CN103759586A - Multi-pointer controller for controlling time and direction of curve flight - Google Patents
Multi-pointer controller for controlling time and direction of curve flight Download PDFInfo
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- CN103759586A CN103759586A CN201310696350.1A CN201310696350A CN103759586A CN 103759586 A CN103759586 A CN 103759586A CN 201310696350 A CN201310696350 A CN 201310696350A CN 103759586 A CN103759586 A CN 103759586A
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Abstract
The invention relates to a multi-pointer controller for controlling the time and the direction of curve flight. The controller comprises a B shaft gear system which is provided with spiral spring strips to be used as the rotating power, a C shaft gear system and a D shaft gear system which are respectively provided with three transmission gears, a E shaft gear system and an F shaft gear system which are respectively provided with two transmission gears, and a pointer system which is provided with five concentric center shafts sheathed together, wherein one end of each center shaft is provided with a transmission gear, and the other end of each center shaft is provided with a heavy pointer. The controller is characterized in that rotary spiral spring rotating discs of the B shaft gear system enable the spiral spring strips to tightly rotate around B shafts, thereby forming the restoring force of the spiral spring strips, i.e. the power to drive the spiral spring rotating discs; the tighter the spiral spring strips rotate, the bigger the restoring force of the spiral spring strips is; the faster the rotating speed of the spiral spring rotating discs in an anti-clockwise direction is, the less the time for rotating one circle for the spiral spring rotating discs; a timing control rotating disc is limited by a limit rod of the timing control rotating disc to only rotate one circle with 360 degrees.
Description
Technical field
The present invention relates to the many pointers controller for controlling curved flight time and direction, be applicable to comprise the curved flight of all aircraft and the automatic control of reset, belong to science and technology of aviation field.
Background technology
In the U.S. and Russian epoch of dominating guided missile lead in the development of science and technology, China fails to contend with it always can do curved flight and avoid the guided missile of anti-ballistic attack, report Russia develops a kind of curved flight guided missile that does not have anti-missile system to attack recently, but their this control curved flight principle is mainly by navigation, and modern war tends to occur unpredictable situation, such as once war starts, satellite system is destroyed by enemy and is lost self-navigation function, or by Navigation Control, can by enemy's utmost point, early be found and be attacked by anti-missile system always, in addition another deadly defect of Navigation Control be exactly they be all by light current controlling run, this light current very easily by enemy's strong electromagnetic destroy and ineffective, preferably there is one can not need navigation and light current to control, and can automatically control the device of not followed the tracks of by electric wave or not destroyed by enemy's strong electromagnetic by enemy of its curved flight, can be unlikely being just blocked at MISSILE LAUNCHING initial stage and mid-term, as everybody knows, from being transmitted into, to lock target of attack actual be exactly a parabola to guided missile, that is to say the line of two points that are launch point and impact point, if there is no anti-missile interception, guided missile just does not need to have done curvilinear motion, but in order to avoid anti-missile interception, must make guided missile do random curve, do such curve easy, when how to make guided missile do curve, can also make guided missile reset and get back on original predetermined some point line track striking target, this is only the most key, the invention " 201310230221.3 clock and watch revolve pin ten thousand varied curve flight self-return direction controllers " of Wei Baiqing has solved a difficult problem for curved flight reset, another invention " 201310458435.6 clock and watch revolve the rotational automatic return direction of pin forceful electric power power-assisted controller " of Wei Baiqing has solved a difficult problem for forceful electric power conversion power
The present invention is the difficult problem while solving machinery control speed control, and forms a set of complete curved flight of mechanical heavy-current control guided missile and resetting systems with above two inventions.
Summary of the invention
The object of this invention is to provide a kind of do not need light current control by heavy pointer one-period time of No. 1, machinery control and other heavy pointer different rotation rates for controlling many pointers controller of curved flight time and direction.
