CN107144186A - A kind of memorial alloy constraint formula interrupter based on inertia - Google Patents

A kind of memorial alloy constraint formula interrupter based on inertia Download PDF

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Publication number
CN107144186A
CN107144186A CN201710498538.3A CN201710498538A CN107144186A CN 107144186 A CN107144186 A CN 107144186A CN 201710498538 A CN201710498538 A CN 201710498538A CN 107144186 A CN107144186 A CN 107144186A
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CN
China
Prior art keywords
rotor
hole
arm
pin
memorial alloy
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Granted
Application number
CN201710498538.3A
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Chinese (zh)
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CN107144186B (en
Inventor
李响
李晓
张俊
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Hubei Sanjiang Aerospace Honglin Exploration and Control Co Ltd
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Hubei Sanjiang Aerospace Honglin Exploration and Control Co Ltd
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Priority to CN201710498538.3A priority Critical patent/CN107144186B/en
Publication of CN107144186A publication Critical patent/CN107144186A/en
Application granted granted Critical
Publication of CN107144186B publication Critical patent/CN107144186B/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/24Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/20Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
    • F42C15/21Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using spring action

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

Formula interrupter is constrained the invention discloses a kind of memorial alloy based on inertia, belongs to fuze safety mechanism technical field.The interrupter includes the body that center is provided with rotor hole, and coaxial sleeve insertion rotor hole in can opposing body rotate rotor, accommodating memorial alloy pin removal, inertial elements part are offered on rotor and body, the corresponding hole of fiery part and detonation transmission part is passed, by optimizing hole location relation, make interrupter that there is larger releasing isolation corner, and settings of multistage insurance institution enables and is locked in corresponding position with the interrupter under arm-to-arm under safe condition.On the one hand the present invention optimizes the arrangement of parts form of interrupter, reduces the bulk of interrupter, improve the applicability of interrupter by above-mentioned setting;On the other hand, two-stage insurance can effectively improve under the security of interrupter, arm-to-arm two-stage locking ignition sequence can be effectively ensured and aligns under safe condition, greatly improve ignition efficiency.

Description

A kind of memorial alloy constraint formula interrupter based on inertia
Technical field
The invention belongs to fuze safety mechanism technical field, and in particular to it is a kind of based on inertia memorial alloy constraint formula every Disembark structure.
Background technology
Priming system is equipped with gunpowder or explosive, is burnt or exploded by being produced after environmental stimuli, with the gunpowder that ignites, ignition charge Or do the disposable component of mechanical work and the general name of device.Interrupter is usually provided with priming system, it is made Be make sensitive firer's element in Explosive sequence usually with next stage firer's element separation, it is ensured that fuse is accidental in its priming system Misfire during preact, so as to avoid ammunition premature burst so that jeopardizing the safety of personnel and equipment.
The security of fuse be related to the demonstration of fuse, design, manufacture, inspection and acceptance, experiment, duties processing, using and The life cycle managements such as explosive disposal.In safety period life-cycle of fuse, the effect of interrupter is to ensure fuse right Arm-to-arm is in effective short-term/space of interacting goals, is safe condition in the case of remaining.
At present, conventional interrupter mechanism has slide block mechanism, lever type mechanisms and isolation rotor mechanism, wherein being turned with level Minor interrupter is relatively conventional.Under normal circumstances, horizontal rotor formula interrupter utilizes torsion spring, clockwork spring (disc spring) or other Spring, with less axial dimension, is adapted to the small occasion of axial dimension requirement, and level as the motive power of mechanism kinematic Rotator type interrupter has larger releasing isolation corner, can ensure that flame proof security generally.But, it is existing Horizontal rotor formula interrupter there is also certain defect, its defect be mainly grouped as it is following some.First, when interrupter is protected After danger releases and moved in place, interrupter does not have lock function, under vibration, easily causes interrupter dislocation, Explosive train is ultimately resulted in align not exclusively;Secondly, the two-stage safety piece Heterogeneous Permutation of horizontal rotor formula interrupter can cause Mechanism size is larger, unreasonable to space utilization;Again, horizontal rotor formula interrupter usually not effectively utilizes the ring on bullet Environment information (such as fly overload, centrifugal force, Aerodynamic Heating), and the driving of two-stage safety piece needs consumption fuse or missile power supply, Energy dissipation is caused, and security is relatively low.Drawbacks described above causes the application of horizontal rotor formula interrupter to be subject to certain restrictions, Security and practicality to interrupter have a certain impact, it is impossible to fully meet the safe handling of fuse.
The content of the invention
For the disadvantages described above or Improvement requirement of prior art, the invention provides a kind of memorial alloy based on inertia about Beam formula interrupter, wherein the setting insured by using two-stage, is provided with larger releasing isolation corner, it is ensured that usually every Quick-fried security, and interrupter has lock function after motion in place, can ensure that under vibration in state in place, it is ensured that The reliability of detonation, lifts the security and practicality of fuze mechanism.
