CN107270770B - A kind of guided missile rear support guiding device for firing box - Google Patents
A kind of guided missile rear support guiding device for firing box Download PDFInfo
- Publication number
- CN107270770B CN107270770B CN201710618701.5A CN201710618701A CN107270770B CN 107270770 B CN107270770 B CN 107270770B CN 201710618701 A CN201710618701 A CN 201710618701A CN 107270770 B CN107270770 B CN 107270770B
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- Prior art keywords
- guided missile
- limit
- rail
- guide rail
- pedestal
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
Abstract
The present invention relates to a kind of guided missile rear support guiding devices for firing box, including the pedestal and the parallel left rail and right guide rail being fixed on pedestal being arranged along the longitudinal direction, the rear end of pedestal is equipped with rear limit assembly for being limited to guided missile rear slider, and the rear end of left rail and right guide rail is correspondingly provided with left limit component and right limit component for being limited to guided missile rear slider.It has the advantages that structure simple, manipulation convenience, functional, highly-safe, the functions such as support, limit, guiding can be provided during missile transport and outlet, and be not necessarily to unlock in MISSILE LAUNCHING and operate, reduce the operating procedure before emitting.
Description
Technical field
The present invention relates to a kind of support devices, have and are related to a kind of guided missile rear support guiding device for firing box, belong to
In MISSILE LAUNCHING technical field.
Background technique
With the development of tactical missile weapon system, the weight and size of guided missile are increasing, this is to MISSILE LAUNCHING
Device proposes more functional requirements.Firing box as guided missile launcher need to collect storage, transport and emission function in
One.The many factors such as support guide, locking limit, production assembly should be fully considered by designing at it in preparation process, to meet
Storage, transport and the mission need of guided missile.But existing firing box and associated transmissions device exist multi-functional integrated insufficient, raw
Produce the problems such as assembly is complicated, operation control is cumbersome, safety is lower.
Summary of the invention
The object of the present invention is to provide a kind of guided missile rear support guiding device for firing box, simple with structure,
Convenience, functional, highly-safe advantage are manipulated, support, limit, guiding etc. can be provided during missile transport and outlet
Function, and in MISSILE LAUNCHING without unlocking operation, the operating procedure before reducing transmitting.
To solve the above problem in the prior art, a kind of guided missile rear support guiding for firing box provided by the invention
Device, the left rail and right guide rail being fixed on pedestal including the pedestal that is arranged along the longitudinal direction and in parallel, the pedestal
Rear end is equipped with rear limit assembly for being limited to guided missile rear slider, and the rear end of the left rail and right guide rail is correspondingly provided with
Left limit component and right limit component for being limited to guided missile rear slider.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the left rail and the right side
Guide rail structure is identical and symmetrical distribution, and left rail includes bottom left, left side and left top, bottom left, left side and
Left guide groove is formed between left top, right guide rail includes right bottom, right side and right top, right bottom, right side and right top
Between form right guide groove.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein limit assembly after described
Including fixed frame and the rear limited block being set on fixed frame；Limit assembly leads to respectively after limit assembly is equipped with two groups, two groups afterwards
Fixed frame is crossed to fix on the base and correspond with the rear end of left rail and right guide rail, the rear limited block of limit assembly after two groups
Front end is equipped with by preceding the inclined scarf under rear.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the fixed frame includes
Bottom plate and the supporting plate for being fixed on bottom plate front end, the cross that the rear limited block includes vertical part and is fixed on vertical part upper end and forward extends out
Portion；The vertical part of limited block is placed on the bottom plate of fixed frame and is connect by attachment screw with supporting plate afterwards, on the rear limited block
The front end of transverse part is arranged in scarf.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the bottom of the fixing seat
Sliding slot along the longitudinal direction is offered on plate, it is sliding to be equipped with the inverted " t " font being placed in sliding slot on the downside of the vertical part of the rear limited block
Block.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the left limit component
Including left limit block, left holding screw and left locking nut, the left limit block is solid by left holding screw and left locking nut
It is scheduled on left rail, and is in the inner end of left limit block on the upside of the bottom left of left rail, pass through the inner end of left holding screw
The left side of left rail；The right limit component includes right limit block, right holding screw and right locking nut, the right limit block
It is fixed on right guide rail by right holding screw and right locking nut, and the inner end of right limit block is made to be in the right bottom of right guide rail
Upside makes the inner end of right holding screw pass through the right side of right guide rail.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein further include being fixed on base
The bullet locking mechanism mounting base of base rear end.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the pedestal includes cutting
Face is the rack of "Ji" type, and the inside of rack is equipped with the multiple interior reinforcing ribs being spaced apart along its length, the left side of pedestal
The multiple external reinforcing ribs being spaced apart along its length are equipped with right side.
