：Limit ring to be used for limiting centrifugal column
Movement locus, the flat shape of its inwall is one, left side semicircle (center of circle is in semicircle front-right), and the two ends of semicircle respectively connect
Length is equal to semicircle radius line segment (line segment is on the tangent line that tie point is located), and the two lines section other end respectively connects in the same plane
One quadrant (center of circle is in inner side), the radius of two quadrants is equal to 1/2nd of semicircle radius, two four
The distance between other end of/mono- circle is equal to semicircle radius and is connected with straight line.
3. a kind of centrifugation force driving device told according to claim 1, it is characterised in that：Two spiral arms are fixed in rotating shaft
Group, the spiral arm of spiral arm group is vertical with rotating shaft, between the hollow rotating shaft for limiting ring and limiting ring fixing structure, each spiral arm group
There are eight spiral arms, each on every spiral arm to cover a slidably spiral arm, between the two slidably, centrifugal column there are eight, and every two ends are each
A circular hole perpendicular to the post heart is opened, the distance of holes is equal to the distance of two spiral arm groups in rotating shaft, will not be in same spiral arm group
On slidably spiral arm be inserted in respectively in two holes of same centrifugal column and slidably, the post heart of every centrifugal column is respectively and rotating shaft
Axle center it is in the same plane and parallel.
4. a kind of centrifugation force driving device told according to claim 1, it is characterised in that：Restriction ring fixing structure is a circle
Respectively there is a hollow shaft at cylindricality grid birdcage shaped configuration, two ends, and axle center on the same line, in sealing shell and can turn
It is dynamic, limit ring and be fixed in restriction ring fixing structure, limit the midpoint position of the circle center line connecting of two quadrants of ring inwall
On the axle center of hollow shaft for limiting ring fixing structure, and its place plane is vertical with the hollow shaft for limiting ring fixing structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611059990.1A CN106628198A (en) | 2016-11-29 | 2016-11-29 | Centrifugal force driving device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611059990.1A CN106628198A (en) | 2016-11-29 | 2016-11-29 | Centrifugal force driving device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106628198A true CN106628198A (en) | 2017-05-10 |
Family
ID=58812184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611059990.1A Pending CN106628198A (en) | 2016-11-29 | 2016-11-29 | Centrifugal force driving device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106628198A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106800098A (en) * | 2015-11-26 | 2017-06-06 | 李宁 | A kind of space capsule structure design of generation acceleration of gravity |
| CN108545200A (en) * | 2018-04-25 | 2018-09-18 | 徐航 | A kind of aircraft |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102180265A (en) * | 2011-04-12 | 2011-09-14 | 陶红明 | Helicopter without rotor wing using centrifugal force as lifting force |
-
2016
- 2016-11-29 CN CN201611059990.1A patent/CN106628198A/en active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102180265A (en) * | 2011-04-12 | 2011-09-14 | 陶红明 | Helicopter without rotor wing using centrifugal force as lifting force |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106800098A (en) * | 2015-11-26 | 2017-06-06 | 李宁 | A kind of space capsule structure design of generation acceleration of gravity |
| CN108545200A (en) * | 2018-04-25 | 2018-09-18 | 徐航 | A kind of aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202550787U (en) | Flywheel battery | |
| CN103463829B (en) | The rotary packed bed mass transfer of the reverse shearing of air-flow and consersion unit | |
| CN104787315B (en) | Duct power set and aircraft | |
| CN102420493A (en) | Flywheel battery | |
| CN105378270B (en) | The application method of the device of wind-force supplement flying wheel battery energy in bicycle running | |
| CN106628198A (en) | Centrifugal force driving device | |
| CN203447804U (en) | Mass transfer and reaction device of rotary filler bed for shearing airflow reversely | |
| CN105804933A (en) | Double-rotating-vane vertical axis wind turbine | |
| US10988236B2 (en) | Pipe props rotary wing | |
| CN107053719A (en) | Belt transmits loop device | |
| CN207157510U (en) | A kind of air-ground amphibious MAV | |
| CN201647124U (en) | Magnetic suspension electrodynamic rotor wing flying disk | |
| CN101207346A (en) | Magnetic suspension accumulated energy flywheel | |
| JP5505749B1 (en) | Rotating device for power generator | |
| CN206885349U (en) | A kind of all-electric coaxial more Rotor thrust devices | |
| WO2020199311A1 (en) | U-shaped driver | |
| CN106915436A (en) | A kind of new culvert type propeller device and its implementation | |
| CN209159801U (en) | Differential control steering wheel mechanism and AGV trolley | |
| CN110013919B (en) | Vacuum pipeline magnetic suspension rock-soil centrifuge | |
| CN205618297U (en) | Two commentaries on classics leaf vertical scroll wind energy conversion systems | |
| CN214750297U (en) | Air cushion suspension type rock-soil centrifugal machine | |
| CN108360098A (en) | A kind of rings component for driving rotation with roller wheel bearing | |
| CN204352941U (en) | A kind of polydispersion dish dual spindle vertical turbine grinding distribution machine | |
| CN113252875A (en) | Air cushion suspension type rock-soil centrifugal machine | |
| CN107606088A (en) | Bicyclic buncher |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170510 |