CN209290729U - A kind of emitter suitable for penetrating umbrella rocket - Google Patents
A kind of emitter suitable for penetrating umbrella rocket Download PDFInfo
- Publication number
- CN209290729U CN209290729U CN201821943898.6U CN201821943898U CN209290729U CN 209290729 U CN209290729 U CN 209290729U CN 201821943898 U CN201821943898 U CN 201821943898U CN 209290729 U CN209290729 U CN 209290729U
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- Prior art keywords
- rocket
- link block
- launcher
- emitter
- penetrating
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Abstract
The emitter that the utility model discloses a kind of suitable for penetrating umbrella rocket, belong to aircraft recovery technology field, rocket link block is arranged by the top half in launcher in it, and rocket cabin link block is arranged in corresponding its, and bracket fixed block is correspondingly arranged by the lower half portion in launcher, launcher lower part and rocket bulkhead plate are correspondingly connected with by it, to realize being stably connected with for launcher top half and lower half portion and rocket bulkhead plate.The emitter of the utility model, its structure is simple, setting is easy, and the application method of emitter is simple, and connection reliability is high, it can effectively reduce setting difficulty of the emitter in rocket cabin, the setting efficiency of emitter is promoted, guarantees stabilization of the emitter in rocket cabin, reliability application, then realizes the accurate transmitting for penetrating umbrella rocket, to improve the efficiency and reliability of aircraft recycling, there is significant economic benefit and fabulous application value.
Description
Technical field
The utility model belongs to aircraft recovery technology field, and in particular to a kind of transmitting dress suitable for penetrating umbrella rocket
It sets.
Background technique
With the continuous development of China's aeronautical technology, all kinds of aircrafts using very extensive.In applying for aircraft
Cheng Zhong, the recycling of aircraft be a highly important process, often affects the service life and aircraft of aircraft
Application quality.
In aircraft recycling field, penetrate umbrella rocket using very extensive, be commonly used for quick overall length and aircraft be straightened
Main chute packet, help parachute to carry out quick parachute-opening, to realize the accurate recycling of aircraft.But due to penetrating umbrella rocket cabin
Size is small, depth is big, needed when so that penetrating the installation of umbrella rocket first by launcher, penetrate umbrella rocket and ignition connector install after it is whole again
Body is packed into rocket cabin, this gives the installation and removal for penetrating umbrella rocket to bring extreme difficulties；Meanwhile it penetrating after umbrella rocket firing due to certainly
The effect of height warm air can generate very large disturbances in rocket cabin, affect its kinetic stability, lead to penetrate umbrella rocket in fire
Launching trajectory in arrow cabin generates offset, even will affect the safety and reliability for penetrating umbrella when serious.
In 107499539 A of earlier application CN of the applicant, discloses and a kind of portable penetrate umbrella rocket launching dress
It sets, including launcher and transmitting bottom plate, the bottom for emitting bottom plate and being set to the launcher, the launcher one side
Lower half portion is equipped with rocket link block, and the outside of the rocket link block is equipped with rocket cabin link block, rocket cabin link block
Quadrangle be equipped with third screw, penetrate umbrella rocket cabin for rocket cabin link block to be fixed on；The top of the launcher
Equipped with guide chute, the guide chute penetrates umbrella rocket for placing；The transmitting bottom plate is equipped with mounting hole.Pass through above-mentioned hair
Injection device can realize the corresponding installation for penetrating umbrella rocket in narrow rocket cabin to a certain extent；But by largely studying and
Using above-mentioned emitter is shown, there are still certain defects in application process, are embodied in following two aspects: 1, penetrating
After umbrella rocket is mounted in emitter, since the position that rocket cabin link block is arranged in rocket cabin is more on the lower side, so that fiery
The assembly and its inconvenience of arrow link block and rocket cabin link block, cause the assembly efficiency of emitter low；2, rocket pod
The connection with rocket bulkhead plate is only realized by the second screw in the middle part of the link block of rocket cabin, between upper part and rocket bulkhead plate
And not set connection structure, cause the integrated connection rigidity of launcher lower, when penetrating the work of umbrella rocket, due to high in rocket cabin
The disturbance of warm air easily makes rocket pod generate shaking, causes the deformation or damage of launcher structure, and umbrella is penetrated in influence
The accuracy of rocket launching track influences to penetrate the normal use of umbrella rocket and the safe retrieving of aircraft.
