CN104260894A - Spatial engine - Google Patents
Spatial engine Download PDFInfo
- Publication number
- CN104260894A CN104260894A CN201410542458.XA CN201410542458A CN104260894A CN 104260894 A CN104260894 A CN 104260894A CN 201410542458 A CN201410542458 A CN 201410542458A CN 104260894 A CN104260894 A CN 104260894A
- Authority
- CN
- China
- Prior art keywords
- flywheel
- engine
- space
- spin
- revolution
- 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
Landscapes
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
The invention discloses a spatial engine. The spatial engine comprises a flywheel rotation system, a flywheel revolution system and a system supporting frame, wherein the system supporting frame is used for supporting the flywheel rotation system and the flywheel revolution system; the flywheel rotation system comprises a flywheel, a flywheel stationary shaft, a flywheel controller, a flywheel rotation motor and a flywheel rotation shaft; the flywheel revolution system comprises a revolution shaft, a revolution motor, a control system and a revolution cantilever; the flywheel revolves around the revolution shaft along the revolution cantilever together with the flywheel stationary shaft, the flywheel controller, the flywheel rotation shaft and the flywheel rotation motor while rotating; the flywheel controller and the control system together control the movement state of the flywheel so as to control the movement state of the spatial engine. The spatial engine has the advantages of convenience in operation, low energy consumption, accurate movement direction and capability of moving towards any direction; by using a new movement mechanism, the spatial engine can directly act with a gravitational field to realize free movement in the gravitational field and low energy consumption for fixed-point stop in air.
Description
Technical field
The present invention relates to a kind of motion engine, particularly a kind of space engine.
Background technology
The existing engine used on space vehicle mainly comprises: aero-engine and airspace engine; The former uses in atmospheric envelope, and the latter can use outside endoatmosphere; These two kinds of engines, in its work, all by forcing gas to move in the opposite direction to engine movement side, and then make engine self obtain the antagonistic force of gas and advance; And when engine stops and do not move, the antagonistic force of gas must be relied on to offset gravity, lot of energy more aloft.Also having a kind of as fire balloon, the aircraft such as dirigible, is rely on the buoyancy of air to offset gravity, but due to the proportion of gas very little, therefore the volume of these aircraft is very large, inconvenience.In recent years, electromagnetic launch is also an active field of research, and electromagnetic launch directly relies on electromagnetic force to offset gravity, but is just in paraboloid state of kinematic motion by projectile once leave catapult-launching gear, can not move to arbitrary specific direction, there is inconvenience and uncertainty.In view of the shortcoming of existing space aircraft engine, we are badly in need of a kind of easy to operate, low power consuming, sense of motion space engine accurately.
Summary of the invention
The object of the present invention is to provide a kind of easy to operate, low power consuming, sense of motion controlled, use new locomotory mechanism, can directly and gravitational field have an effect, realize free motion in gravitational field and the space engine of aerial fixed point remaining low power consuming can be realized.
The present invention is achieved in that
Space of the present invention engine, uses in gravitational field, and space engine comprises flywheel spin system, flywheel revolution system and system holding frame; System holding frame supports described flywheel spin system and flywheel revolution system; Flywheel spin system comprises flywheel, flywheel anchor shaft, flywheel controller, flywheel spin motor and flywheel spin axis; Flywheel revolution system comprises hollow shaft, revoluting motor, control system and revolution cantilever; Flywheel is fixed in system holding frame by described flywheel anchor shaft, and flywheel spin motor is arranged on flywheel spin axis; Flywheel, while spin, spins together with motor with flywheel anchor shaft, the flywheel controller be arranged on flywheel anchor shaft, flywheel spin axis, the flywheel be arranged on flywheel spin axis and does publicly-owned rotation with the cantilever that revolves round the sun around hollow shaft; Revoluting motor and control system are set in turn on hollow shaft; The state of kinematic motion of flywheel controller and control system co-controlling flywheel; The state of kinematic motion of space engine reaches by controlling the state of kinematic motion of flywheel.
In the engine of space, flywheel can be one, two or multiple.
