CN212158327U - A release and insert mechanism that is used for between rocket bomb and launching tube - Google Patents
A release and insert mechanism that is used for between rocket bomb and launching tube Download PDFInfo
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- CN212158327U CN212158327U CN202020807541.6U CN202020807541U CN212158327U CN 212158327 U CN212158327 U CN 212158327U CN 202020807541 U CN202020807541 U CN 202020807541U CN 212158327 U CN212158327 U CN 212158327U
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Abstract
The utility model belongs to the technical field of rocket projectile launcher, concretely relates to take off and insert mechanism that is used for between rocket projectile and the launching tube. The technical scheme is as follows: a disengaging and inserting mechanism used between a rocket projectile and a launching tube comprises a guide plate and a plug mechanism, wherein the guide plate is provided with a guiding chute and a guiding chute respectively; the guide plate is fixed on the launching tube, and a wedge-shaped groove matched with the vertical pin mechanism is formed in the rocket projectile. The utility model provides a can reliably realize taking off the inserting mechanism that takes off between rocket projectile and the launching tube of inserting automatically.
Description
Technical Field
The utility model belongs to the technical field of rocket projectile launcher, concretely relates to take off and insert mechanism that is used for between rocket projectile and the launching tube.
Background
Before the rocket projectile is launched, ground power supply, parameter setting and other controls need to be carried out on the rocket projectile, a circuit needs to be disconnected in time during launching, and a mechanism for bearing the function in the launching device is a disengaging and inserting mechanism. If the connection between the plug in the disengaging and inserting mechanism and the rocket projectile is unreliable, the rocket projectile cannot normally work before being launched, and the flight of the rocket projectile is influenced; if the plug is not reliably separated from the rocket projectile, the socket on the rocket projectile can be damaged, the circuit is short-circuited, and the launching failure can be caused in serious cases, so that the plug-in and release mechanism is an important component on the launching tube.
The existing inserting and extracting mechanism is difficult to realize reliable automatic inserting and extracting.
SUMMERY OF THE UTILITY MODEL
In order to solve the problems existing in the prior art, the utility model aims to provide a can reliably realize that the automatic taking off is inserted and is used for taking off between rocket projectile and the launching tube and insert the mechanism.
The utility model discloses the technical scheme who adopts does:
a disengaging and inserting mechanism used between a rocket projectile and a launching tube comprises a guide plate and a plug mechanism, wherein the guide plate is provided with a guiding chute and a guiding chute respectively; the guide plate is fixed on the launching tube, and a wedge-shaped groove matched with the vertical pin mechanism is formed in the rocket projectile.
Preferably, in the moving direction of the rocket projectile, the guiding chute inclines towards the direction close to the rocket projectile, and the guiding chute inclines towards the direction far away from the rocket projectile.
Preferably, the vertical pin mechanism comprises a vertical pin, the vertical pin is sleeved in the vertical pin hole, the locking hole is formed in the vertical pin, and a vertical spring is connected between the vertical pin and the base body.
Preferably, erect and be provided with spacing step in the pinhole, erect the round pin including gag lever post, intermediate lever and the bolt pole that sets gradually, the locking hole sets up on the gag lever post, is equipped with intermediate lever post between bolt pole and the intermediate lever, and the gag lever post is located one side that rocket projectile was kept away from to spacing step, and vertical spring housing is located on the intermediate lever post, and vertical spring is located between spacing step and the intermediate lever post.
Preferably, the transverse pin mechanism comprises a transverse pin, the transverse pin is sleeved in the transverse pin hole, a transverse spring is connected between the transverse pin and the base body, the transverse pin hole is communicated with the vertical pin hole, and one end of the transverse pin penetrates into the locking hole during locking.
Preferably, the transverse pin hole is internally provided with a baffle ring, the transverse pin comprises a locking rod, a connecting rod and a stop block which are sequentially arranged, one end of the locking rod penetrates into the locking hole during locking, a connecting step is arranged between the locking rod and the connecting rod, the connecting rod is sleeved with a transverse spring, and the transverse spring is arranged between the baffle ring and the connecting step.