Utility model content
One or more of aiming at the above defects or improvement requirements of the prior art, the utility model provides one kind
Suitable for penetrating the emitter of umbrella rocket, wherein being correspondingly arranged rocket link block by the top half in launcher and emitting
The lower half portion of frame is correspondingly arranged bracket fixed block, effectively improves the setting convenience and the connection of emitter of emitter
Rigidity, it is ensured that the normal use for penetrating umbrella rocket improves the launch accuracy for penetrating umbrella rocket.
To achieve the above object, the utility model provides a kind of emitter suitable for penetrating umbrella rocket, including launcher,
Rocket link block and rocket cabin link block, which is characterized in that
It further include bracket fixed block, the bracket fixed block is set to the lower half portion of one side end face of launcher, leads to
It crosses several first screws to achieve a fixed connection with the launcher, and can be realized by several third screws and rocket bulkhead plate
It is fixedly connected；
The rocket link block is set to the top half of the launcher comprising the ontology of plate-like structure and vertically sets
It is placed in the postive stop baffle of ontology side end top, and is set to below the postive stop baffle and is put down with the ontology end face
Capable installation slide plate；Several second screws are correspondingly arranged on the postive stop baffle, and the ontology passes through several described first
Screw achieves a fixed connection with the launcher；
Rocket cabin link block corresponds to the rocket link block setting, and four corners are respectively equipped with the third screw,
For rocket cabin link block to be fixed on the rocket bulkhead plate, and the installation is corresponded on the link block of the rocket cabin
Slide plate is provided with installation sliding slot, and the installation slide plate can correspond in the insertion installation sliding slot, and with postive stop baffle abutting
The top of rocket cabin link block, so that the rocket link block can be connect by second screw with the rocket cabin
Block is correspondingly connected with.
The four corners of the bracket fixed block are respectively arranged with first spiral shell as a further improvement of the utility model,
Nail, and its middle part is arranged at intervals with several third screws.
The postive stop baffle is after the end 90-degree bent of the ontology by obtaining as a further improvement of the utility model,
Perhaps the postive stop baffle and the corresponding side for being welded on the ontology of described body by integral forming or the postive stop baffle
On face.
The launcher is the corresponding frame knot being composed of three blocks of steel plates as a further improvement of the utility model,
Structure comprising front steel plate and the side steel plate for being vertically divided into front steel plate two sides, the front steel plate and the side
Square through hole is offered respectively on the steel plate of face.
The rocket link block is fixedly connected on the front steel plate close to two as a further improvement of the utility model,
On one side end face of the side steel plate, and the limited block and the installation slide plate protrude from the another of the front steel plate
Side end face.
It as a further improvement of the utility model, further include the mounting base for being set to the launcher bottom, it is described
Mounting base is achieved a fixed connection by several first screws with the launcher, and is offered and be used on the mounting base
The ignition module mounting hole of ignition module is installed.
Second screw includes at least and is divided into the postive stop baffle both ends as a further improvement of the utility model,
Two.
Above-mentioned improved technology feature can be combined with each other as long as they do not conflict with each other.
