CN102152852A - Purely magnetomotive airplane - Google Patents
Purely magnetomotive airplane Download PDFInfo
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- CN102152852A CN102152852A CN200810031581XA CN200810031581A CN102152852A CN 102152852 A CN102152852 A CN 102152852A CN 200810031581X A CN200810031581X A CN 200810031581XA CN 200810031581 A CN200810031581 A CN 200810031581A CN 102152852 A CN102152852 A CN 102152852A
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Abstract
The invention discloses a purely magnetomotive airplane. The purely magnetomotive airplane consists of an airplane body (I), a clutch (II), an engine (III), a fixing bolt (IV) and a nut (V), wherein the airplane body (I) is connected with the engine (III) through the clutch (II); the engine (III) is connected with the airplane body (I) through the fixing bolt (IV) and the nut (V); and a magnet (2-2) serves as power in the engine (III). After the method is adopted, the purely magnetomotive airplane can fly without fuel; the flight cost is reduced; and flight is not restrained by distance and time.
Description
The aircraft that the present invention relates to aloft fly is as passenger plane and helicopter.
Existing aircraft, fast as the jet plane flying speed, but big with oil mass, and the propeller aircraft of piston engine, not only need be with oily, flying speed is slow simultaneously.The stroke and the time of their flight all are restricted.
Purpose of the present invention just provides a kind of pure magnetic motive force formula aircraft that need not with oil.
In order to reach above purpose, the principle of work of pure magnetic motive force formula aircraft of the present invention is: the driving engine of aircraft is to utilize mutual action between the magnet; And after the magnet conductively-closed, the character that magnetic force disappears is removed shielding when mechanism is needed magnetic force, and magnet produces magnetic force, when not needing magnetic force, opens mask switch and makes the magnet conductively-closed, and magnet does not produce magnetic force; Thereby reach with magnetic force and drive the engine mechanism work done.In order to satisfy principle of work, its technical scheme is: the driving engine of pure magnetic motive force formula aircraft of the present invention adopts the four-bar linkage induced way, magnetically-actuated mechanism is arranged in the middle of the slide block, being positioned on top magnet can attract each other, its length of slide block changes with the working condition of magnet, slide block one end is fixed, this length changes the drive link rod, crank and motion of main shaft, when slide block will drive link rod and crank when main shaft rotates, the mask switch of magnet is closed under the drive controlling mechanism controls, magnet is in non-shielding state, attracts each other between them, and slide block is the shortening process, this magnetic force that attracts each other drives link motion, thereby main shaft is rotated and generation power.When needing slide block to move upward because of the four-bar linkage motion, the mask switch of magnet is opened under driving control system control, the magnet of forming slide block is in masked state, magnet does not have magnetic force, can be separated from each other between them, at this moment, the motion of this place's magnet is driven by link rod, link rod is driven by main shaft, and main shaft is rotated by the magnet effect in the other slide block.Because slide block is very short by spurring link rod and being spurred fringe time by link rod, the rotation required time of the mask switch of magnet is longer relatively, therefore, only some is made up of expansion space stroke after producing suction between the magnet the whole stroke of slide block movement, another part is that non-magnet produces the suction movement travel, like this, another part stroke can solve above time difference problem.Above each several part can synthesize mechanical rotating mechanism, magnetically-actuated mechanism and drive controlling mechanism; Magnet and mask switch are arranged in the magnetically-actuated mechanism, electromagnet and switch are arranged in the drive controlling mechanism, switch control electromagnet, the make and break of magnet control screen is closed, and closing and open by the control of the part on the four-bar linkage of switch finished.Pure magnetic motive force formula aircraft of the present invention is made up of body, power-transfer clutch, driving engine, bolt of rear end plate and nut, and power-transfer clutch links driving engine and body, and driving engine is linked by bolt of rear end plate and nut and body.
In order to satisfy principle of work, its technical scheme is: the driving engine of pure magnetic motive force formula aircraft of the present invention is made up of mechanical transmission mechanism, magnetically-actuated mechanism and drive controlling mechanism, magnet and mask switch are arranged in the magnetically-actuated mechanism, and drive controlling mechanism also adopts mechanical mechanism.
In order to satisfy principle of work, its technical scheme is: the driving engine of pure magnetic motive force formula aircraft of the present invention adopts main shaft, crank and link rod transmission device, magnetically-actuated mechanism is arranged in the middle of the link rod, being positioned on top magnet can attract each other, and its method of work is identical with slide block in the top principle; The link rod bottom can be rotated around fixed point.
After adopting above method, pure magnetic motive force formula aircraft can fly under the situation of oil firing not, and flight cost is reduced, also make simultaneously the flying distance of aircraft and time unrestricted, do not need the oiling of making a return voyage again, improved the load ability to bear of aircraft, aircraft application is increased.
With drawings and Examples pure magnetic motive force formula aircraft of the present invention is described further below.