Further, a kind of guided missile rear support guiding device for firing box of the present invention, wherein the top of the rack
The multiple through-holes being spaced apart along its length are offered on plate, left plate and right side plate.
A kind of guided missile rear support guiding device for firing box of the present invention compared with prior art, has the advantage that
Pedestal and the parallel left rail and right guide rail that are fixed on pedestal on of the present invention by setting along the longitudinal direction, and in pedestal
The rear limit assembly for being limited to guided missile rear slider is arranged in rear end, is correspondingly arranged use in the rear end of left rail and right guide rail
In the left limit component and right limit component that are limited to guided missile rear slider.Thus just constitute that a kind of structure is simple, manipulation
Convenience, functional, the highly-safe guided missile rear support guiding device for firing box.It in practical applications, will be of the invention
It is fixed in firing box by pedestal, guided missile is slid by guided missile rear slider by front end to the guide groove of left rail and right guide rail
In.In storage and transportational process, rear side limit is carried out to guided missile rear slider by rear limit assembly, by left limit component and
Right limit component carries out left side limit to guided missile rear slider and right side limits, while the bullet locking mechanism by being set in firing box
Limit is carried forward to guided missile rear slider, the purpose limited comprehensively to guided missile rear slider can be realized, ensure that guided missile is store
It deposits and the safety in transportational process；In Missile Launching Process, by the cooperation of guided missile rear slider and left rail and right guide rail,
Support guide effect can be provided guided missile, ensure that the safety of guided missile outlet in emission process.And the present invention by will after
The rear end of pedestal is arranged in limit assembly, after left limit component and right limit component are correspondingly arranged at left rail and right guide rail
End, and the bullet locking mechanism by being set in firing box is carried forward limit to guided missile rear slider, this arrangement only needs
Bullet locking mechanism unlock, without being unlocked operation to rear limit assembly, left limit component and right limit component, can meet and lead
Launching condition is played, the operating procedure before not only reducing transmitting, and interference effect will not be caused to guided missile outlet, have higher
Safety.
The shown specific embodiment guided missile rear support for firing box a kind of to the present invention is oriented to dress with reference to the accompanying drawing
It sets and is described in further detail:
Detailed description of the invention
Fig. 1 is a kind of perspective view of the guided missile rear support guiding device for firing box of the present invention；
Fig. 2 is a kind of top view of the guided missile rear support guiding device for firing box of the present invention；
Fig. 3 is a kind of front view of the guided missile rear support guiding device for firing box of the present invention；
Fig. 4 is a kind of left view enlarged drawing of the guided missile rear support guiding device for firing box of the present invention；
Fig. 5 is a kind of right view enlarged drawing of the guided missile rear support guiding device for firing box of the present invention；
Fig. 6 is the enlarged diagram of location A in Fig. 1；
Fig. 7 is the enlarged diagram of B location in Fig. 2；
Fig. 8 is C-C in Fig. 7 to enlarged diagram；
Fig. 9 is D-D in Fig. 7 to enlarged diagram；
Figure 10 to Figure 12 be in a kind of guided missile rear support guiding device for firing box of the present invention after limit assembly with lead
Play the connection relationship diagram of rear slider；
Figure 13 to Figure 15 is left limit component and the right side in a kind of guided missile rear support guiding device for firing box of the present invention
The connection relationship diagram of limit assembly and guided missile rear slider.
Specific embodiment
Firstly the need of explanation, the nouns of locality such as heretofore described front, back, left, right, up, down only with reference to the accompanying drawings into
Capable description, in order to understand, not to technical solution of the present invention and be claimed range progress limitation.