To achieve the above object, formula is constrained there is provided a kind of memorial alloy based on inertia according to one aspect of the present invention Interrupter, including center are provided with the body of rotor hole, and in coaxial sleeve insertion rotor hole can the rotor that rotates of opposing body, Characterized in that,
The end face of respective rotor offers first blind hole of accommodating inertial elements part one end, for housing on the body Second blind hole of memorial alloy pin removal, and for housing the propagation of explosion hole of detonation transmission part;
With this accordingly, offered on the rotor for the accommodating flash hole for passing fiery part, in the secure state with the One blind hole position it is corresponding for the inertial elements part other end it is accommodating wherein with the 3rd blind hole that locks the safe condition and The latch ends for memorial alloy pin removal corresponding with second blind hole are inserted locking the peace in the secure state The pin hole of total state;
During arm-to-arm is converted under rotor is driven from safe condition, the inertial elements part is driven And depart from from the 3rd blind hole and make it that the inertial elements part is integrally placed in first blind hole, correspondingly, The latch ends of the memorial alloy pin removal are driven to be departed from from the pin hole, and then the rotor can be rotated by driving Certain angle so that the accommodating hole for passing fiery part and the detonation transmission part is aligned, and first blind hole and the latch Hole align and so that one end of the inertial elements part is embedded in the pin hole to lock the arm-to-arm, so as to can realize The arm-to-arm is transformed into from safe condition and locks the arm-to-arm.
As a further improvement on the present invention, arc groove is offered on the rotor, for being led for rotor rotation direction To and limit the rotational angle of rotor.
As a further improvement on the present invention, on cross section the arc groove two ends and rotor hole center line institute The angle that the angle of composition need to be rotated when being converted to arm-to-arm from safe condition with rotor is identical.
As a further improvement on the present invention, on cross section the arc groove two ends and rotor hole center line institute The angle of composition is 75 °~135 °.
As a further improvement on the present invention, it is further opened with being used to house locking member on the end face of rotor correspondence body The 4th blind hole, for housing locking member, correspondingly, corresponding ball pin hole is offered on the body;
The locking member includes Lock spring and ball pin, and the Lock spring is in contraction state in the secure state, The rotor hole end contact of the ball pin end and the body, rotor from safe condition turn to arm-to-arm when, described the Four blind holes are just aligned with the ball pin hole, i.e., the Lock spring compressive state of described locking member is released, and ball pin insertion is described So as to lock the arm-to-arm in ball pin hole.
As a further improvement on the present invention, the inertial elements part includes inertia cylinder and inertial spring, the inertia One end of cylinder offers the groove for fixing described inertial spring one end;
In the secure state, the inertia cylinder is placed in the 3rd blind hole on the side end face of rotor one, described The other end of inertial spring is placed in first blind hole on the body;The rotor turns to pending from safe condition In state procedure, the inertial spring is in compressive state and the inertial elements part is integrally embedded in first blind hole; When the rotor turns to arm-to-arm, first blind hole is aligned with the pin hole on the rotor, and the inertia cylinder is embedded To lock the arm-to-arm in the pin hole.
As a further improvement on the present invention, the memorial alloy pin removal includes pin, limit spring, pressure spiral shell, housing With memorial alloy sleeve;
The pin is T-shaped structure, and its front end is the latch ends of the memorial alloy pin removal, and the limit spring is arranged In the latch ends;
Step groove is offered on one side end face of the housing, the pressure spiral shell that its exit offers through hole by middle part is sealed Dress, step groove is equipped with the memorial alloy sleeve, the pin, the spacing bullet in original state successively from bottom to top Spring, and the memorial alloy sleeve is placed on the ladder in step groove, leave below can house it is absolutely empty in pin rear end Between;
The memorial alloy sleeve is hollow sleeve tubular, and the pin and limit spring are placed in sleeve, and the note The bottom for recalling alloy sleeve is provided with memory step for limiting the pin position in an initial condition;
In the secure state, the bottom of the memorial alloy sleeve has memory step, constrains the limit spring and is in Compressive state, and the latch ends of the pin stretch out from the through hole on the pressure spiral shell, in the pin hole on the embedded rotor with Lock the safe condition;The rotor from safe condition be converted to arm-to-arm when, the memorial alloy pin removal is powered, described The memory step of memorial alloy sleeve bottom disappears, and relieves constraint of the memorial alloy sleeve to the pin, the limit The compressive state of position spring is released, and is detached the latch ends of the pin from the pin hole by elastic force is recovered, releasing pair The locking of the rotor.