In general, have the above technical solutions conceived by the present invention are compared with the prior art, with following
Beneficial effect:
(1) emitter for being suitable for penetrating umbrella rocket of the utility model passes through the top half setting in launcher
The Corresponding matching of rocket link block, and its corresponding setting rocket cabin link block, rocket link block and rocket cabin link block is in rocket
The top in cabin is completed, and the joint efficiency of rocket link block Yu rocket cabin link block is effectively improved, and it is corresponding to reduce two link blocks
Matched difficulty shortens the setting time for penetrating umbrella rocket in rocket cabin, reduces the setting for penetrating umbrella rocket, use cost；
(2) emitter for being suitable for penetrating umbrella rocket of the utility model, by corresponding in the lower half portion of launcher
Bracket fixed block is set, launcher lower part and rocket bulkhead plate are correspondingly connected with by it, is then connected by rocket link block and rocket cabin
The Corresponding matching for connecing block realizes being stably connected with for launcher top and rocket bulkhead plate, and realizes transmitting by bracket fixed block
Frame lower part is stably connected with rocket bulkhead plate, to effectively improve the coupling stiffness of launcher, is reduced and is penetrated umbrella rocket work
The shaking, deformation or damage of launcher, ensure that the accuracy for penetrating umbrella rocket trajectory when making, and improve and penetrate the work of umbrella rocket
Efficiency ensure that the normal use for penetrating umbrella rocket；
(3) emitter for being suitable for penetrating umbrella rocket of the utility model, by the knot for being preferably provided with rocket link block
Structure realizes limit when rocket link block connect Block- matching with rocket cabin by being correspondingly arranged postive stop baffle, and passes through limit
Position baffle realizes the Corresponding matching connection of two link blocks, ensure that the stable connection of rocket link block Yu rocket cabin link block
Property, it ensure that the stability of emitter in use, realize the accurate work for penetrating umbrella rocket；
(4) emitter for being suitable for penetrating umbrella rocket of the utility model, structure is simple, and setting is easy, and emits
The application method of device is simple, and connection reliability is high, can effectively promote setting efficiency of the emitter in rocket cabin, guarantees hair
Stabilization of the injection device in rocket cabin, reliability application then realize the accurate transmitting for penetrating umbrella rocket, return to improve aircraft
The efficiency and reliability of receipts has significant economic benefit and fabulous application value.
Detailed description of the invention
Fig. 1 is the assembling structure perspective view for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
Fig. 2 is the rearview for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
Fig. 3 is the bottom view for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
Fig. 4 is the launcher structural schematic diagram for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
Fig. 5 is the rocket connecting block structure signal for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment
Figure；
Fig. 6 is the rocket cabin connecting block structure signal for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment
Figure；
Fig. 7 is the bracket fixed-block-architecture (FBA) signal for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment
Figure；
Fig. 8 is the mounting base structural schematic diagram for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
Fig. 9 is the application method flow chart for being suitable for penetrating the emitter of umbrella rocket in the utility model embodiment；
In all the appended drawings, same appended drawing reference indicates identical technical characteristic, specifically: 1. launchers, 101. lead
To sliding slot, 102. pin holes；2. rocket link block, 201. postive stop baffles, 202. installation slide plates, 3. rocket cabin link blocks, 301. peaces
Fill sliding slot；4. bracket fixed block, 5. mounting bases, 501. ignition module mounting holes；6. connector, 601. first screws, 602.
Second screw, 603. third screws.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only to explain this
Utility model is not used to limit the utility model.
As long as in addition, technical characteristic involved in the various embodiments of the present invention described below each other it
Between do not constitute conflict and can be combined with each other.
It is suitable for penetrating the emitter of umbrella rocket in the preferred embodiment in the utility model as shown in Fig. 1~8 comprising hair
Frame 1, rocket link block 2, rocket cabin link block 3, bracket fixed block 4 and mounting base 5 are penetrated, and is correspondingly connected with for each component
Connector 6.
Wherein, launcher 1 is made of front steel plate with a pair of of the side steel plate for being relatively arranged on the front steel plate two sides, and two
Side steel plate is fixedly connected with the side of front steel plate respectively with side, and forms frame structure shown in Fig. 1 and Fig. 4, the frame
Several square through holes are offered respectively on the front steel plate of frame structure, two sides steel plate；Connector 6 in preferred embodiment includes
The first screw 601 for connecting for corresponding component with launcher 1 is correspondingly connected with for rocket link block 2 and rocket cabin link block 3
The second screw 602 and the third screw 603 that is correspondingly connected with for the siding in corresponding component and rocket cabin.