For controlling many pointers controller of curved flight time and direction, comprise that one is set with the B shaft gear system of helical spring sheet as rotary power, two covers are respectively equipped with C shaft gear system and the D shaft gear system of three travelling gear, two covers are respectively equipped with E shaft gear system and the F shaft gear system of two travelling gears, and one is set with that five concentric central shafts are nested together mutually and a travelling gear other end is equipped with and is equipped with the index system of a heavy pointer in each central shaft one end; It is characterized in that:
1, the B shaft gear system of helical spring sheet as rotary power is housed, helical spring sheet one end is arranged on B axle, the other end is arranged on the inwall with the helical spring rotating disk of B axle concentric, rotating screw spring rotating disk makes helical spring sheet screw around B axle, thereby even if produce the power of the restoring force helical spring turntable rotation of helical spring sheet, the outside of helical spring rotating disk is provided with the outer elastic claw of multiple uniform helical spring rotating disks with making leaf spring, the outer elastic claw of helical spring rotating disk outside is provided with a timing controlled rotating disk, timing controlled rotating disk inner side is provided with multiple uniform little internal tooths of timing controlled rotating disk, timing controlled rotating disk outside is provided with a timing controlled rotary disk limitation bar, near the stage casing of timing controlled rotary disk limitation bar, there are two location conductive poles, location conductive pole is not connected with timing controlled rotary disk limitation bar, timing controlled rotary disk limitation bar leans against two location during conductive pole, location conductive pole is to the low-angle that tilts away from timing controlled rotary disk limitation bar direction, make the center line of timing controlled rotary disk limitation bar be stuck in 0 ° of position of dial disc, when timing controlled rotary disk limitation bar turns clockwise 360 ° time, location conductive pole is to the low-angle that tilts away from timing controlled rotary disk limitation bar direction, the center line of timing controlled rotary disk limitation bar is still stuck in 0 ° of position of dial disc, thereby guarantee that timing controlled rotary disk limitation bar does while counterclockwise rotating under the effect of helical spring sheet restoring force, can do 360 ° of complete rotations, the effect of location conductive pole has two: the one, and restriction timing controlled rotating disk maximum can only be done the rotation in a week of 360 °, the 2nd, when location conductive pole can and lean against on two location conductive poles at timing controlled turntable rotation, the timing controlled rotary disk limitation bar of conduction is communicated with two location conductive pole conductions, be that timing controlled rotary disk limitation bar is when conductive pole is located in two of contacts, just equal a firing switch, the upside of helical spring rotating disk is provided with a criss-cross helical spring rotating disk cross and connects pawl, there is a helical spring turntable rotation handle in the upside central authorities that helical spring rotating disk cross connects pawl, and this helical spring turntable rotation handle that turns clockwise just can drive helical spring turntable rotation and drive helical spring sheet to screw around B axle, when the helical spring rotating disk that turns clockwise contacts the outer elastic claw of the little internal tooth of timing controlled rotating disk and helical spring rotating disk, the outer elastic claw of the little internal tooth compressing of timing controlled rotating disk helical spring rotating disk, making leaf spring between the outer elastic claw of helical spring rotating disk and helical spring rotating disk is pressed, thereby helical spring rotating disk is turned clockwise in timing controlled rotating disk and screw the helical spring sheet in helical spring rotating disk, when helical spring sheet is tightened onto to a certain degree, unclamp helical spring turntable rotation handle, the effect of helical spring sheet restoring force drives helical spring rotating disk to do counterclockwise rotation, and snap on the little internal tooth of timing controlled rotating disk because of the outer elastic claw of helical spring rotating disk, thereby drive timing controlled turntable rotation, when the timing controlled rotary disk limitation bar rotation of timing controlled rotating disk is touched while coming to two location conductive poles, timing controlled rotating disk stops the rotation, now timing controlled rotating disk is just rotated counterclockwise one week 360 °, when helical spring sheet is tightened onto in various degree, the restoring force of helical spring sheet is also different, the speed that helical spring rotating disk does counterclockwise rotation is also different, helical spring sheet screws tightlyer, the restoring force of helical spring sheet is larger, it is also just faster that helical spring rotating disk does the speed of counterclockwise rotation, and the helical spring turntable rotation cycle of one week is also just less, helical spring sheet screws more loosely, and the restoring force of helical spring sheet is less, and it is also just slower that helical spring rotating disk does the speed of counterclockwise rotation, and the helical spring turntable rotation cycle of one week is also just larger, for the flight curvilinear path that makes guided missile does not duplicate, the curve of General Requirements missile flight arrives the location point of reentrying in helical spring turntable rotation one-period, the upside of timing controlled rotating disk has a timing controlled rotating disk locking key, this timing controlled rotating disk locking key is by ground artificial control or carry out setup control in advance, make guided missile after locking timing controlled rotating disk locking key, guided missile system is in the automatic control without light current duty, thereby make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, without light current work, and then make enemy cannot utilize electromagnetic wave tracking to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when timing controlled turntable rotation touches while coming to two location conductive poles to timing controlled rotary disk limitation bar rotation, this touches by being communicated with two location conductive poles, at this moment the light-current system of guided missile is reset work, guided missile enters the position of reentrying, guided missile positions precision strike to target within the extremely short time, enemy has not just had the time of interception guided missile like this, each helical spring sheet is rotated to different elasticities, the angle and the helical spring turntable rotation period T of a week that are helical spring turntable rotation rotatable handle are done calibration curve, in order to calculating guided missile after the extra-atmospheric flight time in wartime, just can, by helical spring turntable rotation rotatable handle to corresponding angle, determine that guided missile is a helical spring turntable rotation period T in the time of extra-atmospheric flight.
