CN108414255A - A kind of push type firing mount separation simulation device - Google Patents
A kind of push type firing mount separation simulation device Download PDFInfo
- Publication number
- CN108414255A CN108414255A CN201711292179.2A CN201711292179A CN108414255A CN 108414255 A CN108414255 A CN 108414255A CN 201711292179 A CN201711292179 A CN 201711292179A CN 108414255 A CN108414255 A CN 108414255A
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- CN
- China
- Prior art keywords
- fixed
- simulation device
- interface
- firing mount
- ground
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M99/00—Subject matter not provided for in other groups of this subclass
- G01M99/008—Subject matter not provided for in other groups of this subclass by doing functionality tests
-
- 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
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
Abstract
The present invention provides push type firing mount separation simulation device, including：Bearing is fixed on ground；Cylinder, including cylinder body, push rod, force snesor and signal transmission module, one end of the cylinder body is pushed to be fixed with bearing installation, the other end connects one end of the push rod, and the other end of the push rod connects one end of the force snesor；The tail end of the other end connection guided missile of the force snesor, the signal transmission module are fixed on the cylinder body；Controller is connect with signal transmission module signal；Portal frame is fixed on ground；Suspension joint is mounted on the portal frame, has height adjustment capability；Launcher, one end are fixed on suspension joint, and the other end fixes guided missile.Push type firing mount separation simulation device provided by the invention; guided missile is set to be detached with realizations such as launcher, electrical outlets, air-path interfaces under impetus; to verify whether the separation process between guided missile, launcher is coordinated, it is ensured that airborne missile can be smoothly detached in formal transmitting.
Description
Technical field
The present invention relates to guided missile and launcher Separation Test Technology field, more particularly to a kind of push type firing mount separation simulation
Device.
Background technology
Airborne missile is in emission process, it is necessary first to realize guided missile and launcher under the effect of engine initial thrust
Normal separation.Whether the firing mount separation process fully to verify in Missile Launching Process meets technical need, examination guided missile and hair
Can penetrate between frame be smoothly detached, and whether the hair flow control journey between verification guided missile, launcher, carrier aircraft hair control is coordinated, and needs
Carry out the experiment of firing mount separation simulation on ground.When experiment, needs launcher and guided missile combination being fixedly mounted, pass through experimental rig
It pushes guided missile with simulated engine initial thrust, and then realizes the separation simulation of guided missile and launcher.
Invention content
The purpose of the present invention is to provide a kind of push type firing mount separation simulation devices, to solve how to design set of device
The problems such as being smoothly detached between examination guided missile and launcher.
In order to solve the above-mentioned technical problem, the technical scheme is that：A kind of push type firing mount separation simulation dress is provided
It sets, including：Bearing is fixed on ground；Push cylinder, including cylinder body, push rod, force snesor and signal transmission module, the cylinder
The installation of one end of body and the bearing is fixed, and the other end connects one end of the push rod, described in the other end connection of the push rod
One end of force snesor；The tail end of the other end connection guided missile of the force snesor, the signal transmission module is fixed on described
On cylinder body；Controller is connect with the signal transmission module signal；Portal frame is fixed on ground；Suspension joint is mounted on institute
It states on portal frame, there is height adjustment capability；Launcher, one end are fixed on the suspension joint, and the other end fixes guided missile.
Further, the bearing has ground fixed interface and cylinder is pushed to install interface, and the bearing passes through described
Ground fixed interface is fixed with ground, is installed interface by the promotion cylinder and is fixed with promotion cylinder installation.
Further, the promotion cylinder installation interface is the kidney slot being distributed vertically, and has mounting height regulating power.
Further, one end of the cylinder body by mounting hole and the bearing installation fix, the mounting hole with it is described
Push cylinder that Interface Matching is installed.
Further, the portal frame includes ground installation interface and suspension joint installation interface, described gantry
Frame installs interface by the ground and is fixed on ground, and installing interface by the suspension joint is mounted on the suspension joint
On the portal frame.
Further, the suspension joint includes portal frame anchor tip and launcher installation interface, the portal frame
Anchor tip is connect with suspension joint installation interface, and the launcher installation interface is fixedly connected with the launcher.
Further, the quantity of the portal frame is two, and the relative position of two portal frames has tune when installation
Whole ability.
Further, the promotion cylinder further includes displacement sensor, and institute's displacement sensors are fixed on the push rod, is read
Take the position data of the push rod.
Further, the controller is connect by signal wire with the signal transmission module signal.
Push type firing mount separation simulation device provided by the invention makes guided missile be inserted with launcher, electrically under impetus
The realizations such as seat, air-path interface detach, to verify whether the separation process between guided missile, launcher is coordinated, it is ensured that airborne missile exists
It can be smoothly detached when formal transmitting.
Description of the drawings
Invention is described further below in conjunction with the accompanying drawings：
Fig. 1 is structural representation when push type firing mount separation simulation device provided in an embodiment of the present invention does not install guided missile
Figure；
Fig. 2 is structural schematic diagram when push type firing mount separation simulation device provided in an embodiment of the present invention installs guided missile；
Fig. 3 is the bearing structure illustration in push type firing mount separation simulation device provided in an embodiment of the present invention；
Fig. 4 is the promotion cylinder structure schematic diagram in push type firing mount separation simulation device provided in an embodiment of the present invention.