Further, the top of launcher 1 is opposite offers a pair of of guide chute 101, and correspondence is provided with two and sets relatively
On the side steel plate set, the guide chute 101 for penetrating guiding when umbrella rocket launching, and in preferred embodiment is preferably provided with
Away from the side of front steel plate；Further, it is preferable to 101 bottom of guide chute in embodiment is correspondingly arranged on pin hole 102, and
Corresponding its is provided with pin shaft, which is more preferably copper pin, and above-mentioned pin shaft can penetrate umbrella rocket appearance in guide chute 101
When setting in place in corresponding insertion pin hole 102, to realize the Weak link for penetrating umbrella rocket Yu launcher 1, it is ensured that in unmanned plane transmitting, fly
Setting stability of the umbrella rocket in guide chute 101 is penetrated under the conditions of capable vibration, shock environment etc..
Further, it is correspondingly arranged on rocket cabin link block 3 in the top half of launcher 1, launcher 1 and rocket cabin connect
It connects and is provided with rocket link block 2 between block 3, wherein rocket link block 2 is as shown in Figure 5 comprising in rectangular plate-like structure
Ontology is provided with postive stop baffle 201 at the top of ontology, which is vertically installed on a side end face of ontology, end
Correspondence offers several connection through-holes on face, to pass through several second screws 602 and rocket cabin link block for rocket link block 2
3 are correspondingly connected with, and 201 both ends of postive stop baffle in preferred embodiment are respectively arranged with the second screw 602, to fully ensure that two companies
Connect the connective stability of block；It is further preferred that limited block 202 can be by obtaining after the end 90-degree bent of ontology, Huo Zheyu
This body by integral forming, or correspondence are welded on the end face of ontology.
Further, ontology is provided with the ipsilateral of postive stop baffle 201 and is provided with installation slide plate 202, be used for and rocket cabin
3 Corresponding matching of link block, which is parallel to the end face setting of ontology, by axis perpendicular to postive stop baffle 201
Square bar connector correspondence be fixedly connected on ontology end face, and slide plate 202 is installed and ontology end face is at regular intervals, and makes
The two sides that slide plate 202 must be installed protrude from the side of square bar connector, that is, form the rocket link block for being similar to " I-shaped " shape
2。
Further, rocket link block 2 can be correspondingly connected on the top of launcher, further preferably by connector 6
For being correspondingly connected on launcher 1, and being set in preferred embodiment on rocket link block 2 by several first screws 601
One screw 601 is to be divided into four of ontology four corners, and rocket link block 2 connects the inside that launcher 1 is arranged in, i.e. rocket
Link block 2 is correspondingly arranged between two steel plates of 1 two sides of launcher, and makes limiting block after the connection setting of rocket link block 2
Plate 201 and installation slide plate 202 protrude from the end face of 1 front steel plate of launcher.
Further, it is preferable to which the rocket cabin link block 3 in embodiment is as shown in Figure 6, can connect by the way that connector 6 is corresponding
It connects in rocket bulkhead plate, further preferably passes through four third screws 603 and be fixedly connected, four third screws 603
It is divided into the two sides of rocket cabin link block 3, i.e., its two sides, which is respectively separated, opens up that there are two mounting holes, so that third screw 603 can
It corresponds to by being connected in rocket bulkhead plate after mounting hole.
Further, it is correspondingly arranged on bracket fixed block 4 in the lower half portion of launcher 1, for side as shown in Figure 7
Shape plate structure is fixedly connected on front steel plate on a side end face of two sides steel plate by installation part 6；Preferably, it props up
The four corners of frame fixed block 4 are respectively arranged with the first screw 601, can be fixed on bracket fixed block 4 by each first screw 601
On rocket cabin 1；Further, multiple third screws 603 are arranged at intervals at the middle part of bracket fixed block 4, to be used for bracket
Fixed block 4 is fixedly connected on the siding in rocket cabin.