In general, by the contemplated above technical scheme of the present invention compared with prior art, with following beneficial effect Really:
(1) in the constraint formula interrupter of the memorial alloy based on inertia of the invention, make by using inertial elements part For level of safety mechanism, memorial alloy pin removal is used as another grade of insurance institution, two-stage insurance institution collective effect, it is ensured that isolation The rotor of mechanism does not rotate in the secure state, the occurrence of reducing unintended detonation, improves the security of interrupter;
(2) in the constraint formula interrupter of the memorial alloy based on inertia of the invention, when interrupter is in arm-to-arm When, by using locking member as one-level locking mechanism, inertial elements part is used as another grade of locking mechanism, two-stage locking machine Structure collective effect, it is ensured that generating mechanism does not misplace interrupter under arm-to-arm, especially reduces and isolates machine under vibration environment The component dislocation of structure, largely avoided explosive train and aligns incomplete problem;
(3) in the constraint formula interrupter of the memorial alloy based on inertia of the invention, by arc groove and alignment pin to turning Sub- rotation direction and angle are defined, and the isolation corner of setting is larger, and interrupter can be effectively ensured in State Transferring When component align, and greatly promote the daily flame proof security of fuze mechanism;
(4) the two-stage Arming Assembly under the constraint formula interrupter of the memorial alloy based on inertia of the invention, safe condition Optimized the arrangement of with the two-stage Arming Assembly under arm-to-arm, make the latch that memorial alloy pin removal latch ends are housed during safe condition Hole can be in arm-to-arm with accommodating inertial elements part the first blind hole align, for inertial elements part one end be embedded in Arm-to-arm locking is carried out, by rationally designing hole location, idle hole is made full use of, so as to greatly reduce isolation The bulk of mechanism;
(5) the constraint formula interrupter of the memorial alloy based on inertia of the invention, its insurance institution can be utilized respectively on bullet Environmental information and control system instruction, the security of interrupter can be substantially improved.
Brief description of the drawings
Fig. 1 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the overall structure diagram of formula interrupter;
Fig. 2 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the rotor structure side view of formula interrupter;
Fig. 3 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the rotor structure top view of formula interrupter;
Fig. 4 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the driving part sectional view of formula interrupter;
Fig. 5 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the driving part dismounting figure of formula interrupter;
Fig. 6 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the inertial elements part structures of formula interrupter Sectional view;
Fig. 7 is the fiery modular construction section view of biography of the constraint formula interrupter of the memorial alloy based on inertia of the embodiment of the present invention Figure;
Fig. 8 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the locking member structure section view of formula interrupter Figure;
At the beginning of Fig. 9 is the memorial alloy pin removal of the constraint formula interrupter of the memorial alloy based on inertia of the embodiment of the present invention Beginning view;
Figure 10 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the memorial alloy pin removal of formula interrupter View in place;
Figure 11 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the body construction top view of formula interrupter;
Figure 12 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the body construction side view of formula interrupter.
In all of the figs, same reference represents identical technical characteristic, is specially:1. rotor, 101. torsion springs Groove, 102. shaft holes, 103. flash holes, 104. the 4th blind holes, 105. the 5th blind holes, 106. the 3rd blind holes, 107. pin holes, 108. lock hole, 109. dead axle holes, 1010. arc grooves;2. driving part, 201. torsion springs, 202. rotating shafts, 203. axis of rolling Hold, 204. pressing plates;3. inertial elements part, 301. inertia cylinder, 302. inertial springs;4. fiery part is passed, 401. flame detonators, 402. shells, 403. beams;5. locking member, 501. ball pins, 502. Lock springs, 503. wires;6. guide finger, 7. propagation of explosions Part, 8. bodies, 801. rotor holes, 802. shaft holes, 803. first blind holes, 804. second blind holes, 805. ball pin holes, 806. spiral shells Pit, 807. sides position hole, 808. propagation of explosion holes;9. memorial alloy pin removal, 901. pins, 902. limit springs, 903. pressure spiral shells, 904. housings, 905. memorial alloy sleeves, 906. wires.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only to explain the present invention, not For limiting the present invention.
As long as in addition, technical characteristic involved in each embodiment of invention described below is each other not Constituting conflict can just be mutually combined.
Fig. 1 is that the memorial alloy based on inertia of the embodiment of the present invention constrains the overall structure diagram of formula interrupter; Fig. 2 is the rotor structure side view of the interrupter of the embodiment of the present invention;Fig. 3 is the rotor of the interrupter of the embodiment of the present invention Structure front view;Fig. 4 is the driving part structure sectional view of the interrupter of the embodiment of the present invention;Fig. 5 is the embodiment of the present invention Interrupter driving part structure dismounting figure;Fig. 6 is the inertial elements modular construction of the interrupter of the embodiment of the present invention Sectional view;Fig. 7 is the fiery modular construction sectional view of biography of the interrupter of the embodiment of the present invention;Fig. 8 be the embodiment of the present invention every Disembark the locking member structure sectional view of structure;Fig. 9 is the memorial alloy pin removal initial shape of the interrupter of the embodiment of the present invention State schematic diagram;Figure 10 is the memorial alloy pin removal view in place of the interrupter of the embodiment of the present invention;Figure 11 is this The body construction front view of the interrupter of inventive embodiments;Figure 12 is the body construction side of the interrupter of the embodiment of the present invention View.