2, the B1 gear of B axle rotarily drives No. 1 heavy pointer driven gear A1 rotation on No. 1 heavy pointer shaft that is contained in being engaged with, by No. 1 heavy pointer shaft, rotarily drive No. 1 heavy pointer rotation of No. 1 heavy pointer shaft other end, the time cycle that No. 1 heavy pointer rotates a circle is T1; The period of time T 1 that No. 1 heavy pointer rotates a circle equals the helical spring turntable rotation period T of a week;
The B2 gear of B axle rotarily drives the C2 gear rotation on C axle that is contained in being engaged with, C2 gear rotarily drives the rotation of C axle, C axle rotarily drives the C1 gear rotation on C axle, C1 gear rotarily drives No. 2 heavy pointer driven gear A2 rotation on No. 2 heavy pointer shafts that is contained in being engaged with, by No. 2 heavy pointer shafts, rotarily drive No. 2 heavy pointers rotations of No. 2 heavy pointer shaft other ends, the time cycle that No. 2 heavy pointers rotate a circle is T2;
The B3 gear of B axle rotarily drives the D2 gear rotation on D axle that is contained in being engaged with, D2 gear rotarily drives the rotation of D axle, D axle rotarily drives the D1 gear rotation on D axle, D1 gear rotarily drives No. 4 heavy pointer driven gear A4 rotation on No. 4 heavy pointer shafts that is contained in being engaged with, by No. 4 heavy pointer shafts, rotarily drive No. 4 heavy pointers rotations of No. 4 heavy pointer shaft other ends, the time cycle that No. 4 heavy pointers rotate a circle is T4;
The B2 gear of B axle rotarily drives the C2 gear rotation on C axle that is contained in being engaged with, C2 gear rotarily drives the rotation of C axle, C axle rotarily drives the C3 gear rotation on C axle, C3 gear rotarily drives the E2 gear rotation on E axle that is contained in being engaged with, E2 gear rotarily drives E axle and rotates and drive the E1 gear on E axle to rotate, E1 gear rotarily drives No. 3 heavy pointer driven gear A3 rotation on No. 3 heavy pointer shafts that is contained in being engaged with, by No. 3 heavy pointer shafts, rotarily drive No. 3 heavy pointers rotations of No. 3 heavy pointer shaft other ends, the time cycle that No. 3 heavily pointer rotates a circle is T3,
The B3 gear of B axle rotarily drives the D2 gear rotation on D axle that is contained in being engaged with, D2 gear rotarily drives the rotation of D axle, D axle rotarily drives the D3 gear rotation on D axle, D3 gear rotarily drives the F2 gear rotation on F axle that is contained in being engaged with, F2 gear rotarily drives F axle and rotates and drive the F1 gear on F axle to rotate, F1 gear rotarily drives No. 5 heavy pointer driven gear A5 rotation on No. 5 heavy pointer shafts that is contained in being engaged with, by No. 5 heavy pointer shafts, rotarily drive No. 5 heavy pointers rotations of No. 5 heavy pointer shaft other ends, the time cycle that No. 5 heavily pointer rotates a circle is T5.
3, the period of time T period of time T that 1 and No. 2 heavy pointer the rotates a circle period of time T that 2, No. 3 heavy pointer the rotates a circle period of time T that 3, No. 4 heavy pointer the rotates a circle period of time T 5 that 4, No. 5 heavy pointer rotates a circle that No. 1 heavy pointer rotates a circle has following relation: T1=N2 × T2=N3 × T3=N4 × T4=N5 × T5, wherein: N2, N3, N4, N5 be natural number 2,3,4,5,6,, and 1<N2<N3<N4LEssT.L TssT.LTN5; Under the constant condition of T1, design different T2, T3, T4, T5, make guided missile form different curved flights, allow enemy cannot find our guided missile to do the rule of curve motion, thereby cannot calculate interception.
4, location conductive pole is comprised of a joint fixed leg below and a joint activity post above, centre is connected with bulb mortar by a bulb, bulb does certain angle swinging in bulb mortar, approaching face between fixed leg and movable post is the conical surface, between two conical surfaces, there is the gap of 3mm ~ 10 mm, movable post just can be swung to when being subject to less power and be subject to force direction to become the little angle of 1 ° ~ 10 °, thereby timing controlled rotary disk limitation bar is rotated counterclockwise while touching movable post, or timing controlled rotary disk limitation bar turns clockwise while touching movable post, can make the central axis of timing controlled rotary disk limitation bar be parked in 0 ° of position of dial disc, its objective is and make the timing controlled rotary disk limitation bar of timing controlled driven by rotary disc under the effect of helical spring sheet restoring force, can do 360 ° of complete rotations, thereby can make guided missile finish after the curve of one-period, can be returned to and originally do on curve movement locus before.
The present invention compared with prior art has the following advantages:
1, the present invention can be by angle and the helical spring turntable rotation period T curve of a week of the helical spring turntable rotation rotatable handle demarcated in advance, the track time according to the target call guided missile of missile attack in exoatmosphere operation, regulate rapidly the angle of determining helical spring turntable rotation rotatable handle.
2, apparatus of the present invention arrange different T1, T2, T3, T4, T5 parameter, form random curvilinear motion, utilize machine power control guided missile to form multiple irregular curved flight, make guided missile can not send and accept any signal before entering atmosphere again, thereby be difficult for being followed the tracks of interception by enemy.
3, volume of the present invention is little, purposes is wide, cost is low, can symmetrically control flight curve.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention;
Fig. 2 be embodiment illustrated in fig. 1 in No. 1 heavy pointer transmission schematic diagram;
Fig. 3 be embodiment illustrated in fig. 1 in No. 2 heavy pointer transmission schematic diagrames;
Fig. 4 be embodiment illustrated in fig. 1 in No. 3 heavy pointer transmission schematic diagrames;
Fig. 5 be embodiment illustrated in fig. 1 in No. 4 heavy pointer transmission schematic diagrames;
Fig. 6 be embodiment illustrated in fig. 1 in No. 5 heavy pointer transmission schematic diagrames;
Fig. 7 is middle wind spring control time control speed power plate schematic diagram embodiment illustrated in fig. 1;
Fig. 8 is middle M-M generalized section embodiment illustrated in fig. 7;
Fig. 9 is middle N-N generalized section embodiment illustrated in fig. 7;
Figure 10 is middle P enlarged diagram embodiment illustrated in fig. 9;
Figure 11 is middle Q enlarged diagram embodiment illustrated in fig. 7.
