CN103759586B - For many pointers controller in controlling curve flight time and direction - Google Patents
For many pointers controller in controlling curve flight time and direction Download PDFInfo
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- CN103759586B CN103759586B CN201310696350.1A CN201310696350A CN103759586B CN 103759586 B CN103759586 B CN 103759586B CN 201310696350 A CN201310696350 A CN 201310696350A CN 103759586 B CN103759586 B CN 103759586B
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Abstract
For many pointers controller in controlling curve flight time and direction, comprise one and be 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 five concentric central shafts is nested together and the index system that a travelling gear other end is equipped with a heavy pointer is equipped with in each central shaft one end mutually; It is characterized in that: the rotating screw spring rotating disk of B shaft gear system makes helical spring sheet screw around B axle, even if thus produce the power of the restoring force helical spring turntable rotation of helical spring sheet; Helical spring sheet screws tighter, and the restoring force of helical spring sheet is larger, and it is also faster that helical spring rotating disk does the speed counterclockwise rotated, and the helical spring turntable rotation time of one week is also fewer; Timing controlled rotary disk limitation bar restriction timing controlled rotating disk can only do one 360 ° rotating for one week.
Description
Technical field
The present invention relates to the many pointers controller for controlling curve 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
The epoch of guided missile lead in the development of science and technology are dominated in the U.S. and Russia, what China failed to contend with it always can do curved flight to avoid the guided missile of anti-ballistic attack, nearest report Russia develops a kind of curved flight guided missile not having anti-missile system to attack, but their this controlling curve flight theory is mainly by navigation, and often there is unpredictable situation in modern war, such as once war starts, satellite system is destroyed by enemy and loses self-navigation function, or early can be found by enemy pole by Navigation Control always and be attacked by anti-missile system, another deadly defect of Navigation Control is exactly them is in addition all run by vulnerabilities scan, this light current is very easily ineffective by the strong electromagnetic of enemy destruction, preferably there is one that navigation and light current can not be needed to control, and automatically can control not followed the tracks of by electric wave by enemy or not by the device that enemy's strong electromagnetic is destroyed, being unlikely just being blocked at MISSILE LAUNCHING initial stage and mid-term of its curved flight, as everybody knows, from being transmitted into, to lock target of attack actual be exactly a parabola to guided missile, that is be the line of two points of launch point and impact point, if there is no anti-missile interception, guided missile does not just need to do curvilinear motion, but in order to avoid anti-missile interception, guided missile must be made to do random curve, do such curve easy, while how making guided missile do curve, guided missile can also be made to reset get back on the originally predetermined some point line track struck target, this is only the most key, the difficult problem that invention " 201310230221.3 clock and watch revolve pin ten thousand varied curve flight self-return direction controlling instrument " solves a difficult problem for curved flight reset, another invention " 201310458435.6 clock and watch revolve pin forceful electric power power-assisted rotational automatic return direction controlling instrument " of Wei Baiqing solves forceful electric power switching kinetics of Wei Baiqing, the present invention is difficult problem when solving machinery control speed control, and invents with above two the curved flight of mechanical heavy-current control guided missile and resetting system that form complete set.
Summary of the invention
The object of this invention is to provide a kind of do not need vulnerabilities scan by the many pointers controller for controlling curve flight time and direction of No. 1, Mechanical course heavy pointer one-period time and other heavy pointer different rotation rates.