A kind of specific embodiment party of the guided missile rear support guiding device for firing box of the present invention as shown in Fig. 1 to Figure 15
Formula, including the pedestal 1 and the parallel left rail 2 and right guide rail 3 being fixed on pedestal 1 being arranged along the longitudinal direction, in pedestal 1
Rear end is equipped with the rear limit assembly 4 for being limited to guided missile rear slider, and corresponding in the rear end of left rail 2 and right guide rail 3
Left limit component 5 and right limit component 6 for being limited to guided missile rear slider is set.
The use for just constituting that a kind of structure is simple, manipulation is convenient, multifunctionality is strong, highly-safe is set through the above structure
In the guided missile rear support guiding device of firing box.In practical applications, the present invention is fixed in firing box by pedestal 1, it will
Guided missile is slid by guided missile rear slider 8 by front end in the guide groove of left rail 2 and right guide rail 3.In storage and transportational process, lead to
Later limit assembly 4 carries out rear side limit to guided missile rear slider 8, by left limit component 5 and right limit component 6 to sliding after guided missile
Block 8 carries out left side limit and right side limit, while the bullet locking mechanism by being set in firing box marches forward to guided missile rear slider 8
Row limit, can be realized the purpose limited comprehensively to guided missile rear slider 8, ensure that the peace in guided missile storage and transportational process
Quan Xing；In Missile Launching Process, by the cooperation of guided missile rear slider 8 and left rail 2 and right guide rail 3, guided missile can be provided
Support guide effect, ensure that the safety of guided missile outlet in emission process.And the present invention is by existing the setting of rear limit assembly 4
Left limit component 5 and right limit component 6 are correspondingly arranged at the rear end of left rail 2 and right guide rail 3 by the rear end of pedestal 1, and are passed through
The bullet locking mechanism realization being set in firing box is carried forward limit to guided missile rear slider 8, this arrangement only needs to lock bullet
Mechanism unlock, without being unlocked operation to rear limit assembly 4, left limit component 5 and right limit component 6, can meet and lead
Launching condition is played, the operating procedure before not only reducing transmitting, and interference effect will not be caused to guided missile outlet, have higher
Safety.It should be noted that heretofore described bullet locking mechanism (not shown) and guided missile rear slider 8 is the field
Conventional mechanisms and device, bullet locking mechanism is generally disposed in firing box to limit guided missile and to move forward, and specific structure exists
This is repeated no more；And guided missile rear slider 8 mainly includes arc bracket, left branch leg and right supporting leg, the lower end of left branch leg and right supporting leg
It is correspondingly provided with the left guide pad and right guide pad stretched out outward.
As specific embodiment, the present invention allows left rail 2 and right guide rail 3 to use identical structure and symmetrical point
Cloth.Allow left rail 2 to specifically include bottom left 21, left side 22 and left top 23, make bottom left 21, left side 22) and left top
Left guide groove 24 is formed between 23.Allow right guide rail 3 to specifically include right bottom 31, right side 32 and right top 33, make right bottom 31,
Right guide groove 34 is formed between right side 32 and right top 33.In practical application, the left branch leg of guided missile rear slider 8 and right supporting leg pair
It should be placed on the bottom left 21 of left rail 2 and the right bottom 31 of right guide rail 3, and lead the left guide pad of guided missile rear slider 8 and the right side
It is placed in left guide groove 24 and right guide groove 34 to block correspondence.This structure setting makes left rail 2 and right guide rail 3 for guided missile
On the basis of rear slider 8 provides support guide effect, guided missile rear slider 8 can be provided by left top 23 and right top 33 vertical
Limit function has the characteristics that structure is simple, supports firm, functional, contact area small.