Accompanying drawing 1 is pure magnetic motive force formula aircraft the 1st an embodiment subssembly drawing of the present invention.
Accompanying drawing 2 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 3 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 4 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 5 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 6 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 7 is pure magnetic motive force formula aircraft the 1st an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 8 is pure magnetic motive force formula aircraft the 2nd an embodiment subssembly drawing of the present invention.
Accompanying drawing 9 is pure magnetic motive force formula aircraft the 2nd an embodiment subssembly drawing of the present invention.
Accompanying drawing 10 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 11 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 12 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 13 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 14 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 15 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 16 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 17 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 18 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 19 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 20 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 21 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 22 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 23 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 24 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 25 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 26 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 27 is pure magnetic motive force formula aircraft the 2nd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 28 is pure magnetic motive force formula aircraft the 2nd embodiment electrical control circuit figure of the present invention.
Accompanying drawing 29 is pure magnetic motive force formula aircraft the 3rd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 30 is pure magnetic motive force formula aircraft the 3rd an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 31 is pure magnetic motive force formula aircraft the 4th an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 32 is pure magnetic motive force formula aircraft the 5th an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 33 is pure magnetic motive force formula aircraft the 6th an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 34 is pure magnetic motive force formula aircraft the 7th an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 35 is pure magnetic motive force formula aircraft the 7th an embodiment partial assembled enlarged drawing of the present invention.
Accompanying drawing 36 is pure magnetic motive force formula aircraft the 7th an embodiment partial assembled enlarged drawing of the present invention.
At accompanying drawing 1 to the 1st embodiment shown in the accompanying drawing 7, the driving engine of pure magnetic motive force formula aircraft of the present invention is made up of body (I), power-transfer clutch (II), driving engine (III), bolt of rear end plate (IV) and nut (V), and body (I) power-transfer clutch (II) links with driving engine (III); Driving engine (III) is linked with body (I) by bolt of rear end plate (IV) and nut (V); Driving engine (III) is by mechanical transmission mechanism (1), magnetically-actuated mechanism (2) and drive controlling mechanism (3) form, mechanical transmission mechanism (1) is by cabinet (1-1), main shaft (1-2), the shank of connecting rod (1-3) and movable block (1-4) are formed, cabinet (1-1) is by casing (1-1-1), case lid (1-1-2), bolt (1-1-3) and nut (1-1-4) are formed, main shaft (1-2) is by main shaft (1-2-1), bearing (1-2-2), cover (1-2-3), end cap (1-2-4), spindle nut (1-2-5) and bolt of cover (1-2-6) are formed, the shank of connecting rod (1-3) is by link rod (1-3-1), lid (1-3-2), bolt (1-3-3), nut (1-3-4), attachment bolt (1-3-5) and nut (1-3-6) are formed, bolt (1-3-3) and nut (1-3-4) link lid (1-3-2) and link rod (1-3-1) respectively with main shaft (1-2-1), cover (1-2-3), bearing (1-2-2) and spindle nut (1-2-5) are positioned on the main shaft (1-2-1), and casing (1-1-1) and case lid (1-1-2) are linked by bolt (1-1-3) and nut (1-1-4).Link rod (1-3-1) is linked with intermediate bar (1-4-1) by attachment bolt (1-3-5) and nut (1-3-6).Movable block (4-1) is made up of intermediate bar (1-4-1), cover plate (1-4-2), intermediate plate (1-4-3), spring (1-4-4), bolt (1-4-5), base plate (1-4-6), stove bolt (1-4-7), nut (1-4-8) and primary nut (1-4-9) and spring cotter (1-4-10); Magnetic force pedestal (2-1) and intermediate plate (1-4-3) are positioned on the casing (1-1-1) by stove bolt (1-4-7), after putting into spring (1-4-4) between two intermediate plates (1-4-3), be coupled to each other by bolt (1-4-5) and nut (1-4-8), the end is equipped with spring cotter (1-4-10), and connecting between intermediate plate (1-4-3) and the base plate (1-4-6) is also the same.Magnetically-actuated mechanism (2) is made up of magnetic force pedestal (2-1), magnet (2-2), switch (2-3), shell (2-4), cover plate (2-5) and stove bolt (2-6); Drive controlling mechanism (3) is by electromagnet (3-1), lead (3-2), touch switch (3-3) and bolt (3-4) are formed, touch switch (3-3) is by axle (3-3-1), body skin (3-3-2), spring (3-3-3), ball (3-3-4), stop up (3-3-5), setscrew nut (3-3-6), touch panel (3-3-7) and locating plate (3-3-8) are formed, axle (3-3-1) is put into the hole of body skin (3-3-2), in the trough of touch panel (3-3-7) difference glue on body skin (3-3-2) and axle (3-3-1), after ball (3-3-4) and spring (3-3-3) are put into the hole of body skin (3-3-2), on go into to stop up (3-3-5), setscrew nut (3-3-6) is positioned on axle (3-3-1) end, locating plate (3-3-8) is positioned on the intermediate bar (1-4-1) by bolt (3-4), and touch switch (3-3) is positioned on the cover plate (1-4-2) by bolt (3-4).Electromagnet (3-1) is positioned on the magnetic force pedestal (2-1) by bolt (3-4), after the lead of power supply (3-2) passes through from the hole of axle (3-3-1), receive on the touch panel (3-3-7) that is positioned on axle (3-3-1), the touch panel (3-3-7) that is positioned on the body skin (3-3-2) links with cooresponding electromagnet (3-1) by penetrating lead (3-2) in the hole in the body skin (3-3-2), and electromagnet (3-1) other end takes back power supply.Magnet (2-2) is placed in the magnetic force pedestal (2-1), and the protuberance of switch (2-3) is stuck in the groove of magnet (2-2), and cover plate (2-5) is fixing by stove bolt (2-6) and magnetic force pedestal (2-1), and shell (2-4) is stuck on the switch (2-3).When power supply is switched on, touch switch (3-3) is switched on, and behind the shell (2-4) on electromagnet (3-1) suction shaft (2-3), drives switch (2-3) and rotates, and magnet (2-2) does not have conductively-closed.Thereby make the outside magnetic force generation effect of magnet (2-2), magnetically-actuated mechanism (2) produces magnetic force, and begin to attract each other, close mutually between the magnetic force pedestal (2-1), link rod (1-3-1) moves down, simultaneously, spring (1-4-4) is compressed, when near extreme lower position, it is downward that locating plate (3-3-8) is pushed down axle (3-3-1), the touch panel of two contacts (3-3-7) is separated, being positioned on the touch panel (3-3-7) of axle on (3-3-1) contacts with another touch panel (3-3-7) on being positioned on body skin (3-3-2), at this moment, be positioned on the magnetic force pedestal (2-1), originally Gong Zuo electromagnet (3-1) is de-energized and quits work, another group electromagnet (3-1) is switched on, switch (2-3) rotates to other direction, magnet (2-2) conductively-closed, magnetically-actuated mechanism (2) does not have magnetic force, do not have suction between each magnetic force pedestal (2-1), they are under link rod (1-3-1) and spring (1-4-4) effect, and distance constantly increases each other, run into touch switch (3-3) up to intermediate bar (1-4-1), begin another working cycle again.The rotation of main shaft (1-2-1) is finished by another group magnetically-actuated mechanism (2).Driving engine (III) is passed to body (I) with the energy of gained.
At accompanying drawing 1, accompanying drawing 8 to the 2nd embodiment shown in the accompanying drawing 28, the driving engine of pure magnetic motive force formula aircraft of the present invention is made up of mechanical transmission mechanism (4), magnetically-actuated mechanism (5) and drive controlling mechanism (6), and mechanical transmission mechanism (4) is made up of casing assembly (4-1), main shaft assembly (4-2) and link rod part (4-3); Magnetically-actuated mechanism (5) is made up of magnet base part (5-1), connection seat part (5-2), bearing support (5-3), limit tube part (5-4) and reaction spring part (5-5); Partly (6-3) and electrical control part (6-4) are formed with joint efforts by power transfer part (6-1), contact switch part (6-2), electromagnetism in drive controlling mechanism (6); Casing assembly (4-1) is made up of casing (4-1-1), case lid (4-1-2), casing bolt (4-1-3) and nut (4-1-4); Main shaft assembly (4-2) is made up of main shaft (4-2-1), bearing (4-2-2), intermediate sleeve (4-2-3), end cap (4-2-4), bolt of cover (4-2-5) and spindle nut (4-2-6); Link rod part (4-3) is made up of link rod (4-3-1), link rod lid (4-3-2), lid bolt (4-3-3), lid nut (4-3-4), attachment bolt (4-3-5) and coupling nut (4-3-6); Magnet base part (5-1) is made up of magnet (5-1-1), shell (5-1-2), knob (5-1-3), cover clamp (5-1-4) and stove bolt (5-1-5); Coupling part (5-2) is made up of pedestal (5-2-1), bolt (5-2-2) and nut (5-2-3); Bearing support (5-3) is made up of back plate (5-3-1), cushion rubber (5-3-2), buffing pad (5-3-3), stove bolt (5-3-4), nut (5-3-5), overbolt (5-5-6), nut (5-3-7) and cushion block (5-3-8); Limit drum segment (5-4) is made up of cylinder (5-4-1), bolster (5-4-2) and nut (5-4-3); Reaction spring (5-5) is made up of spring (5-5-1) and stand (5-5-2); Power transfer part (6-1) is made up of engaging gear (6-1-1), transmission shaft (6-1-2), little cover (6-1-3), bearing (6-1-4), sleeve (6-1-5), positioning screw (6-1-6), touch panel (6-1-7), end cap (6-1-8), bolt of cover (6-1-9) and spindle nut (6-1-10); Touching main supply switch part (6-2) is made up of feeler lever (6-2-1), spring (6-2-2), touch panel (6-2-3), stem nut (6-2-4) and spring cotter (6-2-5); Electromagnetism is made a concerted effort partly, and (6-3) is made up of electromagnet (6-3-1), attachment bolt (6-3-2), nut (6-3-3), link rod (6-3-4), roller (6-3-5), gusset piece (6-3-6), bull stick (6-3-7), fork (6-3-8), middle cover (6-3-9) and long bolt (6-3-10); The electrical equipment control total value is sent out (6-4) and is made up of lead P, contact switch K and electromagnet R.Casing (4-1-1) and case lid (4-1-2) are linked by casing bolt (4-1-3) and nut (4-1-4).Main shaft (4-2-1), bearing (4-2-2) and intermediate sleeve (4-2-3) are positioned in the casing (4-1-1), and end cap (4-2-4) is positioned on the casing assembly (4-1) by end cap nut (4-2-5), and spindle nut (4-2-6) is positioned on main shaft (4-2-1) end; Link rod (4-3-1) and link rod lid (4-3-2) are linked by lid bolt (4-3-3) and lid nut (4-3-4); Link rod (4-3-1) and pedestal (5-2-1) are linked by attachment bolt (4-3-5) and coupling nut (4-3-6).Magnet (5-1-1) is placed in the shell (5-1-2), and the protuberance of knob (5-1-3) is stuck in the groove of magnet (5-1-1), and cover clamp (5-1-4) is linked by bolt (5-1-5) and shell (5-1-2); Pedestal (5-2-1) and shell (5-1-2) are linked with back plate (5-3-1) by bolt (5-2-2) and nut (5-2-3) respectively; When turning knob (5-1-3) during to left end, magnet (5-1-1) does not have conductively-closed, magnet base part (5-1) produces magnetic force, and cushion rubber (5-3-2) is stuck in the buffing pad (5-3-3), and buffing pad (5-3-3) is linked with back plate (5-3-1) by stove bolt (5-3-4) and nut (5-3-5); Connect by overbolt (5-3-6) and nut (5-3-7) between the back plate (5-3-1) and between back plate (5-3-1) and the casing (4-1-1), between them, be lined with cushion block (5-3-8).After bolster (5-4-2) passes back plate (5-3-1), cylinder (5-4-1) and back plate (5-3-1), nut (5-4-3) is positioned on the bolster (5-4-2), spring (5-5-1) is positioned in the stand (5-5-2), and stand (5-5-2) is welded on the casing (4-1-1); Two engaging gears (6-1-1), one is positioned on main shaft (4-2-1) spline, another is positioned on transmission shaft (6-1-2) spline, little cover (6-1-3), bearing (6-1-4) and sleeve (6-1-5) are positioned on the transmission shaft (6-1-2), positioning screw (6-1-6) links sleeve (6-1-5) and transmission shaft (6-1-2), touch panel (6-1-7) is glued on the sleeve (6-1-5), and spindle nut (6-1-10) is positioned on transmission shaft (6-1-2) two ends; Bolt of cover (6-1-9) is positioned on end cap (6-1-8) on the casing assembly (4-1); Lead P comes out from power supply, the touch panel (6-1-7) that at first being connected on the high order end whole circumference all has is gone up [other 4 sleeves (6-1-5), the touch panel (6-1-7) that has only 1 circular arc above each], pass by the hole in sleeve (6-1-5) and the little cover (6-1-3) from this touch panel (6-1-7) again, respectively with other 4 sleeves (6-1-5) on touch panel (6-1-7) link, contact block (6-2-3) is stuck on the feeler lever (6-2-1), after feeler lever (6-2-1) passes spring (6-2-2) and casing (4-1-1), first-class stem nut (6-2-4) and spring cotter (6-2-5), lead P and contact block (6-2-3) join; Electromagnet (6-3-1) is installed on back plate (5-3-1) and the link rod (6-3-4) by bolt (6-3-2) and nut (6-3-3), bolt (6-3-2) passes gusset piece (6-3-6), link rod (6-3-4) and gusset piece (6-3-6) and links with nut (6-3-3), and bolt (6-3-2) passes gusset piece (6-3-6), roller (6-3-5) and gusset piece (6-3-6) and links with nut (6-3-3); Bull stick (6-3-7), intermediate sleeve (6-3-9) and link rod (6-3-4) are linked by long bolt (6-3-10) and nut (6-3-3), bull stick (6-3-7) and fork (6-3-8) are linked by bolt (6-3-2) and nut (6-3-3), and fork (6-3-8) and knob (5-1-3) are linked by bolt (6-3-2) and nut (6-3-3).In the entire circuit design, switch has main supply switch K
0, contact switch Kab and K switch cb; Electromagnet (6-3-1) represented by Rbd, wherein K
0For can connecting the switch of two circuit, can about closed, can form two kinds of different working condition Kab like this and represent contact switch, wherein a represents the contact switch sequence number, b represents slide block sequence number number; B among the Rbd represents slide block sequence number number, and d represents the ordinal number of electromagnet (6-3-1), wherein 1,2 and 3 represents left side electromagnet (6-3-1), and 4,5 and 6 represent the right side; 1 and 4 represent the 1st layer electromagnet (6-3-1), and 2 and 5 represent the 2nd layer of electromagnet (6-3-1), and 3 people 6 represent the 3rd layer of electromagnet (6-3-1); As main supply switch K