As shown in accompanying drawing 1~12, the interrupter in a preferred embodiment of the present invention mainly includes rotor 1, driving The fiery part 4 of part 2, inertial elements part 3, biography, locking member 5, guide finger 6, detonation transmission part 7, body 8 and memorial alloy are pulled pin Device 9.
Wherein, rotor 1 is to offer to accommodate interrupter critical piece in the core component of interrupter, its both ends of the surface Hole or cell body;Driving part 2 is mainly used in driving rotor 1 and moved, and rotor 1 is switched in arm-to-arm and safe condition, Driving part 2 mainly includes torsion spring 201, the rotating shaft 202 for transmission, the rolling bearing 203 of accessory drive for providing driving force And the pressing plate 204 for fixed drive part 2;Inertial elements part 3 is one of main securing member of interrupter, and it is led To be made up of inertia cylinder 301 and inertial spring 302;It is one of critical piece that fuse is used for ignition to pass fiery part 4, and it is mainly wrapped Include flame detonator 401, shell 402 and beam 403;Locking member 5 is mainly used in when rotor 1 is in arm-to-arm, to turning The location status of son 1 is locked, it is ensured that interrupter occurs without the situation of dislocation;Guide finger 6 is mainly used in controlling rotor 1 The anglec of rotation, it is ensured that the angle that rotor 1 rotates is within certain control range, so that associated components are occurred without before and after rotation Dislocation;Detonation transmission part 7 is mainly used in igniting priming system with passing the fiery mating reaction of part 4;Body 8 is the main body machine of interrupter The hole or cell body for accommodating interrupter critical piece are offered in one of structure, its both ends of the surface;Memorial alloy pin removal 9 is isolation One of main securing member of mechanism, mainly includes pin 901, limit spring 902, pressure spiral shell 903, housing 904, memorial alloy set Cylinder 905 and wire 906.
Further, rotor 1 and body 8 are in that receiving rotor 1 is offered on cylindrical structural, the one end side of body 8 Rotor hole 801, rotor hole 801 is blind cylindrical hole, and the coaxial sleeve of rotor 1 is embedded in rotor hole 801, and can opposing body 8 enter Row is rotated, and the height of rotor 1 is preferably identical with the depth of rotor hole 801.
Specifically, as shown in figures 2-3, using rotor 1 away from the bottom of rotor hole 801 a side end face as its upper surface, turn On the upper surface of son 1, the torsional spring slot 101 for placing torsion spring 201 in driving part 2 is offered, torsional spring slot 101 is annular groove, It is centrally located on the axis of rotor 1, and the bar shaped for being further opened with matching with the protruding end on torsion spring 201 on torsional spring slot 101 is recessed Groove, the both sides of torsional spring slot 101 are further opened with journal stirrup groove, and the both sides journal stirrup for placing pressing plate 204, the depth of torsional spring slot 101 is excellent Choosing is slightly below the thickness sum of pressing plate 204 and torsion spring 201, it is ensured that its upper surface can protrude the upper end of rotor 1 after pressing plate 204 is fixed Face.It is further opened with connecting the through hole of the both sides end face of rotor 1 on rotor 1, is used as the shaft hole of the rotating shaft 202 of arrangement driving part 2 102, the axis of shaft hole 102 is overlapped with the axis of rotor 1.
Further, the arc groove 1010 for placing guide finger 6 is further opened with the upper surface of rotor 1, arc is recessed Groove 1010 is connects the intercommunicating pore of the both ends of the surface of rotor 1, and the center of circle of groove is located on the axis of rotor 1, i.e. arc groove 1010 The each section of distance away from the axis of rotor 1 is all equal.In a preferred embodiment, guide finger 6 is fixedly installed on arc groove 1010 are fixed on body 8 close to one end of the 3rd blind hole 106, the bottom of guide finger 6;Rotor 1 under the limitation of guide finger 6, Rotated in a fixed angle, this angle corresponds to the angle of arc groove 1010.The two ends of arc groove 1010 correspondence turns The angle in the sub 1 end face center of circle is in a preferred embodiment 90 °, and certainly, the angle of arc groove 1010 also can be according to specific Situation selects other numerical value, such as 75 °, 85 °, 105 °, 135 °, in a preferred embodiment, the folder of arc groove 1010 Angular region is 75 °~135 °.