The abundant utilization law of conservation of angular momentum, realize a kind of new locomotory mechanism, make space of the present invention engine operation convenience, low power consuming, sense of motion accurately, can move to any direction, can directly and gravitational field have an effect, realize moving in gravitational field and aerial fixed point remaining low power consuming can be realized.
Space of the present invention engine, in the engine of space, flywheel, while spin, does publicly-owned rotation around hollow shaft.
Make full use of the law of conservation of angular momentum, reach the aerial technical advantage stopping low power consuming.
Space of the present invention engine, the state of kinematic motion of space engine is realized by the change controlling flywheel spin states.
Flywheel controller is by controlling the change of flywheel flywheel spin states in its process of revolution, the motion of implementation space engine in gravitational field.
Flywheel spin states has two kinds: illegal state and enabled state; During flywheel spin, the angle between flywheel spin axis and hollow shaft is θ.
Illegal state: 0 °≤θ≤30 °; Or flywheel roll rate is zero.
Enabled state: 30 ° of < θ≤90 °, and flywheel roll rate is non-vanishing.
By the alternately change of flywheel spin states, the motion of implementation space engine.This implementation, consumes energy little, easily realizes.
Space of the present invention engine, in the first implementation, flywheel anchor shaft and flywheel spin axis are same axle.
In this implementation, the illegal state of flywheel is: flywheel roll rate is zero.
Space of the present invention engine, in the second implementation, flywheel is fixed in flywheel fixed frame, and flywheel anchor shaft is by being fixed on flywheel in system holding frame the fixing of flywheel fixed frame.
Further, flywheel fixed frame is provided with the cross bar for fixing flywheel spin axis.
In this implementation, the illegal state of flywheel is: 0 °≤θ≤30 °.
This implementation power consumption is little, and it is convenient to realize.
Space of the present invention engine, when the sense of motion of space engine is contrary with gravitational field direction, control system control flywheel is positioned at gravitational field direction forward two quadrants when publicly-owned rotation are in illegal state, are in enabled state at two quadrants being positioned at gravitational field direction reverse.
Space of the present invention engine, when the sense of motion of space engine is identical with gravitational field direction, control system control flywheel is positioned at two reverse quadrants of gravitational field direction and is in illegal state, is in enabled state at two quadrants being positioned at gravitational field direction forward when publicly-owned rotation.
When space engine needs to becoming the direction of angle α to move with gravitational field direction, during 0 °≤α <90 °, take sense of motion as z-axis positive axis, with in the three dimensional space of the plane vertical with sense of motion for xy plane, in two spaces (space of axle is born in the space of z-axis positive axis, z-axis) formed for division plane with this plane, control system by drg control flywheel be positioned at the space of z-axis positive axis when publicly-owned rotation time, flywheel is in illegal state, flywheel is positioned at z-axis when bearing the space of axle, and flywheel is in enabled state.
When space engine needs to becoming the direction of angle α to move with gravitational field direction, during 90 ° of < α≤180 °, take sense of motion as z-axis positive axis, with in the three dimensional space of the plane vertical with sense of motion for xy plane, in two spaces (space of axle is born in the space of z-axis positive axis, z-axis) formed for division plane with this plane, control system by drg control flywheel be positioned at when publicly-owned rotation z-axis bear the space of axle time, flywheel is in illegal state, when flywheel is positioned at the space of z-axis positive axis, flywheel is in enabled state.
By this set, just can realize motion engine of the present invention and move to any direction, instead of be only limitted to along gravitational field direction, deviate from gravitational field direction and move.
Multiple spaces of the present invention engine, space automotive engine system can be formed, space automotive engine system is installed on space vehicle and uses, not only there is the advantages such as low energy consumption, easy to operate, fixed point remaining low power consuming aloft, the trip that can also greatly be convenient for people to, alleviate traffic pressure, avoid traffic congestion.
Beneficial effect of the present invention is, space of the present invention engine, easy to operate, low power consuming, sense of motion accurately, can move to any direction, use new locomotory mechanism, can directly and gravitational field have an effect, realize free motion in gravitational field and aerial fixed point remaining low power consuming can be realized.