As prioritization scheme, present embodiment allows rear limit assembly 4 to specifically include fixed frame and be set to fixed frame
On rear limited block, and limit assembly 4 after being arranged two groups allows limit assembly 4 after two groups to be fixed on pedestal 1 by fixed frame respectively
It is upper and corresponded with the rear end of left rail 2 and right guide rail 3, and after two groups limit assembly 4 the setting of rear limited block front end by
The preceding inclined scarf under rear.In practical applications, by allowing guided missile rear slider 8 in the rear end of its left branch leg and right supporting leg
Scarf with the cooperation of rear limited block is set, makes rear limit assembly 4 that not only there is position-limiting action backward to guided missile rear slider 8,
It has been provided simultaneously with upward position-limiting action, has improved the security reliability of limit function, practicability is stronger.Further, this tool
Body embodiment, which allows, fixed mount setting bottom plate 41 and is fixed on the supporting plate 42 of 41 front end of bottom plate, allows rear limited block setting 43 He of vertical part
The transverse part 44 for being fixed on 43 upper end of vertical part and forward extending out.The vertical part 43 of rear limited block is allowed to be placed on the bottom plate 41 of fixed frame and lead to
It crosses attachment screw to connect with supporting plate 42, allows the scarf on rear limited block that the front end of transverse part 44 is set.This structure setting can
The position of limited block, reduces preparation and assembly difficulty after being adjusted by attachment screw.It should be noted that in practical application
In, fixed frame can be used the modes such as welding or bolt and be fixed on pedestal 1, the vertical part 43 of rear limited block and the supporting plate 42 of fixed frame
It generallys use two attachment screws to be attached, on the basis of guaranteeing structural stability, adjusting difficulty can be reduced.In addition, this
Specific embodiment also allows the bottom plate 41 of fixing seat to open up sliding slot along the longitudinal direction, and allows the vertical part 43 of rear limited block at it
Downside is placed in the inverted " t " font sliding block in sliding slot, can be to rear limit by the cooperation of inverted " t " font sliding block and sliding slot
Block carries out positioning and guiding role, not only increases the convenience of adjusting, and can enhancing structure stability.
As the scheme that advanced optimizes, present embodiment allows left limit component 5 to specifically include left limit block 51, a left side tightly
Determine screw 52 and left locking nut 53.Left limit block 51 is set to be fixed on left rail by left holding screw 52 and left locking nut 53
On 2, and the inner end of left limit block 51 is made to be in 21 upside of bottom left of left rail 2, the inner end of left holding screw 52 is made to pass through a left side
The left side 22 of guide rail 2.Right limit component 6 is allowed to specifically include right limit block 61, right holding screw 62 and right locking nut 63.Make
Right limit block 61 is fixed on right guide rail 3 by right holding screw 62 and right locking nut 63, and makes the inner end of right limit block 61
31 upside of right bottom in right guide rail 3, makes the inner end of right holding screw 62 pass through the right side 32 of right guide rail 3.This structure
The left limit component 5 and right limit component 6 of form, can be realized by the inner end of left limit block 51 and right limit block 61 to after guided missile
The upward position-limiting action of sliding block 8, and by left holding screw 52 and right holding screw 62 can realize to guided missile rear slider 8 to the left and
Position-limiting action to the right has the characteristics that structure is simple, functional, and by screwing or unscrewing left holding screw 52 and the right side
The adjustable compression intensity to guided missile rear slider 8 of holding screw 62.Bullet locking mechanism, present embodiment are connected for convenience of installation
It also is provided with bullet locking mechanism mounting base 7 in the rear end of pedestal 1, and makes it through welding manner and is fixed on pedestal 1.
In addition, present embodiment allows pedestal 1 to include rack 11 that section is "Ji" type, and in the inside of rack 11
The multiple interior reinforcing ribs 12 being spaced apart along its length are set, between the left and right side of rack 11 is respectively provided with along its length
Every multiple external reinforcing ribs 13 of distribution.Meanwhile rack 11 being allowed to open up along its length on its top plate, left plate and right side plate
The multiple through-holes being spaced apart.The pedestal 1 of this structure can effectively drop on the basis of guaranteeing support strength and structural stability
Low weight is advantageously implemented lighting purpose.