Correspondingly, using rotor 1 close to the bottom of rotor hole 801 a side end face as its lower surface, in the lower surface of rotor 1 On, flash hole 103 is offered, flash hole 103 is shoulder hole, fiery part 4 is passed for fixed;Also opened on the lower surface of rotor 1 Provided with the 4th blind hole 104, the 4th blind hole 104 is also shoulder hole, for installing locking member 5;In addition, on the lower surface of rotor 1 Three shrinkage pools are further opened with, three shrinkage pools are preferably internal diameter identical blind hole, and the diameter of shrinkage pool is not specifically limited, can basis Concrete condition is selected, and three shrinkage pools are respectively to be used to place the 3rd blind hole 106 of inertial elements part 3, correspondence detonation transmission part 7 5th blind hole 105, and for pin hole 107 corresponding with the latch ends of the pin 901 of memorial alloy pin removal 9.Above-mentioned ladder Hole and the position that opens up of shrinkage pool are not specifically limited, can decision design as the case may be, but the position of shoulder hole and shrinkage pool The relation of putting must hole location corresponding with body 8 be corresponding opens up, the shoulder hole center of circle and the shrinkage pool center of circle with the center of circle of rotor 1 away from From with arc groove 1010 away from identical with a distance from the center of circle, and flash hole 103, the center of circle of the 5th blind hole 105 and the circle center line connecting of rotor 1 The angle of composition must be identical with the angle of arc groove 1010, and the 3rd blind hole 106, two centers of circle of pin hole 107 and rotor 1 are justified The angle that the line of the heart is constituted is also identical with the angle of arc groove 1010.
Corresponding with rotor 1, such as Figure 11~12 show respective rotor on the body 8 in a preferred embodiment, body 8 1 offers corresponding hole slot.Specifically, the overall preferably cylindrical structure of body 8, its upper surface corresponds to the shape of rotor 1 Rotor hole 801 corresponding with the size of rotor 1, i.e. rotor hole 801 are provided with for the cylindrical shrinkage pool with certain depth and diameter; Dead axle hole 109 on the lower surface of the bottom end face center respective rotor 1 of rotor hole 801 offers shaft hole 802, shaft hole 802 essentially cylindrical blind holes, its side offers vertical bar connected in star, for fixed rotating shaft 202;The two of shaft hole 802 Side correspondence is disposed with two blind holes, i.e. the first blind hole 803 and the second blind hole 804.Wherein, the first blind hole 803 is used to house inertia One end of securing member 3, the second blind hole 804 be used for house memorial alloy pin removal 9, further, two blind hole centers of circle for The distance of the axis of body 8 is identical with distance of the arc groove 1010 away from axis on rotor 1, and two blind hole centers of circle and rotor The angle that the bottom surface circle center line connecting of hole 801 is constituted is identical with the angle of arc groove 1010, that is, ensures that fuze mechanism is in safety During state, the first blind hole 803 is aligned with the 3rd blind hole 106 on the lower surface of rotor 1, in the second blind hole 804 and the lower surface of rotor 1 Pin hole 107 align so that ensureing the two-stage insurance of interrupter by rotor 1 can be locked in safe condition when initial Under.
Further, the 4th blind hole 104 on the bottom surface of rotor hole 801 in respective rotor 1 is provided with ball pin hole 805, is used for When ensureing that fuze mechanism is in arm-to-arm, the locking member 5 on rotor 1 can be aligned therewith;Correspondence on the bottom surface of rotor hole 801 The guide finger 6 arranged on rotor 1 is provided with screwed hole 806, the bottom spiral for being directed to pin 6 is fixed on screwed hole 806 In, rotor 1 is limited within certain slewing area indirectly.Side position hole 807 is further opened with the side of body 8, it is opened up Position is that when ensureing that fuze mechanism is in a safe condition, lock hole 108 and the side position hole 807 of rotor 1 are aligned;Further, exist The propagation of explosion hole 808 for placing detonation transmission part 7 is offered on the lower surface of body 8, the depth in propagation of explosion hole 808 is preferably from body 8 Lower surface connect the bottom surface of rotor hole 801, the internal diameter in propagation of explosion hole 808 is not especially limited, can be preferred as the case may be Design, but fuze mechanism is must assure that in arm-to-arm, the flash hole 103 above rotor 1 must be aligned with propagation of explosion hole 808, Ensure that passing fiery part 4 can align with detonation transmission part 7, so as to ensure that Explosive sequence can be aligned.
Further, be as shown in Figures 4 and 5 the driving part 2 in a preferred embodiment, its mainly include torsion spring 201, Rotating shaft 202, rolling bearing 203 and pressing plate 204, torsion spring 201 are mainly that the rotation of rotor 1 provides driving force, and its driving force is not Required driving force when being rotate in place less than rotor 1;Rotating shaft 202 is multi-diameter shaft, following table of the less one end of its diameter of axle from rotor 1 Face passes through and passed from the shaft hole 102 on the upper surface of rotor 1, connects the part of upper level;It is further preferred that pressing plate 204 are fixed on the upper surface of rotor 1, prevent torsion spring 201 from throwing away, and its upper surface protrudes the upper surface of rotor 1, is easy to 1 turn of rotor When dynamic, the only upper surface of pressing plate 204 and upper level component contact, and the upper surface of rotor 1 not with upper level component contact, reduce CONTACT WITH FRICTION area, reduces the rotary resistance of rotor 1;In order to further reduce the pivoting friction resistance of rotor 1, in rotating shaft Rolling bearing 203 is provided between 202 and the lower surface of rotor 1, rolling bearing 203 is set in one that rotating shaft 202 passes through rotor 1 End, and in the dead axle hole 109 being arranged on the lower surface of rotor 1;In addition, the bottom of rotating shaft 202 is fixed on the rotating shaft in the middle of body 8 Among hole 802, in order to prevent rotating shaft 202 from being rotated in shaft hole 802, the side of the bottom fixing end of rotating shaft 202 is provided with one Individual perpendicular strip bulge, shaft hole 802 is correspondingly arranged on a groove, rotating shaft 202 is put into after shaft hole 802, and rotating shaft 202 is relative Do not rotated in body 8.