In Fig. 1-11: 1, B3 gear 2, B1 gear 3, B2 gear 4, B axle 5, C1 gear 6, C axle 7, C2 gear 8, D axle 9, D3 gear 10, D1 gear 11, D2 gear 12, F1 gear 13, F2 gear 14, F axle 15, many pointers center sleeve 16, No. 5 heavy pointer driven gears 17, No. 4 heavy pointer driven gears 18, No. 3 heavy pointer driven gears 19, No. 2 heavy pointer driven gears 20, No. 1 heavy pointer driven gear 21, E axle 22, C3 gear 23, E2 gear 24, E1 gear 25, No. 5 heavy pointer shafts 26, No. 4 heavy pointer shafts 27, No. 3 heavy pointer shafts 28, No. 2 heavy pointer shafts 29, No. 1 heavy pointer shaft 30, No. 1 heavy pointer 31, No. 2 heavy pointers 32, No. 3 heavy pointers 33, No. 4 heavy pointers 34, No. 5 heavy pointers 35, dial disc 36, timing controlled rotating disk 37, the little internal tooth 38 of timing controlled rotating disk, helical spring rotating disk 39, the outer elastic claw 40 of helical spring rotating disk, helical spring sheet 41, circular dial scale 42, location conductive pole 43, timing controlled rotary disk limitation bar 44, helical spring rotating disk cross connects pawl 45, helical spring turntable rotation handle 46, movable post 47, bulb mortar 48, bulb 49, fixed leg 50, making leaf spring 51, making leaf spring stiff end 52, the outer elastic claw rotating shaft 53 of helical spring rotating disk, timing controlled rotating disk locking key.
The specific embodiment
In the embodiment shown in Fig. 1-11: for controlling many pointers controller of curved flight time and direction, comprise that one is set with B axle 4 gear trains of helical spring sheet 40 as rotary power, two covers are respectively equipped with C axle 6 gear trains and D axle 8 gear trains of three travelling gear, two covers are respectively equipped with E axle 21 gear trains and F axle 14 gear trains of two travelling gears, and one is set with that five concentric central shafts are nested together mutually and a travelling gear other end is equipped with and is equipped with the index system of a heavy pointer in each central shaft one end, it is characterized in that: B axle 4 gear trains of helical spring sheet 40 as rotary power are housed, helical spring sheet 40 one end are arranged on B axle 4, the other end is arranged on the inwall with the helical spring rotating disk 38 of B axle 4 concentrics, rotating screw spring rotating disk 38 makes helical spring sheet 40 screw around B axle 4, thereby even if produce the power that the restoring force helical spring rotating disk 38 of helical spring sheet 40 rotates, the outside of helical spring rotating disk 38 is provided with the outer elastic claw 39 of multiple uniform helical spring rotating disks with making leaf spring 50, the outer elastic claw of helical spring rotating disk 39 outsides are provided with a timing controlled rotating disk 36, timing controlled rotating disk 36 inner sides are provided with the little internal tooth 37 of multiple uniform timing controlled rotating disks, timing controlled rotating disk 36 outsides are provided with a timing controlled rotary disk limitation bar 43, near the stage casing of timing controlled rotary disk limitation bar 43, there are two location conductive poles 42, location conductive pole 42 is not connected with timing controlled rotary disk limitation bar 43, timing controlled rotary disk limitation bar 43 leans against two location during conductive pole 42, location conductive pole 42 is to the low-angle that tilts away from timing controlled rotary disk limitation bar 43 directions, make the center line of timing controlled rotary disk limitation bar 43 be stuck in 0 ° of position of dial disc 35, when timing controlled rotary disk limitation bar 43 turns clockwise 360 ° time, location conductive pole 42 is to the low-angle that tilts away from timing controlled rotary disk limitation bar 43 directions, the center line of timing controlled rotary disk limitation bar 43 is still stuck in 0 ° of position of dial disc 35, thereby guarantee that timing controlled rotary disk limitation bar 43 does while counterclockwise rotating under the effect of helical spring sheet 40 restoring forces, can do 360 ° of complete rotations, the effect of location conductive pole 42 has two: the one, and restriction timing controlled rotating disk 36 maximums can only be done the rotation in a week of 360 °, the 2nd, location conductive pole 42 can be when timing controlled rotating disk 36 rotates and lean against on two location conductive poles 42, the timing controlled rotary disk limitation bar 43 of conduction is communicated with two location conductive poles 42 and conducts electricity, be that timing controlled rotary disk limitation bar 43 is when conductive pole 42 is located in two of contacts, just equal a firing switch, the upside of helical spring rotating disk 38 is provided with a criss-cross helical spring rotating disk cross and connects pawl 44, there is a helical spring turntable rotation handle 45 in the upside central authorities that helical spring rotating disk cross connects pawl 44, and this helical spring turntable rotation handle 45 that turns clockwise just can drive helical spring rotating disk 38 to rotate and drive helical spring sheet 40 to screw around B axle 4, when the helical spring rotating disk 38 that turns clockwise contacts the outer elastic claw 39 of the little internal tooth 37 of timing controlled rotating disk and helical spring rotating disk, the little internal tooth 37 of timing controlled rotating disk is oppressed the outer elastic claw 39 of helical spring rotating disk, making leaf spring 50 between the outer elastic claw 39 of helical spring rotating disk and helical spring rotating disk 38 is pressed, thereby helical spring rotating disk 38 is turned clockwise in timing controlled rotating disk 36 and screw the helical spring sheet 40 in helical spring rotating disk 38, when helical spring sheet 40 is tightened onto to a certain degree, unclamp helical spring turntable rotation handle 45, the 40 restoring force effects of helical spring sheet drive helical spring rotating disk 38 to do counterclockwise rotation, and snap on the little internal tooth 37 of timing controlled rotating disk because of the outer elastic claw 39 of helical