Accompanying drawing explanation
Fig. 1 is the structural representation of the space engine in embodiment 1;
Fig. 2 is the structural representation of the space engine in embodiment 2;
Fig. 3 is the right TV structure schematic diagram of the space engine in Fig. 2;
Fig. 4 is the structural representation after the removal system holding frame of space engine in Fig. 3.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention will be further described:
Embodiment 1
Space of the present invention engine, as shown in Figure 1,1 is flywheel spin system, 11 is flywheel (flywheel has two), and 12 is flywheel anchor shaft, and 13 is flywheel controller, 14 is flywheel spin motor, and 15 be flywheel spin axis (be same axle with flywheel anchor shaft 12); 2 flywheel revolution systems, 21 is hollow shaft, and 22 is revoluting motor, and 23 is control system, and 24 is revolution cantilever, and 3 is system holding frame.Flywheel controller 13 is drg, controls the speed of flywheel.
Space of the present invention engine, uses in gravitational field, and as shown in Figure 1, space engine comprises flywheel spin system 1, flywheel revolution system 2 and system holding frame 3; System holding frame 3 support flying wheel spin system 1 and flywheel revolution system 2; Flywheel spin system 1 comprises flywheel 11, flywheel anchor shaft 12, flywheel controller 13 and flywheel spin motor 14; Flywheel revolution system 2 comprises hollow shaft 21, revoluting motor 22, control system 23, revolution cantilever 24; Flywheel 11 is fixed in system holding frame 3 by flywheel anchor shaft 12, and flywheel controller 13 and flywheel spin motor 14 are also set in turn on flywheel anchor shaft 12; Flywheel 11 while spin, with flywheel anchor shaft 12 and be arranged at flywheel controller 13 on flywheel anchor shaft 12 and flywheel and spin together with motor 14 and do publicly-owned rotation with the cantilever 24 that revolves round the sun around hollow shaft 21; Revoluting motor 22 and control system 23 are set in turn on hollow shaft 21; The state of kinematic motion of flywheel controller 13 and control system 23 co-controlling flywheel 11; The state of kinematic motion of space engine reaches by controlling the change of flywheel 11 spin states.
Control system 23 controls by flywheel controller 13 two quadrants that flywheel 11 is positioned at gravitational field direction forward when publicly-owned rotation and being in illegal state (illegal state is zero to realize by controlling flywheel 11 roll rate), being in enabled state at two quadrants being positioned at gravitational field direction reverse, and then implementation space engine moves to the sense of motion contrary with gravitational field direction.
Embodiment 2
Space of the present invention engine, as shown in Figure 2-4,1 is flywheel spin system, and 11 is flywheel (flywheel has two), 12 is flywheel anchor shaft, and 13 is flywheel controller, and 14 is flywheel spin motor, 15 flywheel spin axiss, 16 is flywheel fixed frame, and 17 is cross bar; 2 flywheel revolution systems, 21 is hollow shaft, and 22 is revoluting motor, and 23 is control system, and 24 is revolution cantilever, and 3 is system holding frame.Flywheel controller 13 is tumbler, controls the upset of flywheel, and namely flywheel spins axial change.
Space of the present invention engine, uses in gravitational field, and as in Figure 2-4, space engine comprises flywheel spin system 1, flywheel revolution system 2 and system holding frame 3; System holding frame 3 support flying wheel spin system 1 and flywheel revolution system 2; Flywheel spin system 1 comprises flywheel 11, flywheel anchor shaft 12, flywheel controller 13 and flywheel spin motor 14; Flywheel revolution system 2 comprises hollow shaft 21, revoluting motor 22, control system 23, revolution cantilever 24; Flywheel 11 is fixed in flywheel fixed frame 16, and flywheel anchor shaft 12, by being fixed in system holding frame 3 to the fixing of flywheel fixed frame 16 by flywheel 11, flywheel fixed frame 16 is provided with the cross bar 17 for fixing flywheel spin axis 15; Flywheel controller 13 is arranged on flywheel anchor shaft 12; Flywheel spin motor 14 is arranged on flywheel spin axis 15; Flywheel 11, while spin, spins together with motor 14 with flywheel anchor shaft 12, the flywheel controller 13 be arranged on flywheel anchor shaft 12, flywheel spin axis 15, the flywheel be arranged on flywheel spin axis 15 and does publicly-owned rotation with the cantilever 24 that revolves round the sun around hollow shaft 21; Revoluting motor 22 and control system 23 are set in turn on hollow shaft 21; The state of kinematic motion of flywheel controller 13 and control system 23 co-controlling flywheel 11; The state of kinematic motion of space engine reaches by controlling the change of flywheel 11 spin states.