The inertial elements part 3 in a preferred embodiment is illustrated in figure 6, it is mainly by inertia cylinder 301 and inertia spring 302 compositions, one end of inertia cylinder 301 offers the groove of fixed one end of inertial spring 302.In the secure state, inertia cylinder 301 It is placed in the 3rd blind hole 106 on the side end face of rotor 1 one, insert depth is preferably 2~3mm, the other end of inertial spring 302 It is placed in the first blind hole 803 on body 8;Rotor 1 is turned to during arm-to-arm from safe condition, inertial spring 302 In compressive state and overall embedded first blind hole 803 of inertial elements part 3;When rotor 1 turns to arm-to-arm, first is blind Hole 803 is aligned with the pin hole 107 on rotor 1, and inertia cylinder 301 is embedded in pin hole 107 to lock the arm-to-arm.
The fiery part 4 of biography being illustrated in figure 7 in a preferred embodiment, it is mainly by flame detonator 401, the and of shell 402 Beam 403 is constituted, and screw thread is preferably offered on shell 402, and coordinate the flash hole 103 for being fixed on rotor 1 by screw thread In, pass the lower surface that its lower end after fiery part 4 is fixed does not protrude rotor 1;Further, the bottom beam 403 of fiery part 4 is passed Preferably red copper pad, for buffer protection flame detonator 401, prevents the unexpected triggering flame detonator 401 that clashes.
The locking member 5 in a preferred embodiment is illustrated in figure 8, it is mainly by ball pin 501, the and of Lock spring 502 Wire 503 is constituted, and screw thread is offered on the outer peripheral face of wire 503, for locking member 5 to be arranged on the lower surface of rotor 1 In 4th blind hole 104, and the lower surface of the not prominent rotor 1 in lower surface of wire 503;The upper end of Lock spring 502 is placed on wire In 503, its lower end is placed in the upper recess of ball pin 501, when fuse is in a safe condition, and Lock spring 502 is in pressure Contracting state, the bottom of ball pin 501 is contacted with body 8.When rotor 1 turns to arm-to-arm from safe condition, locking member 5 Aligned with the ball pin hole 805 on body 8, the Lock spring 502 in compressive state promotes ball pin 501 to be embedded into ball pin hole 805 In, the position of rotor 1 is locked in arm-to-arm.
As Fig. 9~10 show memorial alloy pin removal 9 in a preferred embodiment, it is mainly by pin 901, spacing Spring 902, pressure spiral shell 903, housing 904, memorial alloy sleeve 905 and wire 906 are constituted.Specifically, memorial alloy pin removal 9 It is fixed in the second blind hole 804, pin 901 is T-shaped structure, its axial end is the latch ends of memorial alloy pin removal 9, spacing bullet Spring 902 is set in the latch ends;Step groove is offered on one side end face of housing 904, its exit is offered by middle part The pressure spiral shell 903 of through hole is encapsulated, and step groove is equipped with memorial alloy sleeve 905, pin in original state successively from bottom to top 901st, limit spring 902, and memorial alloy sleeve 905 is placed on the ladder in step groove, pin can be housed below by leaving 901 hollow space;Memorial alloy sleeve 905 is hollow sleeve tubular, and pin 901 and limit spring 902 are placed in sleeve, and The bottom of memorial alloy sleeve 905 is provided with the memory step for limiting the position of pin 901 in an initial condition;
In the secure state, the bottom of memorial alloy sleeve 905 has memory step, and constraint limit spring 902 is in pressure Contracting state, and the latch ends of pin 901 stretch out from the through hole on pressure spiral shell 903, to lock in the pin hole 107 on embedded rotor 1 The safe condition;When rotor 1 is converted to arm-to-arm from safe condition, memorial alloy pin removal 9 is powered, memorial alloy sleeve The memory step of 905 bottoms disappears, and relieves constraint of the memorial alloy sleeve 905 to pin 901, the compression of limit spring 902 Status releasing, recovers elastic force by it and detaches the latch ends of pin 901 from pin hole 107, release the locking to rotor 1.