To help skilled in the art to understand the present invention, below to a kind of guided missile rear support for firing box of the present invention
The assembly of guiding device and use process make schematic illustration: 1. first by pedestal 1, left rail 2, right guide rail 3, rear limit assembly 4,
Left limit component 5, right limit component 6 and bullet locking mechanism mounting base 7 are assembled integral；It then will be whole after assembly by pedestal 1
Body is installed on peace and penetrates in case.2. passing through guided missile rear slider 8 when guided missile inlet and outlet to have cooperated with left rail 2 and right guide rail 3
At support guide.Before guided missile inlet, first by the left holding screw 52 of left limit component 5, the right holding screw of right limit component 6
62 and two groups after the corresponding locking nut of attachment screw of limit assembly 4 unscrew, and make left limit component 5,6 and of right limit component
Limit assembly 4 shifts outward after two groups；Guided missile inlet in place after, pass through the left holding screw 52 of locking, 62 and of right holding screw
The attachment screw of limit assembly 4 after two groups, the inner end of the inner end and right limit block 61 that make left limit block 51 are corresponding after guided missile
On the upside of the left guide pad of sliding block 8 and right guide pad, and left holding screw 52 and the correspondence of right holding screw 52 is made to be pressed in left guide pad
With the side of right guide pad, the rear limited block of limit assembly 4 passes through the corresponding left side for being pressed in guided missile rear slider 8 of scarf after making two groups
Supporting leg and right supporting leg rear end.And guided missile rear slider 8 is carried out to front limit by bullet locking mechanism, to realize to sliding after guided missile
The purpose that block 8 is limited comprehensively.3. when MISSILE LAUNCHING outlet, it is only necessary to unlock bullet locking mechanism by control system, guided missile
All building blocks of rear support guiding device will not cause interference effect to outlet, without being unlocked operation.
Show that this bright has the advantages that realizes integrated and multifunction through practical application, by repeatedly transporting
Defeated test and flight test verifying, can fully meet requirement；Support guide function is provided, ensure that Missile Launching Process
The safety of middle outlet；Support limit function is provided, ensure that the safety of guided missile storage, transport；When MISSILE LAUNCHING outlet,
Guided missile rear support guiding device is without unlocking operation, the operating procedure before reducing transmitting.
Above embodiments are only the descriptions carried out to the preferred embodiment of the present invention, and model not is claimed to the present invention
It encloses and is defined, without departing from the spirit of the design of the present invention, the technology of this field engineers and technicians according to the present invention
The various forms of deformations that scheme is made, should fall within the scope of protection determined by the claims of the present invention.
Claims (5)
1. a kind of guided missile rear support guiding device for firing box, which is characterized in that including the pedestal being arranged along the longitudinal direction
(1) and in parallel the left rail (2) and right guide rail (3) being fixed on pedestal (1), the rear end of the pedestal (1) be equipped with for pair
The rear end of the rear limit assembly (4) that guided missile rear slider is limited, the left rail (2) and right guide rail (3), which is correspondingly provided with, to be used for
The left limit component (5) and right limit component (6) that guided missile rear slider is limited；
Left rail (2) distribution identical and symmetrical with right guide rail (3) structure, left rail (2) include bottom left (21),
Left side (22) and left top (23) form left guide groove (24) between bottom left (21), left side (22) and left top (23),
Right guide rail (3) includes right bottom (31), right side (32) and right top (33), right bottom (31), right side (32) and right top
(33) right guide groove (34) are formed between；
The rear limited block that limit assembly (4) includes fixed frame and is set on fixed frame after described；Limit assembly (4) is equipped with two afterwards
Group, after two groups limit assembly (4) be fixed on pedestal (1) by fixed frame respectively and with after left rail (2) and right guide rail (3)
End corresponds, and the rear limited block front end of limit assembly (4) is equipped with by preceding the inclined scarf under rear after two groups；
The fixed frame includes bottom plate (41) and the supporting plate (42) for being fixed on bottom plate (41) front end, and the rear limited block includes vertical part
(43) and the transverse part (44) that is fixed on vertical part (43) upper end and forward extends out；The vertical part (43) of limited block is placed in the bottom of fixed frame afterwards
It is connect on plate (41) and by attachment screw with supporting plate (42), the scarf on the rear limited block is arranged before transverse part (44)
End；
The left limit component (5) includes left limit block (51), left holding screw (52) and left locking nut (53), the left limit
Position block (51) is fixed on left rail (2) by left holding screw (52) and left locking nut (53), and makes left limit block (51)
Inner end be on the upside of the bottom left (21) of left rail (2), so that the inner end of left holding screw (52) is passed through the left side of left rail (2)
Portion (22)；The right limit component (6) includes right limit block (61), right holding screw (62) and right locking nut (63), described
Right limit block (61) is fixed on right guide rail (3) by right holding screw (62) and right locking nut (63), and makes right limit block
(61) inner end is on the upside of the right bottom (31) of right guide rail (3), and the inner end of right holding screw (62) is made to pass through right guide rail (3)
Right side (32).