Preferably, still be provided with a plurality of data connector on the base member, be provided with on the rocket projectile with data connector complex data connection hole.
Preferably, the distance between the leading step and the leading step is the same as the length of the leading slide bar, and the leading slide bar are symmetrically arranged and have the same length.
Preferably, the quantity of deflector is two, sets up the opening on the rocket tube, and two deflectors are fixed in the open-ended both sides respectively, and the both sides of base member all set up and lead in the sliding strip and lead out the sliding strip.
Preferably, one end of the guiding chute facing the guiding chute and one end of the guiding chute facing the guiding chute are both provided with a rounding.
The utility model has the advantages that:
1. the utility model discloses a be provided with on the deflector and lead into the spout and derive the spout, the in-process of pegging graft, lead into the slip strip cover and locate to lead into the spout, erect the round pin mechanism and stretch out this moment. When the rocket projectile is pushed in, the vertical pin mechanism is contacted with the shell of the rocket projectile; when the rocket projectile is pushed to the wedge-shaped groove, the lower end of the vertical pin mechanism falls into the wedge-shaped groove. The rocket projectile is continuously pushed, and the plug mechanism moves along with the rocket projectile. When the plug mechanism moves to the lowest end of the guide sliding groove, the plug mechanism is separated from the guide sliding groove, and at the moment, the rocket projectile is filled in place and the plug mechanism is inserted in place. When the vertical pin mechanism is lowered to a certain position, the transverse pin mechanism can penetrate into the locking hole, and then the vertical pin mechanism is locked. When the rocket is launched, the rocket drives the plug mechanism to move forwards, the guide-out sliding strip slides in the guide-out sliding groove, and then the plug mechanism can be automatically separated from the rocket projectile. At the moment, the vertical pin mechanism is locked by the transverse pin mechanism, and the vertical pin mechanism cannot block the rocket projectile. To sum up, the utility model discloses a take off and insert mechanism can peg graft automatically and take off and insert, and take off and insert the mechanism and remove the time can accurately be connected or throw off with the rocket bomb, use reliably.
2. Because on the moving direction of rocket projectile, the guide sliding groove inclines towards the direction close to the rocket projectile, then the in-process of installing the rocket projectile, the guide sliding strip slides in the guide sliding groove, and the plug mechanism is close to the rocket projectile and is spliced in the rocket projectile. Because the derivation spout is towards the direction slope of keeping away from the rocket projectile, then the in-process of launching the rocket projectile, derives the slip strip and slides in deriving the spout, and plug mechanism keeps away from the rocket projectile and takes off in the rocket projectile and inserts. Therefore, the plug mechanism is reliably inserted and disconnected with the rocket projectile, the condition that the rocket projectile flies is influenced because the plug mechanism cannot normally work before being connected with the rocket projectile when the plug mechanism is not reliably connected with the rocket projectile is avoided, and the condition that the launching fails because a socket on the rocket projectile is damaged and a circuit is short-circuited when the plug is not reliably separated from the rocket projectile is also avoided.
3. In the process of installing the rocket projectile, the vertical pin extends out under the action of the vertical spring, and the lower end of the vertical pin can be reliably inserted into the wedge-shaped groove of the rocket projectile.
4. The limiting step can block the limiting rod, and the vertical pin cannot fall from the vertical pin hole. The vertical spring is positioned between the limiting step and the middle step, when the transverse pin mechanism is not inserted into the locking hole, the vertical spring can accurately push the plug pin rod, and the vertical pin can be accurately inserted into the wedge-shaped groove of the rocket projectile.
5. In the process of installing the rocket projectile, the guide sliding strip slides in the guide sliding groove, and then the plug mechanism gradually approaches the rocket projectile. Therefore, the rocket projectile can push the vertical pin mechanism to move reversely, and when the locking hole of the vertical pin mechanism is aligned with the transverse pin, the transverse pin penetrates into the locking hole under the pushing of the transverse spring, so that the vertical pin mechanism can be reliably locked. When the rocket projectile is launched, the vertical pin mechanism is in a locking state, and after the rocket projectile moves for a certain distance, the vertical pin mechanism can be thoroughly separated from the surface of the rocket projectile and cannot generate friction with the rocket projectile.