For many pointers controller in controlling curve flight time and direction, comprise one and be 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 five concentric central shafts is nested together and the index system that a travelling gear other end is equipped with a heavy pointer is equipped with in each central shaft one end mutually; It is characterized in that:
1, the B shaft gear system of helical spring sheet as rotary power be 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, even if thus 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 helical spring rotating disk of multiple uniform band making leaf spring, outside the outer elastic claw of helical spring rotating disk, a timing controlled rotating disk is installed, multiple uniform timing controlled rotating disk little internal tooth is installed inside timing controlled rotating disk, a timing controlled rotary disk limitation bar is installed outside timing controlled rotating disk, two locating conductive posts are had near the stage casing of timing controlled rotary disk limitation bar, locating conductive post is not connected with timing controlled rotary disk limitation bar, when timing controlled rotary disk limitation bar leans against two locating conductive posts, locating conductive post 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 made to be stuck in 0 ° of position of dial disc, when timing controlled rotary disk limitation bar turn clockwise 360 ° time, locating conductive post 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, thus ensure that timing controlled rotary disk limitation bar does when counterclockwise rotating under the effect of helical spring sheet restoring force, 360 ° of complete rotations can be done, the effect of locating conductive post has two: one to be that maximum a week of can only do 360 ° of restriction timing controlled rotating disk rotates, two is that locating conductive post rotates to when leaning against on two locating conductive posts at timing controlled turntable rotation, the timing controlled rotary disk limitation bar now conducted electricity is communicated with two locating conductive post conductions, namely timing controlled rotary disk limitation bar is when contact two locating conductive posts, 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, the central upper that helical spring rotating disk cross connects pawl has a helical spring turntable rotation handle, 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 makes the outer elastic claw of the little internal tooth of timing controlled rotating disk and helical spring rotating disk contact, the outer elastic claw of timing controlled rotating disk little internal tooth compressing helical spring rotating disk, the outer making leaf spring between elastic claw and helical spring rotating disk of helical spring rotating disk is pressed, thus helical spring rotating disk is turned clockwise in timing controlled rotating disk and screws 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, thus drive timing controlled turntable rotation, when timing controlled rotating disk timing controlled rotary disk limitation bar rotate touch come to two locating conductive posts time, timing controlled rotating disk stops the rotation, now timing controlled rotating disk is just rotated counterclockwise one week namely 360 °, when helical spring sheet is tightened onto in various degree, the restoring force of helical spring sheet is also different, it is also different that helical spring rotating disk does the speed counterclockwise rotated, helical spring sheet screws tighter, the restoring force of helical spring sheet is larger, it is also faster that helical spring rotating disk does the speed counterclockwise rotated, and the helical spring turntable rotation cycle of one week is also less, helical spring sheet screws more loose, and the restoring force of helical spring sheet is less, and it is also slower that helical spring rotating disk does the speed counterclockwise rotated, and the helical spring turntable rotation cycle of one week is also larger, in order to make the flight curvilinear path of guided missile not duplicate, the curve of General Requirements missile flight arrives the location point of reentrying in helical spring turntable rotation one-period, there is a timing controlled rotating disk locking key upside of timing controlled rotating disk, this timing controlled rotating disk locking key is controlled by ground artificial or carries out setup control in advance, make guided missile after locking timing controlled rotating disk locking key, the automatic control system of guided missile is in without light current duty, thus make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, without light current work, and then make enemy that electromagnetic wave tracking cannot be utilized to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when timing controlled turntable rotation to timing controlled rotary disk limitation bar rotate touch come to two locating conductive posts time, this touches by connection two locating conductive posts, the light-current system of guided missile is made to reset work after two locating