spring rotating disk, thereby drive timing controlled rotating disk 36 to rotate, when timing controlled rotary disk limitation bar 43 rotation of timing controlled rotating disk 36 is touched while coming to two location conductive poles 42, timing controlled rotating disk 36 stops the rotation, now timing controlled rotating disk 36 is just rotated counterclockwise one week 360 °, when helical spring sheet 40 is tightened onto in various degree, the restoring force of helical spring sheet 40 is also different, the speed that helical spring rotating disk 38 does counterclockwise rotation is also different, helical spring sheet 40 screws tightlyer, the restoring force of helical spring sheet 40 is larger, it is also just faster that helical spring rotating disk 38 does the speed of counterclockwise rotation, and the cycle that helical spring rotating disk 38 rotates a circle is also just less, helical spring sheet 40 screws more loosely, and the restoring force of helical spring sheet 40 is less, and it is also just slower that helical spring rotating disk 38 does the speed of counterclockwise rotation, and the cycle that helical spring rotating disk 38 rotates a circle is also just larger, for the flight curvilinear path that makes guided missile does not duplicate, the curve of General Requirements missile flight rotates at helical spring rotating disk 38 location point that in one-period, arrival is reentried, the upside of timing controlled rotating disk 36 has a timing controlled rotating disk locking key 53, this timing controlled rotating disk locking key 53 is by ground artificial control or carry out setup control in advance, make guided missile after locking timing controlled rotating disk locking key 53, guided missile system is in the automatic control without light current duty, thereby make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, without light current work, and then make enemy cannot utilize electromagnetic wave tracking to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when rotating to timing controlled rotary disk limitation bar 43 rotation, touches while coming to two location conductive poles 42 by timing controlled rotating disk 36, this touches by being communicated with two location conductive poles 42, at this moment the light-current system of guided missile is reset work, guided missile enters the position of reentrying, guided missile positions precision strike to target within the extremely short time, enemy has not just had the time of interception guided missile like this, each helical spring sheet 40 is rotated to different elasticities, be that the period T that helical spring turntable rotation handle 45 angle of rotating and helical spring rotating disk 38 rotate a circle is done calibration curve, in order to calculating guided missile after the extra-atmospheric flight time in wartime, just helical spring turntable rotation handle 45 can be rotated to corresponding angle, determine that guided missile is a helical spring rotating disk 38 swing circle T in the time of extra-atmospheric flight.
The B1 gear 2 of B axle 4 rotarily drives No. 1 heavy pointer driven gear 20A1 rotation on No. 1 heavy pointer shaft 29 that is contained in being engaged with, No. 1 heavy pointer 30 that rotarily drives No. 1 heavy pointer shaft 29 other ends by No. 1 heavy pointer shaft 29 rotates, and the time cycle that No. 1 heavy pointer 30 rotates a circle is T1; The period of time T 1 that No. 1 heavy pointer 30 rotates a circle equals the period T that helical spring rotating disk 38 rotates a circle;
The B2 gear 3 of B axle 4 rotarily drives the C2 gear 7 being contained on C axle 6 being engaged with and rotates, C2 gear 7 rotarily drives C axle 6 and rotates, the C1 gear 5 that C axle 6 rotarily drives on C axle 6 rotates, C1 gear 5 rotarily drives No. 2 heavy pointer driven gear 19A2 rotation on No. 2 heavy pointer shafts 28 that is contained in being engaged with, No. 2 heavy pointers 31 that rotarily drive No. 2 heavy pointer shaft 28 other ends by No. 2 heavy pointer shafts 28 rotate, and the time cycle that No. 2 heavy pointers 31 rotate a circle is T2;
The B3 gear 1 of B axle 4 rotarily drives the D2 gear 11 being contained on D axle 8 being engaged with and rotates, D2 gear 11 rotarily drives D axle 8 and rotates, the D1 gear 10 that D axle 8 rotarily drives on D axle 8 rotates, D1 gear 10 rotarily drives No. 4 heavy pointer driven gear 17A4 rotation on No. 4 heavy pointer shafts 26 that is contained in being engaged with, No. 4 heavy pointers 33 that rotarily drive No. 4 heavy pointer shaft 26 other ends by No. 4 heavy pointer shafts 26 rotate, and the time cycle that No. 4 heavy pointers 33 rotate a circle is T4;
The B2 gear 3 of B axle 4 rotarily drives the C2 gear 7 being contained on C axle 6 being engaged with and rotates, C2 gear 7 rotarily drives C axle 6 and rotates, the C3 gear 22 that C axle 6 rotarily drives on C axle 6 rotates, C3 gear 22 rotarily drives the E2 gear 23 being contained on E axle 21 being engaged with and rotates, E2 gear 23 rotarily drives E axle 21 and rotates and drive the E1 gear 24 on E axle 21 to rotate, E1 gear 24 rotarily drives No. 3 heavy pointer driven gear 18A3 rotation on No. 3 heavy pointer shafts 27 that is contained in being engaged with, No. 3 heavy pointers 32 that rotarily drive No. 3 heavy pointer shaft 27 other ends by No. 3 heavy pointer shafts 27 rotate, the time cycle that No. 3 heavy pointers 32 rotate a circle is T3,
The B3 gear 1 of B axle 4 rotarily drives the D2 gear 11 being contained on D axle 8 being engaged with and rotates, D2 gear 11 rotarily drives D axle 8 and rotates, the D3 gear 9 that D axle 8 rotarily drives on D axle 8 rotates, D3 gear 9 rotarily drives the F2 gear 13 being contained on F axle 14 being engaged with and rotates, F2 gear 13 rotarily drives F axle 14 and rotates and drive the F1 gear 12 on F axle 14 to rotate, F1 gear 12 rotarily drives No. 5 heavy pointer driven gear 16A5 rotation on No. 5 heavy pointer shafts 25 that is contained in being engaged with, No. 5 heavy pointers 34 that rotarily drive No. 5 heavy pointer shaft 25 other ends by No. 5 heavy pointer shafts 25 rotate, the time cycle that No. 5 heavy pointers 34 rotate a circle is T5.