Control system 23 controls by flywheel controller 13 two quadrants that flywheel 11 is positioned at gravitational field direction forward when publicly-owned rotation and is in illegal state (illegal state is by changing spin axis direction, even if angle theta=0 ° between spin axis and hollow shaft 21, namely spin axis is parallel with hollow shaft 21 and reach), be in enabled state being positioned at two reverse quadrants of gravitational field direction, and then implementation space engine moves to the sense of motion contrary with gravitational field direction.
Space of the present invention engine, easy to operate, low power consuming, sense of motion accurately, can move to any direction, use new locomotory mechanism, can directly and gravitational field have an effect, realize free motion in gravitational field and aerial fixed point remaining low power consuming can be realized.
The above embodiment is only be described the preferred embodiment of the present invention; not scope of the present invention is limited; under not departing from the present invention and designing the prerequisite of spirit; the various distortion that those of ordinary skill in the art make technical scheme of the present invention and improvement, all should fall in protection domain that claims of the present invention determine.
Claims (10)
1. a space engine, is characterized in that, described space engine uses in gravitational field, and described space engine comprises flywheel spin system (1), flywheel revolution system (2) and system holding frame (3); Described system holding frame (3) supports described flywheel spin system (1) and flywheel revolution system (2); Described flywheel spin system (1) comprises flywheel (11), flywheel anchor shaft (12), flywheel controller (13), flywheel spin motor (14) and flywheel spin axis (15); Described flywheel revolution system (2) comprises hollow shaft (21), revoluting motor (22), control system (23) and revolution cantilever (24); Flywheel (11) is fixed in system holding frame (3) by described flywheel anchor shaft (12), and described flywheel controller (13) is arranged on described flywheel anchor shaft (12); Described flywheel spin motor (14) is arranged on described flywheel spin axis (15); Described flywheel (11), while spin, spins together with motor (14) with described flywheel anchor shaft (12), the flywheel controller (13) be arranged on described flywheel anchor shaft (12), flywheel spin axis (15), the flywheel be arranged on described flywheel spin axis (15) and does publicly-owned rotation with described revolution cantilever (24) around hollow shaft (21); Described revoluting motor (22) and control system (23) are set in turn on described hollow shaft (21); The state of kinematic motion of described flywheel controller (13) and control system (23) co-controlling flywheel (11); The state of kinematic motion of described space engine reaches by controlling the state of kinematic motion of described flywheel (11).
2. space as claimed in claim 1 engine, is characterized in that, the state of kinematic motion of described space engine is realized by the change controlling flywheel (11) spin states.
3. space as claimed in claim 2 engine, it is characterized in that, described flywheel (11) spin states comprises illegal state and enabled state, during described flywheel (11) spin, the angle between described flywheel (11) spin axis and described hollow shaft (21) is θ; In described illegal state, 0 °≤θ≤30 °, or described flywheel (11) roll rate is zero; In described enabled state, 30 ° of < θ≤90 °, and described flywheel (11) roll rate is non-vanishing.
4. space as claimed in claim 3 engine, is characterized in that, described flywheel anchor shaft (12) and described flywheel spin axis (15) are same axle.
5. space as claimed in claim 4 engine, it is characterized in that, described illegal state is: described flywheel (11) roll rate is zero.