0When closing to the left, power supply enters each contact switch Kab place, because contact switch Kab is made up of touch panel (6-1-7) and contact block (6-2-3), this contact switch Kab has four, each is seen on same axle section and differs 90 degree, simultaneously, after lead P comes out from touch panel (6-2-3), link with other two lead P, one of these leads P connects left side three electromagnet (6-3-1) in this drive controlling mechanism (6), another root connects three electromagnet in right side (6-3-1) in another drive controlling mechanism (6) that differs 180 degree, thereby reach link rod (4-3-1) when moving to nadir, Kab is switched on left side three electromagnet (6-3-1) circuit, magnet (5-1-1) conductively-closed, can not produce magnetic force, its motion is driven by main shaft (4-2-1), meanwhile, and corresponding middle three electromagnet in right side (6-3-1) circuit of another drive controlling mechanism (6) that differs 180 degree is switched on, the magnet (5-1-1) of its corresponding control is not increased by screen, produce work done by magnetic force, drive link rod part (4-3) and move downward, thereby main shaft (4-2-1) is rotated, other two groups of link rods parts (4-3) also have corresponding state of kinematic motion.As main supply switch K
0When closing to the right, with K
21, K
22, K
23And K
24Connect, all magnet (5-1-1) all screen close, and magnet (5-1-1) does not have magnetic force, thereby reach the purpose of stopping burning of stopping.In the time will starting, with K
21, K
22, K
23And K
24Disconnect K
0Close to the left to close and get final product.Because main shaft (4-2-1) is by two identical gear meshing gears (6-1-1) transferring power, so, the moving situation of it and transmission shaft (6-1-2) is identical, the suffered pulling force of four link rods (4-3-1) all is to produce when moving downward, and 90 degree that stagger mutually, thereby make whole engine stressed even in operation process.When link rod (4-3-1) up-and-down movement, cylinder (5-4-1) supports the easy motion of whole back plate (5-3-1); When back plate (5-3-1) when moving downward, each cushion rubber (5-3-2) is in contact with one another respectively, and does not contact between the shell (5-1-2), thereby prevents that magnet base part (5-1) is damaged and produces big noise; The spring (5-5-2) of casing (4-1-1) bottom is compressed; When back plate (5-3-1) upward movement, spring (5-5-2) is upspring, and bolt (5-3-6) has been held each back plate (5-3-1), simultaneously, because of cushion block (5-3-8) has been arranged noise is reduced.
At accompanying drawing 1, accompanying drawing 8, accompanying drawing 9, accompanying drawing 12 to accompanying drawing 27, and among the 3rd embodiment shown in accompanying drawing 29 and the accompanying drawing 30, pure magnetic motive force formula aircraft of the present invention and the 2nd embodiment difference are: the shielding mode of controlling magnet (5-1-1) is transformed into mechanical type control by original electromagnetic type control.On its concrete structure be: electromagnet (6-3-1) and electrical control part (6-4) that original contact switch part (6-2), electromagnetism are made a concerted effort in the part (6-3) all remove, its little cover (6-1-3) and touch panel (6-1-7) on transmission shaft (6-1-2) removes, increased mechanical control mechanism (7), mechanical control mechanism (7) is made up of resilience car part (7-1) and half wheel part (7-2); Resilience car part (7-1) is made up of car body (7-1-1), underframe (7-1-2), bottom roller (7-1-3), spring (7-1-4), spring pedestal (7-1-5), roller (7-1-6), roller cushion cover (7-1-7), pinch roller (7-1-8), pinch roller seat (7-1-9), pinch roller screw rod (7-1-10), pinch roller nut (7-1-11), stove bolt (7-1-12) and nut (7-1-13); Partly doing part (7-2) is made up of half wheel (7-2-1) and positioning screw (7-2-2).Underframe (7-1-12) is welded in car body (7-1-1) bottom, stove bolt (7-1-12) and nut (7-1-13) are positioned on bottom roller (7-1-3) on the underframe (7-1-2), spring pedestal (7-1-5) is welded on the casing (4-1-1), spring (7-1-4) is placed in the spring pedestal (7-1-5), and roller (7-1-6), roller cushion cover (7-1-7) and link rod (6-3-4) [link rod (6-3-4) end has increased annulus] are linked by stove bolt (7-1-12) and nut (7-1-13); Pinch roller seat (7-1-9) is installed on the car body (7-1-1) by stove bolt (7-1-12), and pinch roller (7-1-8) is installed on the pinch roller seat (7-1-9) by pinch roller screw rod (7-1-10) and pinch roller nut (7-1-11).Half wheel (7-2-1) is installed on the transmission shaft (6-1-2) by positioning screw (7-2-2).The control of the magnet base part (5-1) in the present embodiment directly adopts transmission shaft (6-1-2) to finish.After transmission shaft (6-1-2) rotates, being positioned on half top wheel (7-2-1) rotates, when protuberance and pinch roller (7-1-8) when contacting, resilience car part (7-1) is extruded, link rod (6-3-4) translation to the right, when partly taking turns (7-2-1) when being rotated further low level, resilience car part (7-1) translation to the left under spring (7-1-4) effect.