The period of time T 5 that 4, No. 5 heavy pointers 34 of period of time T that 3, No. 4 heavy pointers 33 of period of time T that 2, No. 3 heavy pointers 32 of period of time T that 1 and No. 2 heavy pointers 31 of period of time T that No. 1 heavy pointer 30 rotates a circle rotate a circle rotate a circle rotate a circle rotate a circle has following relation: T1=N2 × T2=N3 × T3=N4 × T4=N5 × T5, wherein: N2, N3, N4, N5 be natural number 2,3,4,5,6,, and 1<N2<N3<N4LEssT.L TssT.LTN5; Under the constant condition of T1, design different T2, T3, T4, T5, make guided missile form different curved flights, allow enemy cannot find our guided missile to do the rule of curve motion, thereby cannot calculate interception.
Location conductive pole 42 is comprised of a joint fixed leg 49 below and a joint activity post 46 above, centre is connected with bulb mortar 47 by a bulb 48, bulb 48 does certain angle swinging in bulb mortar 47, approaching face between fixed leg 49 and movable post 46 is the conical surface, between two conical surfaces, there is the gap of 3mm ~ 10 mm, movable post 46 just can be swung to when being subject to less power and be subject to force direction to become the little angle of 1 ° ~ 10 °, thereby timing controlled rotary disk limitation bar 43 is rotated counterclockwise while touching movable post 46, or timing controlled rotary disk limitation bar 43 turns clockwise while touching movable post 46, can make the central axis of timing controlled rotary disk limitation bar 43 be parked in 0 ° of position of dial disc 35, its objective is and make timing controlled rotary disk limitation bar 43 that timing controlled rotating disk 36 drives under the 40 restoring force effects of helical spring sheet, can do 360 ° of complete rotations, thereby can make guided missile finish after the curve of one-period, can be returned to and originally do on curve movement locus before.
Claims (3)
1. for controlling many pointers controller of curved flight time and direction, comprise that one is set with B axle (4) gear train of helical spring sheet (40) as rotary power, two covers are respectively equipped with C axle (6) gear train and D axle (8) gear train of three travelling gear, two covers are respectively equipped with E axle (21) gear train and F axle (14) gear train of two travelling gears, and one is set with that five concentric central shafts are nested together mutually and a travelling gear other end is equipped with and is equipped with the index system of a heavy pointer in each central shaft one end, it is characterized in that: B axle (4) gear train of helical spring sheet (40) as rotary power is housed, helical spring sheet (40) one end is arranged on B axle (4), the other end is arranged on the inwall with the helical spring rotating disk (38) of B axle (4) concentric, rotating screw spring rotating disk (38) makes helical spring sheet (40) screw around B axle (4), thus produce helical spring sheet (40) even the power of restoring force helical spring rotating disk (38) rotation, the outside of helical spring rotating disk (38) is provided with the outer elastic claw (39) of helical spring rotating disk of multiple uniform band making leaf springs (50), the outer elastic claw (39) of helical spring rotating disk outside is provided with a timing controlled rotating disk (36), timing controlled rotating disk (36) inner side is provided with multiple uniform little internal tooths of timing controlled rotating disk (37), timing controlled rotating disk (36) outside is provided with a timing controlled rotary disk limitation bar (43), near the stage casing of timing controlled rotary disk limitation bar (43), there are two location conductive poles (42), location conductive pole (42) is not connected with timing controlled rotary disk limitation bar (43), when timing controlled rotary disk limitation bar (43) leans against two location conductive poles (42), location conductive pole (42) is to the low-angle that tilts away from timing controlled rotary disk limitation bar (43) direction, make the center line of timing controlled rotary disk limitation bar (43) be stuck in 0 ° of position of dial disc (35), when timing controlled rotary disk limitation bar (43) turns clockwise 360 ° time, location conductive pole (42) is to the low-angle that tilts away from timing controlled rotary disk limitation bar (43) direction, the center line of timing controlled rotary disk limitation bar (43) is still stuck in 0 ° of position of dial disc (35), thereby guarantee that timing controlled rotary disk limitation bar (43) does while counterclockwise rotating under the effect of helical spring sheet (40) restoring force, can do 360 ° of complete rotations, the effect of location conductive pole (42) has two: the one, and restriction timing controlled rotating disk (36) maximum can only be done the rotation in a week of 360 °, the 2nd, location conductive pole (42) can be when timing controlled rotating disk (36) rotate and lean against on two location conductive poles (42), the timing controlled rotary disk limitation bar (43) of conduction is communicated with two location conductive poles (42) conduction, be that timing controlled rotary disk limitation bar (43) is when two location conductive poles of contact (42), just equal a firing switch, the upside of helical spring rotating disk (38) is provided with a criss-cross helical spring rotating disk cross and connects pawl (44), there is a helical spring turntable rotation handle (45) in the upside central authorities that helical spring rotating