6. The dog is located beyond the transverse pin hole, makes things convenient for reuse the utility model discloses the time-spent locking hole of will seting out the transverse pin through the dog. The transverse spring is arranged between the baffle ring and the connecting step, so that the transverse spring is reliably connected, and when the locking hole is aligned with the transverse pin, the transverse pin spring can timely push the locking rod into the locking hole, and reliable locking is guaranteed.
7. In the process of installing the rocket projectile, the lower end of the vertical pin mechanism is inserted into the wedge-shaped groove, and the data connector on the base body is inserted into the data connecting hole of the rocket projectile, so that data transmission is guaranteed.
8. The interval between leading step and the derivation step is the same with the length of leading into the sliding strip, and leads into the sliding strip and set up and length the same with the symmetry of deriving the sliding strip, then when leading into the sliding strip and just deviate from the guide and advance the spout, the front end of deriving the sliding strip just is located the entrance of deriving the spout, has guaranteed to derive the sliding strip and has got into smoothly when launching rocket projectile and derive the spout.
9. The guide plates are arranged on the two sides of the plug mechanism, so that the two sides of the plug mechanism can be guided, the stability of the plug mechanism in the moving process is improved, the situation that the plug mechanism is blocked or released from the guide plates is avoided, and the use reliability of the release and insertion mechanism is ensured.
10. The one end of leading the spout orientation and deriving the spout and the one end of deriving the spout orientation and leading the spout all are equipped with the radius, then lead the sliding strip and can roll off more smoothly and lead the spout, and derive the sliding strip and can slide in more smoothly and derive the spout.
The advantages of the invention are not limited to the description, but rather are described in greater detail in the detailed description for better understanding.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention. The objectives and other advantages of the invention may be realized and attained by the structure particularly pointed out in the written description and drawings.
It will be appreciated by those skilled in the art that the objects and advantages that can be achieved with the present invention are not limited to the details set forth above, and that these and other objects that can be achieved with the present invention will be more clearly understood from the following detailed description.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the structure of the guide plate;
FIG. 3 is a schematic structural view of a plug mechanism;
FIG. 4 is an assembly view of the present invention with a rocket projectile and launch canister;
FIG. 5 is an enlarged view of a portion of FIG. 4 at A;
FIG. 6 is a cross-sectional view of the present invention assembled with a rocket projectile and launch canister;
fig. 7 is a partially enlarged view at B in fig. 6.
In the figure: 1-a guide plate; 2-a substrate; 3-a vertical pin mechanism; 4-a cross pin mechanism; 5-locking holes; 6-a launch canister; 7-rocket projectile; 11-a guide chute; 12-a lead-out chute; 21-guiding in the sliding bar; 22-leading out a sliding bar; 23-vertical pin holes; 24-transverse pin holes; 25-a data connector; 31-a vertical pin; 32-vertical springs; 41-transverse pin; 42-transverse spring; 71-wedge-shaped grooves; 72-data connection hole; 231-a limit step; 241-baffle ring; 311-a limiting rod; 312-a middle rod; 313-a latch rod; 411-a locking lever; 412-a connecting rod; 413-stop.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implying any number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
As shown in fig. 1 to 7, the detaching and inserting mechanism for a rocket projectile and a launch canister of the present embodiment includes a guide plate 1 and a plug mechanism, the guide plate 1 is provided with a guide chute 11 and a guide chute 12, the plug mechanism includes a base body 2, the base body 2 is provided with a guide sliding bar 21 and a guide sliding bar 22, the base body 2 is provided with a vertical pin hole 23 and a horizontal pin hole 24, the vertical pin hole 23 is sleeved with a vertical pin mechanism 3, the horizontal pin hole 24 is sleeved with a horizontal pin mechanism 4, the vertical pin mechanism 3 is provided with a locking hole 5, and one end of the horizontal pin mechanism 4 penetrates into the locking hole 5 during locking; the guide plate 1 is fixed on the launching tube 6, and the rocket projectile 7 is provided with a wedge-shaped groove 71 matched with the vertical pin mechanism 3.