conductive posts are communicated with energising, guided missile enters position of reentrying, guided missile positions precision strike to target within the extremely short time, such enemy does not just have the time of interception guided missile, different elasticities is rotated to each helical spring sheet, namely the angle of helical spring turntable rotation rotatable handle and the helical spring turntable rotation cycle T of a week do calibration curve, in order to calculating guided missile after the extra-atmospheric flight time in wartime, just by helical spring turntable rotation rotatable handle to corresponding angle, can determine that guided missile is a helical spring turntable rotation cycle 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 be contained on No. 1 heavy pointer shaft be engaged with, rotarily driven No. 1 heavily pointer rotation of No. 1 heavy pointer shaft other end by No. 1 heavy pointer shaft, No. 1 time cycle that heavily 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 cycle T of a week;
The B2 gear of B axle rotarily drives the C2 gear be contained on C axle be engaged with and rotates, C2 gear rotarily drives C axle and rotates, the C1 gear that C axle rotarily drives on C axle rotates, C1 gear rotarily drives No. 2 heavy pointer driven gear A2 be contained on No. 2 heavy pointer shafts be engaged with and rotates, rotarily driven No. 2 heavily pointers rotations of No. 2 heavy pointer shaft other ends by No. 2 heavy pointer shafts, No. 2 time cycles that heavily pointer rotates a circle are T2;
The B3 gear of B axle rotarily drives the D2 gear be contained on D axle be engaged with and rotates, D2 gear rotarily drives D axle and rotates, the D1 gear that D axle rotarily drives on D axle rotates, D1 gear rotarily drives No. 4 heavy pointer driven gear A4 be contained on No. 4 heavy pointer shafts be engaged with and rotates, rotarily driven No. 4 heavily pointers rotations of No. 4 heavy pointer shaft other ends by No. 4 heavy pointer shafts, No. 4 time cycles that heavily pointer rotates a circle are T4;
The B2 gear of B axle rotarily drives the C2 gear be contained on C axle be engaged with and rotates, C2 gear rotarily drives C axle and rotates, the C3 gear that C axle rotarily drives on C axle rotates, C3 gear rotarily drives the E2 gear be contained on E axle be engaged with and rotates, 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 be contained on No. 3 heavy pointer shafts be engaged with and rotates, No. 3 heavy pointers being rotarily driven No. 3 heavy pointer shaft other ends by No. 3 heavy pointer shafts are rotated, No. 3 time cycles that heavily pointer rotates a circle are T3,
The B3 gear of B axle rotarily drives the D2 gear be contained on D axle be engaged with and rotates, D2 gear rotarily drives D axle and rotates, the D3 gear that D axle rotarily drives on D axle rotates, D3 gear rotarily drives the F2 gear be contained on F axle be engaged with and rotates, 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 be contained on No. 5 heavy pointer shafts be engaged with and rotates, No. 5 heavy pointers being rotarily driven No. 5 heavy pointer shaft other ends by No. 5 heavy pointer shafts are rotated, No. 5 time cycles that heavily pointer rotates a circle are T5.
3, period of time T 2, No. 3 period of time T that heavy pointer rotates a circle 3, No. 4 period of time T that heavy pointer rotates a circle 4, No. 5 period of time T that heavy pointer rotates a circle 5 that the period of time T 1 that rotates a circle of No. 1 heavy pointer and No. 2 heavy pointers rotate a circle have 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 condition that T1 is constant, design different T2, T3, T4, T5, make guided missile form different curved flights, allow enemy that our guided missile cannot be found to do the rule of curve motion, thus cannot interception be calculated.
4, locating conductive post is made up of a joint fixed leg below and the movable post of a joint 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, the gap of 3mm ~ 10 mm is had between two conical surfaces, movable post just can be swung to when being subject to less power little angle that Impact direction becomes one 1 ° ~ 10 °, thus when timing controlled rotary disk limitation bar being rotated counterclockwise touch movable post, or timing controlled rotary disk limitation bar turns clockwise when touching movable post, the central axis of timing controlled rotary disk limitation bar can be made to 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, complete 360 ° of rotations can be done, thus can make guided missile after finishing the curve of one-period, can be returned on the movement locus before originally doing curve.
The present invention compared with prior art has the following advantages:
1, the present invention can pass through angle and the helical spring turntable rotation cycle T curve of a week of the helical spring turntable rotation rotatable handle demarcated in advance, according to the trajectory time that the target call guided missile of missile attack runs in exoatmosphere, regulate rapidly the angle determining helical spring turntable rotation rotatable handle.