6. space as claimed in claim 3 engine, it is characterized in that, described flywheel (11) is fixed in flywheel fixed frame (16), and described flywheel anchor shaft (12) is by being fixed on flywheel (11) in system holding frame (3) the fixing of flywheel fixed frame (16).
7. space as claimed in claim 6 engine, is characterized in that, described flywheel fixed frame (16) is provided with the cross bar (17) for fixing flywheel spin axis (15).
8. space as claimed in claim 7 engine, it is characterized in that, described illegal state is: 0 °≤θ≤30 °.
9. the space engine as described in any one of claim 5 or 8, it is characterized in that, when the sense of motion of described space engine is contrary with gravitational field direction, described control system (23) controls by described flywheel controller (13) two quadrants that flywheel (11) is positioned at gravitational field direction forward when publicly-owned rotation and is in illegal state, is in enabled state at two quadrants being positioned at gravitational field direction reverse.
10. the space engine as described in any one of claim 5 or 8, it is characterized in that, when the sense of motion of described space engine is identical with gravitational field direction, described control system (23) controls flywheel (11) by described flywheel controller (13) and is positioned at two reverse quadrants of gravitational field direction when publicly-owned rotation and is in illegal state, is in enabled state at two quadrants being positioned at gravitational field direction forward.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410542458.XA CN104260894A (en) | 2014-06-25 | 2014-10-14 | Spatial engine |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410289569.4 | 2014-06-25 | ||
| CN201410289569 | 2014-06-25 | ||
| CN201410542458.XA CN104260894A (en) | 2014-06-25 | 2014-10-14 | Spatial engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104260894A true CN104260894A (en) | 2015-01-07 |
Family
ID=52152529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410542458.XA Pending CN104260894A (en) | 2014-06-25 | 2014-10-14 | Spatial engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104260894A (en) |
-
2014
- 2014-10-14 CN CN201410542458.XA patent/CN104260894A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10479496B2 (en) | Magnetic orientation detent with motor assist | |
| JP6535137B2 (en) | Takeoff and landing control system and control method for unmanned aircraft | |
| US10370089B2 (en) | Weight-shifting coaxial helicopter | |
| US10502188B2 (en) | Wind-powered recharging for a weight-shifting coaxial helicopter | |
| CN103592099A (en) | Measuring equipment for wind tunnel free-rolling vibration test and measuring method thereof | |
| CN103317512B (en) | Extensible spherical robot mechanism | |
| CN203958613U (en) | The coaxial multi-rotor aerocraft of duct | |
| CN107161343A (en) | A kind of rotor wing unmanned aerial vehicle and its replacing battery system | |
| CN110803304B (en) | Satellite attitude control system | |
| CN205186507U (en) | Four rotor crafts of folded cascade | |
| CN209064371U (en) | It is a kind of can the unmanned plane photographic device that is shot of multi-angle | |
| CN104260894A (en) | Spatial engine | |
| CN111114807A (en) | Many rotor unmanned aerial vehicle keep away barrier device | |
| CN102267570A (en) | Method for realizing take-off by utilizing gravitational potential energy of aircraft to nose down and accelerate | |
| CN103213681A (en) | Six-degree-of-freedom four-shaft aircraft | |
| CN206931287U (en) | A kind of device for simulating micro-nano satellite motion | |
| CN105539825A (en) | Monitoring air vehicle | |
| CN103151897B (en) | A kind of structure of rotary magnetic transmission | |
| CN105346714A (en) | Vertical take-off and landing unmanned plane | |
| CN201459564U (en) | Modified airport runway | |
| CN103631280A (en) | Variable inertia reaction flywheel | |
| CN203759549U (en) | Biaxial omni-directional closed-loop indifference control solar automatic tracking system | |
| CN103244581B (en) | Spatial tether system elastic clamp piece brake mechanism | |
| CN206050066U (en) | A kind of portable multi-rotor aerocraft of Spliced type | |
| CN104802991A (en) | Micro single board type UAV (unmanned aerial vehicle) system with suction function and control method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150107 |
|
| RJ01 | Rejection of invention patent application after publication |