The utility model discloses a be provided with on deflector 1 and lead into spout 11 and derive spout 12, the in-process of pegging graft, lead into the 21 covers of slide bar and locate to lead into spout 11 in, erect round pin mechanism 3 this moment and stretch out. When the rocket projectile 7 is pushed in, the vertical pin mechanism 3 is contacted with the shell of the rocket projectile 7; when pushed to the wedge groove 71 of the rocket projectile 7, the lower end of the vertical pin mechanism 3 falls into the wedge groove 71. The rocket projectile 7 continues to be pushed in, and the plug mechanism moves along with the rocket projectile 7. When the plug mechanism moves to the lowest end of the guide chute 11, the plug mechanism is separated from the guide chute 11, and at the moment, the rocket projectile 7 is filled in place and the plug mechanism is inserted in place. When the vertical pin mechanism 3 is lowered to a certain position, the transverse pin mechanism 4 can penetrate into the locking hole 5, and then the vertical pin mechanism 3 is locked. When the rocket is launched, the rocket drives the plug mechanism to move forwards, the guide-out sliding strip 22 slides in the guide-out sliding groove 12, and then the plug mechanism can be automatically separated from the rocket projectile 7. At this time, the vertical pin mechanism 3 is locked by the horizontal pin mechanism 4, and the vertical pin mechanism 3 does not block the rocket projectile 7. To sum up, the utility model discloses a take off and insert the mechanism and can peg graft automatically and take off and insert, and take off and insert the mechanism and can accurately be connected with rocket projectile 7 or throw off when removing, use reliably.
In the moving direction of the rocket projectile 7, the guiding chute 11 is inclined toward the direction close to the rocket projectile 7, and the guiding chute 12 is inclined toward the direction away from the rocket projectile 7. Because in the moving direction of rocket projectile 7, guide chute 11 inclines towards the direction close to rocket projectile 7, in the process of installing rocket projectile 7, guide sliding bar 21 slides in guide chute 11, and plug mechanism is close to rocket projectile 7 and is spliced in rocket projectile 7. Because the derivation chute 12 inclines towards the direction far away from the rocket projectile 7, in the process of launching the rocket projectile 7, the derivation sliding strip 22 slides in the derivation chute 12, and the plug mechanism is far away from the rocket projectile 7 and is separated from and inserted into the rocket projectile 7. Therefore, the plug-in connection and the disconnection of the plug mechanism and the rocket projectile 7 are reliable, the situation that the rocket projectile 7 flies is influenced because the plug mechanism cannot normally work before being connected with the rocket projectile 7 when the plug mechanism and the rocket projectile 7 are not reliable is avoided, and the situation that the plug and the rocket projectile 7 are not reliable in separation is also avoided, the socket on the rocket projectile 7 is damaged, the circuit is short-circuited, and the launching failure can be caused when the circuit is serious.
Specifically, the vertical pin mechanism 3 includes a vertical pin 31, the vertical pin 31 is sleeved in the vertical pin hole 23, the locking hole 5 is arranged on the vertical pin 31, and a vertical spring 32 is connected between the vertical pin 31 and the base body 2. In the process of installing the rocket projectile 7, the vertical pin 31 extends out under the action of the vertical spring 32, and the lower end of the vertical pin 31 can be reliably inserted into the wedge-shaped groove 71 of the rocket projectile 7.