2, apparatus of the present invention arrange different T1, T2, T3, T4, T5 parameters, form random curvilinear motion, namely utilize machine power to control guided missile and form multiple irregular curved flight, make guided missile can not send and accept any signal before entering atmosphere again, thus not easily followed the tracks of interception by enemy.
3, volume of the present invention is little, purposes is wide, cost is low, symmetrically can 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, locating conductive post 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.
Detailed description of the invention
In the embodiment shown in Fig. 1-11: for many pointers controller in controlling curve flight time and direction, comprise one and be 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 five concentric central shafts is nested together and the index system that a travelling gear other end is equipped with a heavy pointer is equipped with in each central shaft one end mutually, 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, even if thus the power that rotates of the restoring force helical spring rotating disk 38 producing helical spring sheet 40, 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 spring 50, outside the outer elastic claw 39 of helical spring rotating disk, a timing controlled rotating disk 36 is installed, multiple uniform timing controlled rotating disks little internal tooth 37 is installed inside timing controlled rotating disk 36, a timing controlled rotary disk limitation bar 43 is installed outside timing controlled rotating disk 36, two locating conductive posts 42 are had near the stage casing of timing controlled rotary disk limitation bar 43, locating conductive post 42 is not connected with timing controlled rotary disk limitation bar 43, when timing controlled rotary disk limitation bar 43 leans against two locating conductive posts 42, locating conductive post 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 made to be stuck in 0 ° of position of dial disc 35, when timing controlled rotary disk limitation bar 43 turn clockwise 360 ° time, locating conductive post 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, thus ensure that timing controlled rotary disk limitation bar 43 does when counterclockwise rotating under the effect of helical spring sheet 40 restoring force, 360 ° of complete rotations can be done, the effect of locating conductive post 42 has two: one to be that maximum a week of can only do 360 ° of restriction timing controlled rotating disk 36 rotates, two are locating conductive posts 42 timing controlled rotating disk 36 rotate and rotate to lean against on two locating conductive posts 42 time, the timing controlled rotary disk limitation bar 43 now conducted electricity is communicated with two locating conductive posts 42 and conducts electricity, namely timing controlled rotary disk limitation bar 43 is when contact two locating conductive posts 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, the central upper that helical spring rotating disk cross connects pawl 44 has a helical spring turntable rotation handle 45, 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 makes the outer elastic claw 39 of the little internal tooth 37 of timing controlled rotating disk and helical spring rotating disk contact, the little internal tooth 37 of timing controlled rotating disk oppresses the outer elastic claw 39 of helical spring rotating disk, the outer making leaf spring 50 between elastic claw 39 and helical spring rotating disk 38 of helical spring rotating disk is pressed, thus helical spring rotating disk 38 is turned clockwise in timing controlled rotating disk 36 and screws the helical spring sheet 40 in helical spring rotating disk 38, when helical spring sheet 40 screws, unclamp helical spring turntable rotation handle 45, the effect of helical spring sheet 40 restoring force drives 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, thus drive timing controlled rotating disk 36 to rotate, when timing controlled rotating disk 36 timing controlled rotary disk limitation bar 43 rotate touch come to two locating conductive posts 42 time, timing controlled rotating disk 36 stops the rotation, now timing controlled rotating disk 36 is just rotated counterclockwise one week namely 360 °, when helical spring sheet 40 rotates the different number of turns, the restoring force of helical spring sheet 40 is also different, it is also different that helical spring rotating disk 38 does the speed counterclockwise rotated, helical spring sheet 40 screws tighter, the restoring force of helical spring sheet 40 is larger, it is also faster that helical spring rotating disk 38 does the speed counterclockwise rotated, and the cycle that helical spring rotating disk 38 rotates a circle is also less, helical spring sheet 40 screws more loose, and the restoring force of helical spring sheet 40 is less, and it is also slower that helical spring rotating disk 38 does the speed counterclockwise rotated, and the cycle that helical spring rotating disk 38 rotates a circle is also larger, in order to make the flight curvilinear path of guided