disk cross connects pawl (44), and this helical spring turntable rotation handle (45) that turns clockwise just can drive helical spring rotating disk (38) to rotate and drive helical spring sheet (40) to screw around B axle (4), when the helical spring rotating disk (38) that turns clockwise contacts the outer elastic claw (39) of the little internal tooth of timing controlled rotating disk (37) and helical spring rotating disk, the outer elastic claw (39) of the little internal tooth of timing controlled rotating disk (37) compressing helical spring rotating disk, making leaf spring (50) between the outer elastic claw (39) of helical spring rotating disk and helical spring rotating disk (38) is pressed, thereby helical spring rotating disk (38) is turned clockwise in timing controlled rotating disk (36) and screw the helical spring sheet (40) in helical spring rotating disk (38), when helical spring sheet (40) is tightened onto to a certain degree, unclamp helical spring turntable rotation handle (45), helical spring sheet (40) restoring force effect drives helical spring rotating disk (38) to do counterclockwise rotation, and snap on the little internal tooth of timing controlled rotating disk (37) because of the outer elastic claw (39) of helical spring rotating disk, thereby drive timing controlled rotating disk (36) rotation, when timing controlled rotary disk limitation bar (43) rotation of timing controlled rotating disk (36) is touched while coming to two location conductive poles (42), timing controlled rotating disk (36) stops the rotation, now timing controlled rotating disk (36) is just rotated counterclockwise one week 360 °, when helical spring sheet (40) is tightened onto in various degree, the restoring force of helical spring sheet (40) is also different, the speed that helical spring rotating disk (38) does counterclockwise rotation is also different, helical spring sheet (40) screws tightlyer, the restoring force of helical spring sheet (40) is larger, it is also just faster that helical spring rotating disk (38) does the speed of counterclockwise rotation, and the cycle that helical spring rotating disk (38) rotates a circle is also just less, helical spring sheet (40) screws more loosely, and the restoring force of helical spring sheet (40) is less, and it is also just slower that helical spring rotating disk (38) does the speed of counterclockwise rotation, and the cycle that helical spring rotating disk (38) rotates a circle is also just larger, for the flight curvilinear path that makes guided missile does not duplicate, the curve of General Requirements missile flight arrives the location point of reentrying in helical spring rotating disk (38) rotation one-period, the upside of timing controlled rotating disk (36) has a timing controlled rotating disk locking key (53), this timing controlled rotating disk locking key (53) is by ground artificial control or carry out setup control in advance, make guided missile after locking timing controlled rotating disk locking key (53), guided missile system is in the automatic control without light current duty, thereby make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, without light current work, and then make enemy cannot utilize electromagnetic wave tracking to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when rotating to timing controlled rotary disk limitation bar (43) rotation, touches while coming to two location conductive poles (42) by timing controlled rotating disk (36), this touches by being communicated with two location conductive poles (42), at this moment the light-current system of guided missile is reset work, guided missile enters the position of reentrying, guided missile positions precision strike to target within the extremely short time, enemy has not just had the time of interception guided missile like this, each helical spring sheet (40) is rotated to different elasticities, be that the angle of helical spring turntable rotation handle (45) rotation and period T that helical spring rotating disk (38) rotates a circle are done calibration curve, in order to calculating guided missile after the extra-atmospheric flight time in wartime, just helical spring turntable rotation handle (45) can be rotated to corresponding angle, determine that guided missile is a helical spring rotating disk (38) swing circle T in the time of extra-atmospheric flight,
The B1 gear (2) of B axle (4) rotarily drives No. 1 heavy pointer driven gear (20) the A1 rotation on No. 1 heavy pointer shaft (29) that is contained in being engaged with, by No. 1 heavy pointer shaft (29), rotarily drive No. 1 heavy pointer (30) rotation of No. 1 heavy pointer shaft (29) other end, the time cycle that No. 1 heavy pointer (30) rotates a circle is T1; The period of time T 1 that No. 1 heavy pointer (30) rotates a circle equals the period T that helical spring rotating disk (38) rotates a circle;
The B2 gear (3) of B axle (4) rotarily drives C2 gear (7) rotation on C axle (6) that is contained in being engaged with, C2 gear (7) rotarily drives C axle (6) rotation, C axle (6) rotarily drives C1 gear (5) rotation on C axle (6), C1 gear (5) rotarily drives No. 2 heavy pointer driven gear (19) the A2 rotations on No. 2 heavy pointer shafts (28) that are contained in that are engaged with, by No. 2 heavy pointer shafts (28), rotarily drive No. 2 heavy pointers (31) rotation of No. 2 heavy pointer shaft (28) other ends, the time cycle that No. 2 heavy pointers (31) rotate a circle is T2,