Specific implementation mode
Push type firing mount separation simulation device proposed by the present invention is made below in conjunction with the drawings and specific embodiments further
It is described in detail.According to following explanation and claims, advantages and features of the invention will become apparent from.It should be noted that attached drawing
It is all made of very simplified form and uses non-accurate ratio, only to convenient, lucidly the aid illustration present invention is implemented
The purpose of example.
Core of the invention thought is that push type firing mount separation simulation device provided by the invention makes guided missile push
Effect is lower to be detached with realizations such as launcher, electrical outlets, air-path interfaces, is with the separation process verified between guided missile, launcher
No coordination, it is ensured that airborne missile can be smoothly detached in formal transmitting.
Fig. 1 is structural representation when push type firing mount separation simulation device provided in an embodiment of the present invention does not install guided missile
Figure；Fig. 2 is structural schematic diagram when push type firing mount separation simulation device provided in an embodiment of the present invention installs guided missile；Fig. 4 is
Promotion cylinder structure schematic diagram in push type firing mount separation simulation device provided in an embodiment of the present invention.Referring to Fig.1, Fig. 2 and
Fig. 4, the embodiment of the present invention provide a kind of push type firing mount separation simulation device, including：Bearing 1, is fixed on ground；Cylinder 2 is pushed,
Including cylinder body 41, push rod 42, force snesor 45 and signal transmission module 44, one end of the cylinder body 41 is pacified with the bearing 1
Dress is fixed, and the other end connects one end of the push rod 42, and the other end of the push rod 42 connects one end of the force snesor 45；
The tail end of the other end connection guided missile 8 of the force snesor 45, the force snesor 45 are fixed on the push rod 42, the letter
Number transmission module 44 is fixed on the cylinder body 41；Controller 3 is connect with 44 signal of the signal transmission module；Portal frame 5,
It is fixed on ground；Suspension joint 6 is mounted on the portal frame 5, has height adjustment capability；Launcher 7, one end is fixed on
On the suspension joint 6, the other end fixes guided missile 8.
Fig. 3 is the bearing structure illustration in push type firing mount separation simulation device provided in an embodiment of the present invention.Reference
Fig. 3, the bearing 1 have ground fixed interface 31 and cylinder are pushed to install interface 32, and the bearing 1 is solid by the ground
Stationary interface 31 is fixed with ground, is installed interface 32 by the promotion cylinder and is fixed with the promotion cylinder 2 installation.The promotion cylinder peace
Attaching mouth 31 is the kidney slot being distributed vertically, and has mounting height regulating power.One end of the cylinder body passes through mounting hole 43
It installs and fixes with the bearing 1, the mounting hole 43 is matched with promotion cylinder installation interface 31.
The portal frame 5 includes that ground installation interface and the suspension joint install interface, and the portal frame 5 passes through
The ground installation interface is fixed on ground, and interface is installed by the suspension joint 6 mounted on described by the suspension joint
On portal frame 5.The quantity of the portal frame 5 is two, and the relative position of two portal frames 5 has adjustment energy when installation
Power.
The suspension joint 6 includes that portal frame anchor tip and launcher install interface, the portal frame anchor tip
It is connect with suspension joint installation interface, the launcher installation interface is fixedly connected with the launcher 7.
In embodiments of the present invention, the promotion cylinder further includes displacement sensor, and institute's displacement sensors are fixed on described
On push rod 42, the position data of the push rod 42 is read.
Further, the controller 3 is connect by signal wire 4 with 44 signal of the signal transmission module, and controller 3 has
Standby data acquisition function, can acquire the position for pushing cylinder 2 to feed back, thrust data in real time；Controller 3 can be to the position of acquisition
Data convert, and obtain real-time speed, acceleration parameter.
When being tested using push type firing mount separation simulation device provided in an embodiment of the present invention, first by bearing 1
It fixes on the ground, then cylinder 2 will be pushed to be fixed on the corresponding position on bearing 1, then by two portal frames 5 according to spacing
It is required that after fixing on the ground, suspension joint 6 is installed, 6 lower section of suspension joint is equipped with launcher 7 and guided missile 8.Later, it will push away
2 push rod of dynamic cylinder, 42 front end is connect with 8 rear end of guided missile, and the control of controller 3 being connected to by signal wire 4 pushes pushing away for 2 push rod 42 of cylinder
The actions such as dynamic and braking make guided missile 8 be detached with the realization of launcher 7 under impetus, to verify in airborne Missile Launching Process
Can guided missile normally detach with firing mount.
To sum up, the embodiment of the present invention is docked by the assembling of each component, can be pushed away by the initial of motive force simulated engine
Power makes guided missile be detached with realizations such as launcher, electrical outlets, air-path interfaces under impetus, with verify guided missile, launcher it
Between separation process whether coordinate, it is ensured that airborne missile can be smoothly detached in formal transmitting.