missile not duplicate, the curve of General Requirements missile flight rotates in one-period at helical spring rotating disk 38 location point arriving and reentry, there is a timing controlled rotating disk locking key 53 upside of timing controlled rotating disk 36, this timing controlled rotating disk locking key 53 is controlled by ground artificial or carries out setup control in advance, make guided missile after locking timing controlled rotating disk locking key 53, the automatic control system of guided missile is in without light current duty, thus make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, without light current work, and then make enemy that electromagnetic wave tracking cannot be utilized to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when timing controlled rotating disk 36 rotate to timing controlled rotary disk limitation bar 43 rotate touch come to two locating conductive posts 42 time, this touches by connection two locating conductive posts 42, the light-current system of guided missile is made to reset work after two locating conductive posts 42 are communicated with energising, guided missile enters position of reentrying, guided missile positions precision strike to target within the extremely short time, such enemy does not just have the time of interception guided missile, different elasticities is rotated to each helical spring sheet 40, namely the angle that rotates of helical spring turntable rotation handle 45 and the cycle T that rotates a circle of helical spring rotating disk 38 do 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 be contained on No. 1 heavy pointer shaft 29 be engaged with and rotates, No. 1 heavy pointer 30 being rotarily driven No. 1 heavy pointer shaft 29 other end by No. 1 heavy pointer shaft 29 is rotated, 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 cycle T that helical spring rotating disk 38 rotates a circle;
The B2 gear 3 of B axle 4 rotarily drives the C2 gear 7 be contained on C axle 6 be 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 be contained on No. 2 heavy pointer shafts 28 be engaged with and rotates, No. 2 heavy pointers 31 being rotarily driven No. 2 heavy pointer shaft 28 other ends by No. 2 heavy pointer shafts 28 are rotated, 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 be contained on D axle 8 be 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 be contained on No. 4 heavy pointer shafts 26 be engaged with and rotates, No. 4 heavy pointers 33 being rotarily driven No. 4 heavy pointer shaft 26 other ends by No. 4 heavy pointer shafts 26 are rotated, 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 be contained on C axle 6 be 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 be contained on E axle 21 be 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 be contained on No. 3 heavy pointer shafts 27 be engaged with and rotates, No. 3 heavy pointers 32 being rotarily driven No. 3 heavy pointer shaft 27 other ends by No. 3 heavy pointer shafts 27 are rotated, 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 be contained on D axle 8 be 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 be contained on F axle 14 be 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 be contained on No. 5 heavy pointer shafts 25 be engaged with and rotates, No. 5 heavy pointers 34 being rotarily driven No. 5 heavy pointer shaft 25 other ends by No. 5 heavy pointer shafts 25 are rotated, the time cycle that No. 5 heavy pointers 34 rotate a circle is T5.
The period of time T 1 that No. 1 heavy pointer 30 rotates a circle and the period of time T 5 that period of time T 4, No. 5 heavy pointers 34 that period of time T 3, No. 4 heavy pointers 33 that period of time T 2, No. 3 heavy pointers 32 that No. 2 heavy pointers 31 rotate a circle rotate a circle rotate a circle rotate a circle have 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 condition that T1 is constant, design different T2, T3, T4, T5, make guided missile form different curved flights, allow enemy that our guided missile cannot be found to do the rule of curve motion, thus cannot interception be calculated.
Locating conductive post 42 is made up of a joint fixed leg 49 below and the movable post 46 of a joint 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, the gap of 3mm ~ 10 mm is had between two conical surfaces, movable post 46 just can be swung to when being subject to less power little angle that Impact direction becomes one 1 ° ~ 10 °, thus when timing controlled rotary disk limitation bar 43 being rotated counterclockwise touch movable post 46, or timing controlled rotary disk limitation bar 43 turns clockwise when touching movable post 46, the central axis of timing controlled rotary disk limitation bar 43 can be made to be parked in 0 ° of position of dial disc 35, its objective is that the timing controlled rotary disk limitation bar 43 that timing controlled rotating disk 36 is driven is under the effect of helical spring sheet 40 restoring force, complete 360 ° of rotations can be done, thus can make guided missile after finishing the curve of one-period, can be returned on the movement locus before originally doing curve.