Further, it is preferable to which 1 bottom of launcher in embodiment is provided with mounting base 5 as shown in Figure 8, level is set
It sets in the bottom of launcher 1, is correspondingly connected with by several first screws 601 in the bottom of front steel plate, it is preferable that mounting base
5 settings triangular in shape, the both ends of one side are correspondingly arranged on the first screw 601, and open up away from the side of side correspondence
There is ignition module mounting hole 501, with the corresponding installation for ignition module.
By the Corresponding matching of above-mentioned component, emitter as illustrated in figures 1-3 can be formed, and for penetrating umbrella rocket
Transmitting.
The transmitting for being suitable for penetrating umbrella rocket in the preferred embodiment in the utility model is decorated in use, its application method such as Fig. 9
Shown in, and preferably include following steps:
S1: rocket cabin link block 3 is corresponded to and is fixedly connected on the siding in rocket cabin with third screw 603；
Rocket link block 2, bracket fixed block 4: being correspondingly connected on launcher 1 by S2 with multiple first screws 601 respectively,
Rocket link block 2 is fixedly connected on a upper lateral part of the front steel plate close to two sides steel plate, and bracket fixed block 4 is fixedly connected on just
Face steel plate deviates from a side lower part of two sides steel plate；
S3: will penetrate umbrella rocket correspondence and be placed in guide chute 101, and respectively correspond two pins afterwards in place penetrating the accommodating of umbrella rocket
Pin shaft is arranged in hole 102, so that realizing the Weak link for penetrating umbrella rocket Yu launcher 1 in pin shaft insertion pin hole 102, umbrella fire is penetrated in guarantee
Setting stability of the arrow before not working；
S4: it is correspondingly connected with the ignition module for penetrating umbrella rocket in the tail portion for penetrating umbrella rocket, while being connected in the bottom of launcher 1
Mounting base 5 is set, and ignition module correspondence is mounted in ignition module mounting hole 501；
S5: will be provided with the launcher 1 for penetrating umbrella rocket and be correspondingly placed into rocket cabin, so that the installation of rocket link block 2 is sliding
Plate 202 is correspondingly embedded in the installation sliding slot 301 of rocket cabin link block 3, until the postive stop baffle 201 of rocket link block 2 abuts fire
The top of arrow cabin link block 3；
Rocket link block 2 and rocket cabin link block 3: being correspondingly connected with by S6 by several second screws 602, and by several
Bracket fixed block 4 is fixedly connected on the siding in rocket cabin by third screw 603, realizes the consolidating in rocket cabin of launcher 1
Fixed setting, to complete to penetrate application of the umbrella rocket projector in rocket cabin.
It is suitable for penetrating the emitter of umbrella rocket in the utility model, structure is simple, and setting is easy, by being correspondingly arranged
Rocket cabin link block and bracket fixed block effectively realize fixed setting of the launcher in rocket cabin, ensure that launcher
Upper and lower part is fixedly connected with rocket bulkhead plate respectively, is greatly improved junction steel plate of the launcher in rocket cabin, is mentioned
The stability in use of emitter is risen, it is ensured that penetrate the accuracy of umbrella rocket launching track；And by by rocket cabin link block
It is correspondingly arranged at the top of launcher with rocket link block, improves the convenience of two link block Corresponding matchings, shortens and penetrate umbrella
The setting period of rocket has significant economic benefit and vast market prospect.
As it will be easily appreciated by one skilled in the art that the above is only the preferred embodiment of the utility model only, not
To limit the utility model, any modification made within the spirit and principle of the present invention, equivalent replacement and change
Into etc., it should be included within the scope of protection of this utility model.