Obviously, those skilled in the art can carry out the present invention essence of various changes and deformation without departing from the present invention
God and range.In this way, if these modifications and changes of the present invention belongs to the range of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to include these modifications and variations.
Claims (9)
1. a kind of push type firing mount separation simulation device, which is characterized in that including：
Bearing is fixed on ground；
Cylinder, including cylinder body, push rod, force snesor and signal transmission module, one end of the cylinder body is pushed to pacify with the bearing
Dress is fixed, and the other end connects one end of the push rod, and the other end of the push rod connects one end of the force snesor；The power
The tail end of the other end connection guided missile of sensor, the signal transmission module are fixed on the cylinder body；
Controller is connect with the signal transmission module signal；
Portal frame is fixed on ground；
Suspension joint is mounted on the portal frame, has height adjustment capability；
Launcher, one end are fixed on the suspension joint, and the other end fixes guided missile.
2. push type firing mount separation simulation device as described in claim 1, which is characterized in that the bearing is fixed with ground
Interface and promotion cylinder install interface, and the bearing is fixed by the ground fixed interface with ground, and the promotion cylinder is passed through
Interface is installed to fix with promotion cylinder installation.
3. push type firing mount separation simulation device as claimed in claim 2, which is characterized in that the promotion cylinder installs interface and is
The kidney slot being distributed vertically, and there is mounting height regulating power.
4. push type firing mount separation simulation device as claimed in claim 3, which is characterized in that one end of the cylinder body passes through peace
It fills hole to fix with bearing installation, the mounting hole installs Interface Matching with the promotion cylinder.
5. push type firing mount separation simulation device as described in claim 1, which is characterized in that the portal frame includes ground peace
Attaching mouth and the suspension joint install interface, and the portal frame installs interface by the ground and is fixed on ground, passes through
The suspension joint is mounted on the portal frame by the suspension joint installation interface.
6. push type firing mount separation simulation device as claimed in claim 5, which is characterized in that the suspension joint includes gantry
Frame anchor tip and launcher install interface, and the portal frame anchor tip is connect with suspension joint installation interface, institute
Launcher installation interface is stated to be fixedly connected with the launcher.
7. push type firing mount separation simulation device as described in claim 1, which is characterized in that the quantity of the portal frame is two
A, the relative position of two portal frames has adjustment capability when installation.
8. push type firing mount separation simulation device as described in claim 1, which is characterized in that the promotion cylinder further includes displacement
Sensor, institute's displacement sensors are fixed on the push rod, read the position data of the push rod.
9. push type firing mount separation simulation device as described in claim 1, which is characterized in that the controller passes through signal wire
It is connect with the signal transmission module signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711292179.2A CN108414255A (en) | 2017-12-07 | 2017-12-07 | A kind of push type firing mount separation simulation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711292179.2A CN108414255A (en) | 2017-12-07 | 2017-12-07 | A kind of push type firing mount separation simulation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108414255A true CN108414255A (en) | 2018-08-17 |
Family
ID=63125415
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711292179.2A Pending CN108414255A (en) | 2017-12-07 | 2017-12-07 | A kind of push type firing mount separation simulation device |
Country Status (1)
| Country | Link |
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| CN (1) | CN108414255A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110230949A (en) * | 2019-07-01 | 2019-09-13 | 江西洪都航空工业集团有限责任公司 | A kind of guided missile experiment transmitting hanging frame device of adjustable launching elevation and stop spacing |
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
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| CN106017951A (en) * | 2016-05-10 | 2016-10-12 | 中国北方车辆研究所 | Integrated simulated hydro-pneumatic suspension testing system with road load and environmental stress integration |
| CN205785819U (en) * | 2016-05-24 | 2016-12-07 | 华中科技大学 | A kind of test device for rocket engine ground firing |
| CN106643294A (en) * | 2017-02-09 | 2017-05-10 | 沈阳航空航天大学 | Dual-mode launcher for airborne missile |
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| CN2316624Y (en) * | 1998-03-11 | 1999-04-28 | 中国航天工业总公司第四研究院第四十一研究所 | Rocket launching apparatus for increasing rain and preventing hailstone |
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| CN104236881A (en) * | 2014-08-26 | 2014-12-24 | 中国直升机设计研究所 | Rigid damping testing device |
| CN204388707U (en) * | 2014-12-23 | 2015-06-10 | 西安电子工程研究所 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110230949A (en) * | 2019-07-01 | 2019-09-13 | 江西洪都航空工业集团有限责任公司 | A kind of guided missile experiment transmitting hanging frame device of adjustable launching elevation and stop spacing |
| CN110230949B (en) * | 2019-07-01 | 2021-07-16 | 江西洪都航空工业集团有限责任公司 | Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance |
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
| CN114485262B (en) * | 2022-01-29 | 2024-03-29 | 重庆零壹空间航天科技有限公司 | System for verifying missile oblique launching reliability |
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| PB01 | Publication | ||
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Application publication date: 20180817 |