Claims (1)
1. for many pointers controller in controlling curve flight time and direction, comprise one and be set with B axle (4) gear train of helical spring sheet (40) as rotary power, a set of C axle (6) gear train and a set of D axle (8) gear train of three travelling gear are respectively housed, a set of E axle (21) gear train and a set of F axle (14) gear train of two travelling gears are respectively housed, and one is set with five concentric central shafts is nested together and the index system that a travelling gear other end is equipped with a heavy pointer is equipped with in each central shaft one end mutually, 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 if the power that rotates of restoring force helical spring rotating disk (38), 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 spring (50), outer elastic claw (39) outside of helical spring rotating disk is provided with a timing controlled rotating disk (36), timing controlled rotating disk (36) inner side is provided with multiple uniform little internal tooth of timing controlled rotating disk (37), timing controlled rotating disk (36) outside is provided with a timing controlled rotary disk limitation bar (43), two locating conductive posts (42) are had near the stage casing of timing controlled rotary disk limitation bar (43), locating conductive post (42) is not connected with timing controlled rotary disk limitation bar (43), when timing controlled rotary disk limitation bar (43) leans against two locating conductive post (42), locating conductive post (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 made to be stuck in 0 ° of position of dial disc (35), when timing controlled rotary disk limitation bar (43) turn clockwise 360 ° time, locating conductive post (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), thus ensure that timing controlled rotary disk limitation bar (43) is done when counterclockwise rotating under the effect of helical spring sheet (40) restoring force, 360 ° of complete rotations can be done, the effect of locating conductive post (42) has two: one to be that maximum a week of can only do 360 ° of restriction timing controlled rotating disk (36) rotates, two are locating conductive posts (42) timing controlled rotating disk (36) rotate and rotate to lean against two locating conductive posts (42) upper time, the timing controlled rotary disk limitation bar (43) now conducted electricity is communicated with two locating conductive post (42) conductions, namely timing controlled rotary disk limitation bar (43) is when contact two locating conductive post (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), the central upper that helical spring rotating disk cross connects pawl (44) has a helical spring turntable rotation handle (45), 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 makes the outer elastic claw (39) of the little internal tooth of timing controlled rotating disk (37) and helical spring rotating disk contact, the outer elastic claw (39) of the little internal tooth of timing controlled rotating disk (37) compressing helical spring rotating disk, the outer making leaf spring (50) between elastic claw (39) and helical spring rotating disk (38) of helical spring rotating disk is pressed, thus helical spring rotating disk (38) is turned clockwise in timing controlled rotating disk (36) and screws the helical spring sheet (40) in helical spring rotating disk (38), when helical spring sheet (40) screws, 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, thus drive timing controlled rotating disk (36) to rotate, when timing controlled rotating disk (36) timing controlled rotary disk limitation bar (43) rotate touch come to two locating conductive post (42) time, timing controlled rotating disk (36) stops the rotation, now timing controlled rotating disk (36) is just rotated counterclockwise one week namely 360 °, when helical spring sheet (40) rotates the different number of turns, the restoring force of helical spring sheet (40) is also different, it is also different that helical spring rotating disk (38) does the speed counterclockwise rotated, helical spring sheet (40) screws tighter, the restoring force of helical spring sheet (40) is larger, it is also faster that helical spring rotating disk (38) does the speed counterclockwise rotated, and the cycle that helical spring rotating disk (38) rotates a circle is also less, helical spring sheet (40) screws more loose, and the restoring force of helical spring sheet (40) is less, and it is also slower