Claims (7)
1. a kind of emitter suitable for penetrating umbrella rocket, including launcher (1), rocket link block (2) and rocket cabin link block
(3), which is characterized in that
It further include bracket fixed block (4), the bracket fixed block (4) is set to the lower half portion of (1) one side end face of launcher,
It is achieved a fixed connection by several first screws (601) with the launcher (1), and can pass through several third screws (603)
Realization is fixedly connected with rocket bulkhead plate；
The rocket link block (2) is set to the top half of the launcher (1) comprising the ontology of plate-like structure and vertical
Be set to the postive stop baffle (201) of ontology side end top, and be set to below the postive stop baffle (201) and with institute
State the parallel installation slide plate (202) in ontology end face；Several second screws (602) are correspondingly arranged on the postive stop baffle (201),
And the ontology is achieved a fixed connection by several first screws (601) with the launcher (1)；
Corresponding rocket link block (2) setting of rocket cabin link block (3), four corners are respectively equipped with the third screw
(603), for rocket cabin link block (3) to be fixed on the rocket bulkhead plate, and on rocket cabin link block (3)
The corresponding installation slide plate (202) is provided with installation sliding slot (301), and the installation slide plate (202) can correspond to the insertion installation
In sliding slot (301), and the top of rocket cabin link block (3) is abutted with the postive stop baffle (201), so that described the
The rocket link block (2) can be correspondingly connected with by two screws (602) with rocket cabin link block (3).
2. the emitter according to claim 1 for being suitable for penetrating umbrella rocket, wherein the four of the bracket fixed block (4)
First screw (601) is respectively arranged at angle, and its middle part is arranged at intervals with several third screws (603).
3. according to claim 1 or 2 be suitable for penetrating the emitter of umbrella rocket, wherein the postive stop baffle (201) by
The perhaps postive stop baffle (201) and described body by integral forming or described are obtained after the end 90-degree bent of the ontology
Postive stop baffle (201) correspondence is welded on a side end face of the ontology.
4. the emitter according to claim 1 or 2 for being suitable for penetrating umbrella rocket, wherein the launcher (1) is three pieces
The corresponding frame structure being composed of steel plate comprising front steel plate and the side steel for being vertically divided into front steel plate two sides
Square through hole is offered respectively on plate, the front steel plate and the side steel plate.
5. the emitter according to claim 4 for being suitable for penetrating umbrella rocket, wherein the rocket link block (2) is fixed
The front steel plate is connected on a side end face of the two side steel plates, and the limited block and the installation slide plate
(202) another side end face of the front steel plate is protruded from.
6. the emitter according to claim 1 or 2 for being suitable for penetrating umbrella rocket, wherein further include being set to the hair
The mounting base (5) of frame (1) bottom is penetrated, the mounting base (5) passes through several first screws (601) and the launcher
(1) it achieves a fixed connection, and offers the ignition module mounting hole for installing ignition module on the mounting base (5).
7. the emitter according to claim 1 or 2 for being suitable for penetrating umbrella rocket, wherein second screw (602) is extremely
Few includes two for being divided into the postive stop baffle (201) both ends.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821943898.6U CN209290729U (en) | 2018-11-23 | 2018-11-23 | A kind of emitter suitable for penetrating umbrella rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821943898.6U CN209290729U (en) | 2018-11-23 | 2018-11-23 | A kind of emitter suitable for penetrating umbrella rocket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209290729U true CN209290729U (en) | 2019-08-23 |
Family
ID=67645889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821943898.6U Active CN209290729U (en) | 2018-11-23 | 2018-11-23 | A kind of emitter suitable for penetrating umbrella rocket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209290729U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398765A (en) * | 2018-11-23 | 2019-03-01 | 襄阳宏伟航空器有限责任公司 | A kind of emitter and its application method suitable for penetrating umbrella rocket |
-
2018
- 2018-11-23 CN CN201821943898.6U patent/CN209290729U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398765A (en) * | 2018-11-23 | 2019-03-01 | 襄阳宏伟航空器有限责任公司 | A kind of emitter and its application method suitable for penetrating umbrella rocket |
| CN109398765B (en) * | 2018-11-23 | 2024-04-19 | 襄阳宏伟航空器有限责任公司 | Launching device suitable for parachute-shooting rocket and using method thereof |
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