At accompanying drawing 1, accompanying drawing 8, accompanying drawing 9, accompanying drawing 12 to the 4th embodiment shown in accompanying drawing 27 and the accompanying drawing 31, pure magnetic motive force formula aircraft of the present invention and the 2nd embodiment difference are: the action of half wheel (7-2-1) of control resilience car part (7-1) is replaced by electromagnet (6-3-1), and electromagnet (6-3-1) has only one group in left side.[right side electromagnet (6-3-1) by taken down], its control is close with the 2nd embodiment, and difference is: this electromagnet (6-3-1) is positioned on resilience car partly (7-1) and above the casing (4-1-1).When electromagnet (6-3-1) when being switched on, resilience car part (7-1) moves to the left; When electromagnet (6-3-1) when power supply is disconnected, spring (7-1-4) is pushing away resilience car part (7-1) and is moving to the right, reaches translation control magnet base part (5-1) work of link rod (6-3-4), thereby controls the braking and the work of whole driving engine.
To the 5th embodiment shown in accompanying drawing 27 and the accompanying drawing 32, pure magnetic motive force formula aircraft of the present invention and the 4th embodiment difference are: the work of electromagnet (6-3-1) is replaced by pneumatic part (8) at accompanying drawing 1, accompanying drawing 8, accompanying drawing 9, accompanying drawing 12.Pneumatic part (8) is made up of cylinder (8-1), air valve (8-2), tracheae (8-3) and bolt (8-4).Cylinder (8-1) is linked by tracheae (8-3) and air valve (8-2), and source of the gas inserts air valve (8-2), and the electromagnetic valve switch of air valve (8-2) is controlled by contact switch Kab.Kab is switched on when contact switch, this electromagnetic valve is opened air valve (8-2), cylinder (8-1) promotes resilience car part (7-1) and moves to the left side, Kab is closed when contact switch, there is not pressure gas in the cylinder (8-1), spring (7-1-4) promotes resilience car part (7-1) and moves to the left side, thereby reaches translation control magnet base part (5-1) work of link rod (6-3-4), drives main shaft (4-2-1) and rotates.
To the 6th embodiment shown in accompanying drawing 28 and the accompanying drawing 33, pure magnetic motive force formula aircraft of the present invention and the 2nd embodiment difference are: it is not that propulsion source is placed on the slide block, but is placed in the link rod at accompanying drawing 1, accompanying drawing 9.Mechanical transmission mechanism on the concrete structure (4) is replaced by new bar part (9) with main shaft assembly (4-2) (identical with former scheme), link rod part (4-3) by casing assembly (4-1).New bar part (9) is made up of the new body of rod (9-1), body skin (9-2), attachment bolt (9-3) and coupling nut (9-4).The new body of rod (9-1) is by the body of rod (9-1-1) [former link rod (4-3-1) is synthesized together with pedestal (5-2-1)], bowl cover (9-1-2), lid bolt (9-1-3) and nut (9-1-4) are formed, the bowl cover (9-1-2) and the body of rod (9-1-1) are linked by lid bolt (9-1-3) and nut (9-1-4), the centre is equipped with main shaft (4-2-1), and link rod (4-3-1) is linked with back plate (5-3-1) by bolt (5-2-2) and nut (5-2-3).Connected by overbolt (5-3-6) and nut (5-3-7) between back plate (5-3-1) and the body skin (9-2), stand (5-5-2) is welded on the body skin (9-2); Body skin (9-2) is linked with casing (4-1-1) by attachment bolt (9-3) and coupling nut (9-4).When magnetically-actuated mechanism (5) worked in body skin (9-2), body skin (9-2) rotated around coupling nut (9-3), and the body of rod (9-1-1) rotates around main shaft (4-2-1).