that helical spring rotating disk (38) does the speed counterclockwise rotated, and the cycle that helical spring rotating disk (38) rotates a circle is also larger, in order to make the flight curvilinear path of guided missile not duplicate, require that the curve of missile flight rotates at helical spring rotating disk (38) location point arriving in one-period and reentry, there is a timing controlled rotating disk locking key (53) upside of timing controlled rotating disk (36), this timing controlled rotating disk locking key (53) is controlled by ground artificial or carries out setup control in advance, make guided missile after locking timing controlled rotating disk locking key (53), the automatic control system of guided missile is in without light current duty, thus make guided missile not send any electromagnetic wave in extraatmospheric flight stage casing, and the automatic control system of guided missile is in without light current duty, and then make enemy that electromagnetic wave tracking cannot be utilized to find missile target, more make enemy cannot utilize advanced strong electromagnetic system destruction guided missile system, but when timing controlled rotating disk (36) rotate to timing controlled rotary disk limitation bar (43) rotate touch come to two locating conductive post (42) time, this touches by connection two locating conductive posts (42), the light-current system of guided missile is made to reset work after two locating conductive posts (42) are communicated with energising, guided missile enters position of reentrying, guided missile positions precision strike to target within the extremely short time, such enemy does not just have the time of interception guided missile, different elasticities is rotated to each helical spring sheet (40), namely the cycle T that the angle that rotates of helical spring turntable rotation handle (45) and helical spring rotating disk (38) rotate a circle does 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 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) A1 be contained on No. 1 heavy pointer shaft (29) be engaged with and rotates, No. 1 heavy pointer (30) being rotarily driven No. 1 heavy pointer shaft (29) other end by No. 1 heavy pointer shaft (29) is rotated, 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 cycle T that helical spring rotating disk (38) rotates a circle;
The B2 gear (3) of B axle (4) rotarily drives the C2 gear (7) be contained on C axle (6) be 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 (19) A2 be contained on No. 2 heavy pointer shafts (28) be engaged with and rotates, No. 2 heavy pointers (31) being rotarily driven No. 2 heavy pointer shaft (28) other ends by No. 2 heavy pointer shafts (28) are rotated, No. 2 time cycles that heavily pointer (31) rotates a circle are T2,
The B3 gear (1) of B axle (4) rotarily drives the D2 gear (11) be contained on D axle (8) be 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 (17) A4 be contained on No. 4 heavy pointer shafts (26) be engaged with and rotates, No. 4 heavy pointers (33) being rotarily driven No. 4 heavy pointer shaft (26) other ends by No. 4 heavy pointer shafts (26) are rotated, No. 4 time cycles that heavily pointer (33) rotates a circle are T4,
The B2 gear (3) of B axle (4) rotarily drives the C2 gear (7) be contained on C axle (6) be 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) be contained on E axle (21) be 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 (18) A3 be contained on No. 3 heavy pointer shafts (27) be engaged with and rotates, No. 3 heavy pointers (32) being rotarily driven No. 3 heavy pointer shaft (27) other ends by No. 3 heavy pointer shafts (27) are rotated, No. 3 time cycles that heavily pointer (32) rotates a circle are T3,
The B3 gear (1) of B axle (4) rotarily drives the D2 gear (11) be contained on D axle (8) be 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) be contained on F axle (14) be 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 (16) A5 be contained on No. 5 heavy pointer shafts (25) be engaged with and rotates, No. 5 heavy pointers (34) being rotarily driven No. 5 heavy pointer shaft (25) other ends by No. 5 heavy pointer shafts (25) are rotated, No. 5 time cycles that heavily pointer (34) rotates a circle are T5.
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| NL7408362A (en) * | 1973-08-02 | 1975-02-04 | Krauss Maffei Ag | METHOD AND DEVICE FOR SIMULATING THE FIRE OR DISCHARGE OF A PROJECTILE. |
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