Furthermore, be provided with spacing step 231 in the vertical pin hole 23, vertical pin 31 is including gag lever post 311, intermediate lever 312 and the bolt pole 313 that sets gradually, and locking hole 5 sets up on gag lever post 311, is equipped with intermediate step between bolt pole 313 and the intermediate lever 312, and gag lever post 311 is located one side that rocket projectile 7 was kept away from to spacing step 231, and vertical spring 32 overlaps on locating intermediate lever 312, and vertical spring 32 is located between spacing step 231 and the intermediate step. The stop step 231 can block the stop rod 311, so that the vertical pin 31 will not fall out of the vertical pin hole 23. The vertical spring 32 is located between the limit step 231 and the middle step, and when the transverse pin mechanism 4 is not inserted into the locking hole 5, the vertical spring 32 can accurately push the latch rod 313, and the vertical pin 31 can be accurately inserted into the wedge-shaped groove 71 of the rocket projectile 7.
Specifically, the transverse pin mechanism 4 includes a transverse pin 41, the transverse pin 41 is sleeved in the transverse pin hole 24, a transverse spring 42 is connected between the transverse pin 41 and the substrate 2, the transverse pin hole 24 is communicated with the vertical pin hole 23, and one end of the transverse pin 41 penetrates into the locking hole 5 during locking. In the process of installing the rocket projectile 7, the guiding sliding bar 21 slides in the guiding sliding groove 11, and the plug mechanism gradually approaches the rocket projectile 7. Therefore, the rocket projectile 7 pushes the vertical pin mechanism 3 to move reversely, and when the locking hole 5 of the vertical pin mechanism 3 is aligned with the transverse pin 41, the transverse pin 41 penetrates into the locking hole 5 under the pushing of the transverse spring 42, and the vertical pin mechanism 3 can be locked reliably. When the rocket projectile 7 is launched, the vertical pin mechanism 3 is in a locked state, and after the rocket projectile 7 moves for a certain distance, the vertical pin mechanism 3 can be completely separated from the surface of the rocket projectile 7 and cannot generate friction with the rocket projectile 7.
Furthermore, a blocking ring 241 is arranged in the transverse pin hole 24, the transverse pin 41 comprises a locking rod 411, a connecting rod 412 and a stopper 413 which are arranged in sequence, one end of the locking rod 411 penetrates through the locking hole 5 during locking, a connecting step is arranged between the locking rod 411 and the connecting rod 412, the connecting rod 412 is sleeved with the transverse spring 42, and the transverse spring 42 is arranged between the blocking ring 241 and the connecting step. The stop 413 is located outside the transverse pin hole 24, so that the utility model can be used again conveniently, and the transverse pin 41 is pulled out of the locking hole 5 through the stop 413. The transverse spring 42 is arranged between the baffle ring 241 and the connecting step, so that the transverse spring 42 is reliably connected, and when the locking hole 5 is aligned with the transverse pin 41, the transverse pin 41 can push the locking rod 411 into the locking hole 5 in time by the spring, and reliable locking is ensured.
Furthermore, a plurality of data connectors 25 are arranged on the base body 2, and data connecting holes 72 matched with the data connectors 25 are arranged on the rocket projectile 7. In the process of installing the rocket projectile 7, the lower end of the vertical pin mechanism 3 is inserted into the wedge-shaped groove 71, and the data connector 25 on the base body 2 is inserted into the data connecting hole 72 of the rocket projectile 7, so that the connection reliability of the plug mechanism and the rocket projectile 7 is further improved, and the situation that the rocket projectile 7 cannot normally work before being launched and the flying of the rocket projectile 7 is influenced when the plug in the disconnecting and inserting mechanism is not reliably connected with the rocket projectile 7 is avoided.
The distance between the leading-in step and the leading-out step is the same as the length of the leading-in sliding strip 21, and the leading-in sliding strip 21 and the leading-out sliding strip 22 are symmetrically arranged and have the same length. The interval between the leading-in step and the leading-out step is the same with the length of leading-in sliding strip 21, and the symmetry setting and the length of leading-in sliding strip 21 and leading-out sliding strip 22 are the same, and then when leading-in sliding strip 21 just deviate from leading-in spout 11, the front end of leading-out sliding strip 22 just lies in the entrance of leading-out spout 12, has guaranteed to derive sliding strip 22 and has got into smoothly when launching rocket projectile 7 and derive spout 12.