In the interrupter of a preferred embodiment, when it is in initial safe state, the first blind hole on body 8 803 align with the 3rd blind hole 106 on the lower surface of rotor 1, the second blind hole 804 and 107 pairs of pin hole on the lower surface of rotor 1 Just, i.e. the inertia cylinder 301 of inertial elements part 3 is embedded in the 3rd blind hole 106, and the insertion first of inertial spring 302 of the other end is blind In hole 803, it is embedded in as the pin 901 of the level of safety of interrupter, and memorial alloy pin removal 9 in pin hole 107, as Rotor 1 is locked in the home position of safe condition, drive division by the other level of safety of interrupter, two-stage insurance collective effect Part 2 can not drive rotor 1 to rotate, now, pass fiery part 4 away from detonation transmission part 7, even if passing the fiery accidental action of part 4, also will not Detonation transmission part 7 is ignited, the security of fuze mechanism is fully ensured that;When fuze mechanism is transformed into arm-to-arm by safe condition, When i.e. interrupter experiences lasting environment overload, the inertia cylinder 301 of inertial elements part 3 is under sustained overload effect, compression Inertial spring 302 is moved, and inertia cylinder 301 departs from from the 3rd blind hole 106 of embedded rotor 1, and inertial elements part 3 is released to turning The constraint of son 1.Meanwhile, control system assigns power supply instruction, the note of the bottom of memorial alloy sleeve 905 to memorial alloy pin removal 9 Recall step disappearance, relieve constraint of the memorial alloy sleeve 905 to pin 901, the compressive state of limit spring 902 is released, according to Recover elastic force by it to detach the latch ends of pin 901 from pin hole 107, release the locking to rotor 1.Now, rotor 1 exists Under the twisting resistance driving of the torsion spring 201 of driving part 2, arm-to-arm, in this course, drive division are rotated to by safe condition The driving force of torsion spring 201 of part 2 otherwise required driving force when being rotate in place less than rotor 1, guide finger 6 are played in this course Guide effect and position-limiting action, it is ensured that rotor 1 can turn to correspondence position, and can be limited to the position.When fuze mechanism turns When changing to arm-to-arm, the ball pin 501 of locking member 5 is embedded in corresponding ball pin hole 805, accordingly, memorial alloy pin removal 9 Deenergization, the first blind hole 803 is now aligned with being used to house the pin hole 107 of pin 901 on the lower surface of original rotor 1, Then the inertia cylinder 301 of inertial elements part 3 is embedded in pin hole 107 to lock the arm-to-arm, i.e. the now He of locking member 5 Inertial elements part 3 carries out state locking to the interrupter under arm-to-arm.Further, under arm-to-arm the fiery part of biography 4 align with detonation transmission part 7, when primary priming system is acted on, and ignite and pass fiery part 4, then ignite detonation transmission part 7, be finally completed The ignition of whole priming system.
As it will be easily appreciated by one skilled in the art that the foregoing is merely illustrative of the preferred embodiments of the present invention, it is not used to The limitation present invention, any modifications, equivalent substitutions and improvements made within the spirit and principles of the invention etc., it all should include Within protection scope of the present invention.

Claims (7)

1. a kind of memorial alloy constraint formula interrupter based on inertia, including center are provided with the body (8) of rotor hole (801), And can the rotor (1) that rotates of opposing body (8) in coaxial sleeve insertion rotor hole (801), it is characterised in that
The end face of respective rotor (1) offers first blind hole of accommodating inertial elements part (3) one end on the body (8) (803), for housing the second blind hole (804) of memorial alloy pin removal (9), and for housing the propagation of explosion of detonation transmission part (7) Hole (808);
With this accordingly, offered on the rotor (1) for the accommodating flash hole (103) for passing fiery part (4), in safe condition Lower inertial elements part (3) other end that is used for corresponding with the first blind hole (803) position houses wherein to lock the safe condition The 3rd blind hole (106) and in the secure state it is corresponding with second blind hole (804) be used for memorial alloy pin removal (9) latch ends are inserted locking the pin hole (107) of the safe condition;
During arm-to-arm is converted under rotor (1) is driven from safe condition, the inertial elements part (3) is driven Move and depart from from the 3rd blind hole (106) and cause the inertial elements part (3) to be integrally placed in first blind hole (803) in, correspondingly, the latch ends of the memorial alloy pin removal (9) are driven to be departed from from the pin hole (107), is entered And the rotor (1) can be driven and be turned an angle so that the accommodating fiery part (4) of biography and the detonation transmission part (7) Hole align, and first blind hole (803) and the pin hole (107) align and cause the inertial elements part (3) One end is embedded in the pin hole (107) to lock the arm-to-arm, thus can realize be transformed into from safe condition it is described pending State simultaneously locks the arm-to-arm.
2. the memorial alloy constraint formula interrupter according to claim 1 based on inertia, wherein, opened up on the rotor (1) There is arc groove (1010), for turning to the rotation that arm-to-arm is oriented to and limits rotor (1) from safe condition for rotor (1) Angle.
3. formula interrupter is constrained according to the memorial alloy based on inertia of claim 1 or 2, wherein, it is described on cross section The angle that the line at arc groove (1010) two ends and rotor hole (801) center is constituted is changed with rotor (1) from safe condition The angle that need to be rotated during for arm-to-arm is identical.