2. a kind of guided missile rear support guiding device for firing box described in accordance with the claim 1, which is characterized in that described solid
Determine to offer sliding slot along the longitudinal direction on the bottom plate (41) of frame, is equipped on the downside of the vertical part (43) of the rear limited block and is placed in sliding slot
In inverted " t " font sliding block.
3. a kind of guided missile rear support guiding device for firing box according to claim 2, which is characterized in that further include
It is fixed on the bullet locking mechanism mounting base (7) of pedestal (1) rear end.
4. according to a kind of described in any item guided missile rear support guiding devices for firing box of claim 1-3, feature exists
In the pedestal (1) includes the rack (11) that section is "Ji" type, and the inside of rack (11) is equipped with interval point along its length
Multiple interior reinforcing ribs (12) of cloth, the left and right side of rack (11) are equipped with the multiple outer reinforcements being spaced apart along its length
Muscle (13).
5. a kind of guided missile rear support guiding device for firing box according to claim 4, which is characterized in that described
The multiple through-holes being spaced apart along its length are offered on the top plate of frame (11), left plate and right side plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710618701.5A CN107270770B (en) | 2017-07-26 | 2017-07-26 | A kind of guided missile rear support guiding device for firing box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710618701.5A CN107270770B (en) | 2017-07-26 | 2017-07-26 | A kind of guided missile rear support guiding device for firing box |
Publications (2)
| Publication Number | Publication Date |
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| CN107270770A CN107270770A (en) | 2017-10-20 |
| CN107270770B true CN107270770B (en) | 2019-01-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710618701.5A Active CN107270770B (en) | 2017-07-26 | 2017-07-26 | A kind of guided missile rear support guiding device for firing box |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502727B (en) * | 2018-03-28 | 2023-12-05 | 蓝箭航天技术有限公司 | Lifting device and crane |
| CN108534602B (en) * | 2018-05-29 | 2023-05-26 | 湖北三江航天万峰科技发展有限公司 | Debugging method and debugging mechanism for double V-shaped guide rail of small-caliber transmitting box |
| CN110162084B (en) * | 2018-10-11 | 2022-01-11 | 北京机电工程研究所 | Formation control method of flying missile cluster system based on consistency theory |
| CN111006558A (en) * | 2019-12-18 | 2020-04-14 | 湖北航天技术研究院总体设计所 | Auxiliary supporting device for warhead |
| CN112696978B (en) * | 2020-12-24 | 2022-12-27 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
| CN113295368B (en) * | 2021-04-29 | 2022-12-27 | 中国航天空气动力技术研究院 | Model test launching mechanism for backward separation wind tunnel release |
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| US8317025B1 (en) * | 2007-03-01 | 2012-11-27 | San Diego Composites, Inc. | Self-adjusting wedge bumper |
| JP2013108718A (en) * | 2011-11-24 | 2013-06-06 | Toshiba Corp | Launching device |
| CN104803006A (en) * | 2015-04-27 | 2015-07-29 | 西北工业大学 | UAV (Unmanned Aerial Vehicle) catapult-assisted take-off device |
| CN105151350A (en) * | 2015-09-02 | 2015-12-16 | 北京航天发射技术研究所 | Boxing device for simultaneous de-orbit firing |
| CN205279856U (en) * | 2015-11-25 | 2016-06-01 | 中国空空导弹研究院 | Prevent rolling guided missile brace table of guided missile and butt joint frock |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8317025B1 (en) * | 2007-03-01 | 2012-11-27 | San Diego Composites, Inc. | Self-adjusting wedge bumper |
| JP2013108718A (en) * | 2011-11-24 | 2013-06-06 | Toshiba Corp | Launching device |
| CN104803006A (en) * | 2015-04-27 | 2015-07-29 | 西北工业大学 | UAV (Unmanned Aerial Vehicle) catapult-assisted take-off device |
| CN105151350A (en) * | 2015-09-02 | 2015-12-16 | 北京航天发射技术研究所 | Boxing device for simultaneous de-orbit firing |
| CN205279856U (en) * | 2015-11-25 | 2016-06-01 | 中国空空导弹研究院 | Prevent rolling guided missile brace table of guided missile and butt joint frock |
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| Publication number | Publication date |
|---|---|
| CN107270770A (en) | 2017-10-20 |
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