The B3 gear (1) of B axle (4) rotarily drives D2 gear (11) rotation on D axle (8) that is contained in being engaged with, D2 gear (11) rotarily drives D axle (8) rotation, D axle (8) rotarily drives D1 gear (10) rotation on D axle (8), D1 gear (10) rotarily drives No. 4 heavy pointer driven gear (17) the A4 rotations on No. 4 heavy pointer shafts (26) that are contained in that are engaged with, by No. 4 heavy pointer shafts (26), rotarily drive No. 4 heavy pointers (33) rotation of No. 4 heavy pointer shaft (26) other ends, the time cycle that No. 4 heavy pointers (33) rotate a circle is T4,
The B2 gear (3) of B axle (4) rotarily drives C2 gear (7) rotation on C axle (6) that is contained in being engaged with, C2 gear (7) rotarily drives C axle (6) rotation, C axle (6) rotarily drives C3 gear (22) rotation on C axle (6), C3 gear (22) rotarily drives E2 gear (23) rotation on E axle (21) that is contained in being engaged with, E2 gear (23) rotarily drives E axle (21) and rotates and drive the E1 gear (24) on E axle (21) to rotate, E1 gear (24) rotarily drives No. 3 heavy pointer driven gear (18) the A3 rotations on No. 3 heavy pointer shafts (27) that are contained in that are engaged with, by No. 3 heavy pointer shafts (27), rotarily drive No. 3 heavy pointers (32) rotation of No. 3 heavy pointer shaft (27) other ends, the time cycle that No. 3 heavy pointers (32) rotate a circle is T3,
The B3 gear (1) of B axle (4) rotarily drives D2 gear (11) rotation on D axle (8) that is contained in being engaged with, D2 gear (11) rotarily drives D axle (8) rotation, D axle (8) rotarily drives D3 gear (9) rotation on D axle (8), D3 gear (9) rotarily drives F2 gear (13) rotation on F axle (14) that is contained in being engaged with, F2 gear (13) rotarily drives F axle (14) and rotates and drive the F1 gear (12) on F axle (14) to rotate, F1 gear (12) rotarily drives No. 5 heavy pointer driven gear (16) the A5 rotations on No. 5 heavy pointer shafts (25) that are contained in that are engaged with, by No. 5 heavy pointer shafts (25), rotarily drive No. 5 heavy pointers (34) rotation of No. 5 heavy pointer shaft (25) other ends, the time cycle that No. 5 heavy pointers (34) rotate a circle is T5.
2. as claimed in claim 1 for controlling many pointers controller of curved flight time and direction, it is characterized in that: the period of time T 2 that 1 and No. 2 heavy pointers of period of time T (31) that No. 1 heavy pointer (30) rotates a circle rotate a circle, the period of time T 3 that No. 3 heavy pointers (32) rotate a circle, the period of time T 4 that No. 4 heavy pointers (33) rotate a circle, the period of time T 5 that No. 5 heavy pointers (34) rotate a circle has following relation: T1=N2 × T2=N3 × T3=N4 × T4=N5 × T5, wherein: N2, N3, N4, N5 is natural number 2, 3, 4, 5, 6, and 1<N2<N3<N4LEssT.L TssT.LTN5, under the constant condition of T1, design different T2, T3, T4, T5, make guided missile form different curved flights, allow enemy cannot find our guided missile to do the rule of curve motion, thereby cannot calculate interception.
3. as claimed in claim 1 for controlling many pointers controller of curved flight time and direction, it is characterized in that: location conductive pole (42) is comprised of a joint fixed leg (49) below and a joint activity post (46) above, centre is connected with bulb mortar (47) by a bulb (48), bulb (48) does certain angle swinging in bulb mortar (47), approaching face between fixed leg (49) and movable post (46) is the conical surface, between two conical surfaces, there is the gap of 3mm ~ 10 mm, movable post (46) just can be swung to when being subject to less power and be subject to force direction to become the little angle of 1 ° ~ 10 °, thereby timing controlled rotary disk limitation bar (43) is rotated counterclockwise while touching movable post (46), or timing controlled rotary disk limitation bar (43) turns clockwise while touching movable post (46), can make the central axis of timing controlled rotary disk limitation bar (43) be parked in 0 ° of position of dial disc (35), its objective is and make the timing controlled rotary disk limitation bar (43) of timing controlled rotating disk (36) drive under helical spring sheet (40) restoring force effect, can do 360 ° of complete rotations, thereby can make guided missile finish after the curve of one-period, can be returned to and originally do on curve movement locus before.
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Cited By (1)
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| CN106628197A (en) * | 2016-12-02 | 2017-05-10 | 武汉航空仪表有限责任公司 | Speed and time control structure |
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| CN103759586B (en) | 2015-11-04 |
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Effective date of registration: 20181206 Address after: 401120 Jinxianglin 17 Building-1-2, 25 Kaige Second Branch Road, Huixing Street, Yubei District, Chongqing Patentee after: Chongqing Moyan Technology Co.,Ltd. Address before: 314408 304, room 2, 30 shallow water bay, Kashi street, Haining, Jiaxing, Zhejiang. Patentee before: Wei Boqing |
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Effective date of registration: 20201218 Address after: 224000 southeast Industrial Park, Yandong Town, Tinghu District, Yancheng City, Jiangsu Province (19) Patentee after: YANCHENG CITY RONGYILAI TEXTILE MACHINERY Co.,Ltd. Address before: 401120 Jinxianglin 17 Building-1-2, 25 Kaige Second Branch Road, Huixing Street, Yubei District, Chongqing Patentee before: Chongqing Moyan Technology Co.,Ltd. |
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