4. formula interrupter is constrained according to the memorial alloy according to any one of claims 1 to 3 based on inertia, wherein, institute It is 75 °~135 ° to state the angle between arc groove (1010) two ends and rotor (1) axis.
5. formula interrupter is constrained according to the memorial alloy according to any one of claims 1 to 4 based on inertia, wherein, The 4th blind hole (104) is further opened with the end face of rotor (1) the correspondence body (8), for housing locking member (5), accordingly The ball pin hole (805) of corresponding matching is offered on ground, the body (8);
The locking member (5) includes Lock spring (502) and ball pin (501), in the secure state, Lock spring (502) place In contraction state, ball pin (501) end and rotor hole (801) end contact of the body (8), rotor (1) is from safety When state turns to arm-to-arm, the 4th blind hole (104) just aligns with the ball pin hole (805), i.e., described sticking department Lock spring (502) compressive state of part (5) is released, and ball pin (501) is inserted pending so as to lock this in the ball pin hole (805) State.
6. formula interrupter is constrained according to the memorial alloy according to any one of claims 1 to 5 based on inertia, wherein, institute Stating inertial elements part (3) includes inertia cylinder (301) and inertial spring (302), and one end of the inertia cylinder (301) is offered admittedly The groove of fixed described inertial spring (302) one end;
In the secure state, the inertia cylinder (301) is placed in the 3rd blind hole on the side end face of rotor (1) one (106) in, the other end of the inertial spring (302) is placed in first blind hole (803) on the body (8);Institute State rotor (1) to turn to during arm-to-arm from safe condition, the inertial spring (302) is in compressive state and described used Property securing member (3) integrally in embedded described first blind hole (803);When the rotor (1) turns to arm-to-arm, described first Blind hole (803) is aligned with the pin hole (107) on the rotor (1), the embedded pin hole of inertia cylinder (301) (107) to lock the arm-to-arm in.
7. formula interrupter is constrained according to the memorial alloy according to any one of claims 1 to 6 based on inertia, wherein, institute Stating memorial alloy pin removal (9) includes pin (901), limit spring (902), pressure spiral shell (903), housing (904) and memorial alloy Sleeve (905);
The pin (901) is T-shaped structure, and its front end is the latch ends of the memorial alloy pin removal (9), the limit spring (902) it is set in the latch ends;
Step groove is offered on one side end face of the housing (904), its exit is offered the pressure spiral shell of through hole by middle part (903) encapsulate, step groove is equipped with the memorial alloy sleeve (905), the pin in original state successively from bottom to top Sub (901), the limit spring (902), and the memorial alloy sleeve (905) are placed on the ladder in step groove, under it Fang Liuyou can house the hollow space of pin (901) rear end;
The memorial alloy sleeve (905) is hollow sleeve tubular, and the pin (901) and limit spring (902) are placed in sleeve It is interior, and the bottom of the memorial alloy sleeve (905) is provided with for limiting the pin (901) position in an initial condition Remember step;
In the secure state, the bottom of the memorial alloy sleeve (905) has memory step, constrains the limit spring (902) compressive state is in, and the latch ends of the pin (901) are stretched out from the through hole on the pressure spiral shell (903), it is embedded described To lock the safe condition in pin hole (107) on rotor (1);The rotor (1) is converted to arm-to-arm from safe condition When, the memorial alloy pin removal (9) is powered, and the memory step of memorial alloy sleeve (905) bottom disappears, and relieves institute Constraint of the memorial alloy sleeve (905) to the pin (901) is stated, the compressive state of the limit spring (902) is released, relied on Recover elastic force to detach the latch ends of the pin (901) from the pin hole (107), release the lock to the rotor (1) It is fixed.
CN201710498538.3A 2017-06-27 2017-06-27 A kind of memorial alloy constraint formula interrupter based on inertia Active CN107144186B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023277816A3 (en) * 2021-06-29 2023-03-02 St Engineering Advanced Material Engineering Pte. Ltd. Safe-and-arm device

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US20140131508A1 (en) * 2006-09-29 2014-05-15 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
CN104677204A (en) * 2015-02-13 2015-06-03 湖北三江航天红林探控有限公司 Fuze isolation mechanism
CN204461248U (en) * 2015-02-13 2015-07-08 湖北三江航天红林探控有限公司 A kind of interrupter mechanism

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Publication number Priority date Publication date Assignee Title
DE3126289C2 (en) * 1981-07-03 1988-05-26 Diehl Gmbh & Co, 8500 Nuernberg, De
US20140131508A1 (en) * 2006-09-29 2014-05-15 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
CN104677204A (en) * 2015-02-13 2015-06-03 湖北三江航天红林探控有限公司 Fuze isolation mechanism
CN204461248U (en) * 2015-02-13 2015-07-08 湖北三江航天红林探控有限公司 A kind of interrupter mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023277816A3 (en) * 2021-06-29 2023-03-02 St Engineering Advanced Material Engineering Pte. Ltd. Safe-and-arm device

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