At accompanying drawing 1, accompanying drawing 8 and accompanying drawing 9, accompanying drawing 12 is to accompanying drawing 27, accompanying drawing 29 to accompanying drawing 30 and accompanying drawing 34 to the 7th embodiment shown in the accompanying drawing 36, pure magnetic motive force formula aircraft of the present invention and the 3rd embodiment difference are: increased dwang part (10), simultaneously, casing assembly (4-1), main shaft (4-2-1), end cap (6-1-8) and transmission shaft (6-1-2) change to some extent.Dwang part (10) is made up of bull stick (10-1), bearing (10-2), cover (10-3) spindle nut (10-4), end cap (10-5), end cap nut (10-6); Have groove P (as shown in Figure 35) on the case lid (4-1-2), also for flute profile is arranged, behind main shaft (4-2-1) and transmission shaft (6-1-2) the two ends lengthening, bull stick (10-1) can be installed in the middle of the end cap (6-1-8).Bull stick (10-1) is installed in main shaft (4-2-1) and transmission shaft (6-1-2) two ends, and bearing (10-2), cover (10-3) and spindle nut (10-4) are positioned on main shaft (4-2-1) two ends, and spindle nut (10-4) is positioned on transmission shaft (6-1-2) two ends.
The present invention is above several schemes of limit only, and when in the technical scheme not being mutual use between the magnet, but magnet is to the effect of magnetic conductor (as iron); In the 1st embodiment, remove spring (1-4-4); In the 2nd embodiment, remove spring (5-5-1); In the 1st embodiment, add the 2nd embodiment medi-spring (5-5-1); In the 2nd embodiment, add upper spring (1-4-4); When magnet (5-1-1) is electromagnet; Pneumatic part in the 5th embodiment (8) is a hydraulic part, adopts hydraulic part to get the moving part of ventilation; When main shaft (4-2-1) is with power-transfer clutch; When above scheme combination; Each screw propeller of the single driving of driving engine; When above many parallel connections (or series connection) all are content of the present invention when using.
Claims (19)
1. a pure magnetic motive force formula aircraft is made up of body (I), power-transfer clutch (II), bolt of rear end plate (IV) and nut (V), and body (I), power-transfer clutch (II) link with driving engine (III); Driving engine (III) is linked with body (I) by bolt of rear end plate (IV) and nut (V), and it is characterized in that: the power of driving engine (III) derives from the magnetic force of magnet (2-2) and magnet (5-1-1) respectively; In service at whole engine, when the magnetic force of magnet (2-2) and magnet (5-1-1) will produce power, rotate by switch (2-3) and knob (5-1-3) respectively, make the not shielding of magnet (2-2) and magnet (5-1-1), when in idle travel, switch (2-3) and knob (5-1-3) rotate respectively, the conductively-closed respectively of magnet (2-2) and magnet (5-1-1), and magnet (2-2) and magnet (5-1-1) outwards do not have magnetic force respectively.
2. pure magnetic motive force formula aircraft according to claim 1 is characterized in that: the driving engine (III) of pure magnetic motive force formula aircraft is made up of mechanical transmission mechanism (1), magnetically-actuated mechanism (2) and drive controlling mechanism (3); Magnetically-actuated mechanism (2) produces power by magnet (2-2), control magnetically-actuated mechanism of drive controlling mechanism (3) (2) work, and mechanical transmission mechanism (1) outwards transmits the power that produces by the certain movement rule.
3. according to claim 1,2 described pure magnetic motive force formula aircrafts, it is characterized in that: magnetically-actuated mechanism (2) is made up of magnetic force pedestal (2-1), magnet (2-2), switch (2-3), shell (2-4), cover plate (2-5) and stove bolt (2-6); Magnet (2-2) is placed in the magnetic force pedestal (2-1), the protuberance of switch (2-3) is stuck in the groove of magnet (2-2), cover plate (2-5) is fixing by stove bolt (2-6) and magnetic force pedestal (2-1), shell (2-4) is stuck on the switch (2-3), can control magnet (2-2) when rotating switch (2-3) and outwards whether produce magnetic force.
4. according to claim 1,2 and 3 described pure magnetic motive force formula aircrafts, it is characterized in that: drive controlling mechanism (3) is made up of electromagnet (3-1), lead (3-2), touch switch (3-3) and bolt (3-4), touch switch (3-3) control electromagnet (3-1), electromagnet (3-1) master cock (2-3); Closing and open by mechanical transmission mechanism (1) of touch switch (3-3) controlled.
5. pure magnetic motive force formula aircraft according to claim 1, it is characterized in that: the driving engine (III) of pure magnetic motive force formula aircraft is made up of mechanical transmission mechanism (4), magnetically-actuated mechanism (5) and drive controlling mechanism (6), magnetically-actuated mechanism (5) produces power by magnet (5-1-1), control magnetically-actuated mechanism of drive controlling mechanism (6) (5) work, mechanical transmission mechanism (4) outwards transmits the power that produces by the certain movement rule.