Furthermore, the quantity of deflector 1 is two, sets up the opening on the rocket tube, and two deflectors 1 are fixed in the open-ended both sides respectively, and the both sides of base member 2 all set up and lead in slide bar 21 and lead out slide bar 22. The guide plates 1 are arranged on the two sides of the plug mechanism, so that the two sides of the plug mechanism can be guided, the stability of the plug mechanism in the moving process is improved, the situation that the plug mechanism is blocked or released from the guide plates 1 is avoided, and the use reliability of the release and insertion mechanism is ensured.
Furthermore, the end of the guiding chute 11 facing the guiding chute 12 and the end of the guiding chute 12 facing the guiding chute 11 are both provided with a radius. One end of the guiding chute 11 facing the guiding chute 12 and one end of the guiding chute 12 facing the guiding chute 11 are both provided with a rounding, so that the guiding sliding strip 21 can slide out of the guiding chute 11 more smoothly, and the guiding sliding strip 22 can slide into the guiding chute 12 more smoothly.
The working principle is as follows:
inserting and connecting action: the guiding sliding bar 21 is sleeved in the guiding chute 11, and the vertical pin 31 extends under the pushing of the vertical spring 32. When the rocket projectile 7 is pushed in, the vertical pin mechanism 3 is contacted with the shell of the rocket projectile 7; when pushed to the wedge groove 71 of the rocket projectile 7, the lower end of the vertical pin 31 falls into the wedge groove 71. The rocket projectile 7 continues to be pushed in, and the plug mechanism moves along with the rocket projectile 7. When the plug mechanism moves to the lowest end of the guide chute 11, the plug mechanism is separated from the guide chute 11, and at the moment, the rocket projectile 7 is filled in place and the plug mechanism is inserted in place. When the vertical pin 31 is lowered to a certain position, the horizontal pin 41 will be inserted into the locking hole 5 under the action of the horizontal spring 42, and the vertical pin 31 is locked.
And (3) disengaging and inserting action: the rocket drives the plug mechanism to move forward, the guiding-out sliding strip 22 slides in the guiding-out sliding groove 12, and then the plug mechanism can be automatically separated from the rocket projectile 7. At this time, the vertical pin 31 is locked by the horizontal pin 41, and the vertical pin 31 does not block the rocket projectile 7.
The present invention is not limited to the above-mentioned optional embodiments, and any other products in various forms can be obtained by anyone under the teaching of the present invention, and any changes in the shape or structure thereof, all the technical solutions falling within the scope of the present invention, are within the protection scope of the present invention.
Claims (10)
1. The utility model provides a take off and insert mechanism that is used for between rocket bomb and launch canister which characterized in that: the plug device comprises a guide plate (1) and a plug mechanism, wherein the guide plate (1) is provided with a guide sliding groove (11) and a guide sliding groove (12), the plug mechanism comprises a base body (2), the base body (2) is provided with a guide sliding strip (21) and a guide sliding strip (22), a vertical pin hole (23) and a transverse pin hole (24) are arranged in the base body (2), a vertical pin mechanism (3) is sleeved in the vertical pin hole (23), a transverse pin mechanism (4) is sleeved in the transverse pin hole (24), a locking hole (5) is arranged in the vertical pin mechanism (3), and one end of the transverse pin mechanism (4) penetrates into the locking hole (5) during locking; the guide plate (1) is fixed on the launching tube (6), and the rocket projectile (7) is provided with a wedge-shaped groove (71) matched with the vertical pin mechanism (3).
2. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: in the moving direction of the rocket projectile (7), the guiding chute (11) inclines towards the direction close to the rocket projectile (7), and the guiding chute (12) inclines towards the direction far away from the rocket projectile (7).
3. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: the vertical pin mechanism (3) comprises a vertical pin (31), the vertical pin (31) is sleeved in the vertical pin hole (23), the locking hole (5) is formed in the vertical pin (31), and a vertical spring (32) is connected between the vertical pin (31) and the base body (2).
4. A release and insertion mechanism for a rocket projectile and a launch barrel according to claim 3, wherein: be provided with spacing step (231) in erecting pinhole (23), erect round pin (31) including gag lever post (311), intermediate lever (312) and bolt pole (313) that set gradually, locking hole (5) set up on gag lever post (311), be equipped with intermediate lever post (313) between bolt pole (313) and intermediate lever (312), gag lever post (311) are located one side that rocket projectile (7) was kept away from in spacing step (231), vertical spring (32) cover is located on intermediate lever (312), vertical spring (32) are located between spacing step (231) and the intermediate lever.
5. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: the transverse pin mechanism (4) comprises a transverse pin (41), the transverse pin (41) is sleeved in a transverse pin hole (24), a transverse spring (42) is connected between the transverse pin (41) and the base body (2), the transverse pin hole (24) is communicated with a vertical pin hole (23), and one end of the transverse pin (41) penetrates into a locking hole (5) during locking.
6. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 5, wherein: be provided with in horizontal pinhole (24) and keep off ring (241), horizontal round pin (41) are including check lock lever (411), connecting rod (412) and dog (413) that set gradually, and the one end of check lock lever (411) penetrates check lock hole (5) during locking, is equipped with between check lock lever (411) and connecting rod (412) and connects the step, and connecting rod (412) are located to horizontal spring (42) cover on, and horizontal spring (42) set up between keeping off ring (241) and connecting the step.
7. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: still be provided with a plurality of data connector (25) on base member (2), be provided with on rocket projectile (7) with data connector (25) complex data connection hole (72).
8. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: the distance between the leading-in step and the leading-out step is the same as the length of the leading-in sliding strip (21), and the leading-in sliding strip (21) and the leading-out sliding strip (22) are symmetrically arranged and have the same length.
9. The release and insertion mechanism for use between a rocket projectile and a launch barrel of claim 1, wherein: the quantity of deflector (1) is two, sets up the opening on the rocket tube, and open-ended both sides are fixed in respectively in two deflector (1), and the both sides of base member (2) all set up and lead into slide bar (21) and derive slide bar (22).
10. The release and insertion mechanism for a rocket projectile and a launch barrel according to any one of claims 1 to 9, wherein: one end of the guiding chute (11) facing the guiding chute (12) and one end of the guiding chute (12) facing the guiding chute (11) are both provided with a rounding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020807541.6U CN212158327U (en) | 2020-05-14 | 2020-05-14 | A release and insert mechanism that is used for between rocket bomb and launching tube |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020807541.6U CN212158327U (en) | 2020-05-14 | 2020-05-14 | A release and insert mechanism that is used for between rocket bomb and launching tube |
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| Publication Number | Publication Date |
|---|---|
| CN212158327U true CN212158327U (en) | 2020-12-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020807541.6U Active CN212158327U (en) | 2020-05-14 | 2020-05-14 | A release and insert mechanism that is used for between rocket bomb and launching tube |
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| CN (1) | CN212158327U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114678729A (en) * | 2022-03-07 | 2022-06-28 | 上海机电工程研究所 | Guided missile cross double-pulling plate type electric plug falling mechanism |
| CN114719675A (en) * | 2022-03-09 | 2022-07-08 | 上海机电工程研究所 | Plug-in mechanism and solid bullet ware synchronous unlocking mechanism |
-
2020
- 2020-05-14 CN CN202020807541.6U patent/CN212158327U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114678729A (en) * | 2022-03-07 | 2022-06-28 | 上海机电工程研究所 | Guided missile cross double-pulling plate type electric plug falling mechanism |
| CN114678729B (en) * | 2022-03-07 | 2023-11-17 | 上海机电工程研究所 | Missile cross double-shifting plate type electric plug falling mechanism |
| CN114719675A (en) * | 2022-03-09 | 2022-07-08 | 上海机电工程研究所 | Plug-in mechanism and solid bullet ware synchronous unlocking mechanism |
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