6. according to claim 1 and 5 described pure magnetic motive force formula aircrafts, it is characterized in that: the magnet base part (5-1) of magnetically-actuated mechanism (5) is made up of magnet (5-1-1), shell (5-1-2), knob (5-1-3), cover clamp (5-1-4) and stove bolt (5-1-5); Magnet (5-1-1) is positioned in the shell (5-1-2), and whether magnet (5-1-1) outwards produces magnetic force is controlled by knob (5-1-3).
7. according to claim 1,5 and 6 described pure magnetic motive force formula aircrafts, it is characterized in that: partly (6-3) and electrical control part (6-4) are formed with joint efforts by power transfer part (6-1), contact switch part (6-2), electromagnetism in drive controlling mechanism (6).
8. according to claim 1,5,6 and 7 described pure magnetic motive force formula aircrafts, it is characterized in that: drive controlling mechanism (6) makes a concerted effort to remove each part of electromagnet (6-3-1) in the part (6-3) by power transfer part (6-1), electromagnetism and mechanical control mechanism (7) forms, and they finish the control to magnetically-actuated mechanism (5) jointly.
9. according to claim 1,2,3 and 4 described pure magnetic motive force formula aircrafts, it is characterized in that: mechanical transmission mechanism (1) adopts the four-bar linkage induced way, and the Slipper in its this mechanism is equipped with magnetically-actuated mechanism (2).
10. according to claim 1,5,6,7 and 8 described pure magnetic motive force formula aircrafts, it is characterized in that: mechanical transmission mechanism (4) adopts the four-link mechanism induced way, and the Slipper of its this mechanism is equipped with magnetically-actuated mechanism (2).
11. according to claim 1,2,3,4,5,6,7 and 8 described pure magnetic motive force formula aircrafts, it is characterized in that: the link rod in mechanical transmission mechanism (1) and the mechanical transmission mechanism (4) partly is equipped with magnetically-actuated mechanism (5).
12. according to claim 1,2,3,4,9,10 and 11 described pure magnetic motive force formula aircrafts, it is characterized in that: magnetically-actuated mechanism (2) is moving linearly in cabinet (1-1).
13., it is characterized in that: magnet base part (5-1) moving linearly in casing assembly (4-1) according to claim 1,5,6,7,8,9,10 and 11 described pure magnetic motive force formula aircrafts.
14. according to claim 1,2,3,4,9,10,11 and 12 described pure magnetic motive force formula aircrafts, it is characterized in that: the motion of main shaft (1-2-1) is for rotating.
15. according to claim 1,5,6,7,8,9,10,11 and 13 described pure magnetic motive force formula aircrafts, it is characterized in that: the motion of main shaft (4-2-1) is for rotating.
16. according to claim 1,5,6,7,8,9,10,11,13 and 15 described pure magnetic motive force formula aircrafts, it is characterized in that: contact switch Kab is made up of touch panel (6-1-7) and contact block (6-2-3), touch panel (6-1-7) is positioned on the sleeve (6-1-5), and sleeve (6-1-5) is positioned on the transmission shaft (6-1-2) by positioning screw (6-1-6); Contact block (6-2-3) is stuck on the feeler lever (6-2-1), and is after feeler lever (6-1-2) passes spring (6-2-2) and casing (4-1-1), fixing by stem nut (6-2-4) and spring cotter (6-2-5).
17. according to claim 1,5,6,7,8,9,10,11,12,14,15 and 16 described pure magnetic motive force formula aircrafts, it is characterized in that: the knob (5-1-3) in control magnet base part (5-1) magnetic field is controlled by mechanism controls mechanism (7).
18. according to claim 1,5,6,7,8,9,10,11,12,14,16 and 17 described pure magnetic motive force formula aircrafts, it is characterized in that: the knob (5-1-3) in control magnet base part (5-1) magnetic field is by dwang part (10) control.
19. according to claim 1,5,6,7,8,9,10,11,12,14,16,17 and 18 described pure magnetic motive force formula aircrafts, it is characterized in that: in driving engine (III) operational process, when two magnet bases parts (5-1) attracted each other and be close, cushion rubber (5-2-3) and cushion rubber (5-2-3) were in contact with one another.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810031581XA CN102152852A (en) | 2008-06-26 | 2008-06-26 | Purely magnetomotive airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810031581XA CN102152852A (en) | 2008-06-26 | 2008-06-26 | Purely magnetomotive airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102152852A true CN102152852A (en) | 2011-08-17 |
Family
ID=44434607
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200810031581XA Pending CN102152852A (en) | 2008-06-26 | 2008-06-26 | Purely magnetomotive airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102152852A (en) |
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2008
- 2008-06-26 CN CN200810031581XA patent/CN102152852A/en active Pending
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Open date: 20110817 |