CN108177747A - A kind of naval vessel sourceless seism rocket projectile fixed transmission air deflector - Google Patents
A kind of naval vessel sourceless seism rocket projectile fixed transmission air deflector Download PDFInfo
- Publication number
- CN108177747A CN108177747A CN201711400421.3A CN201711400421A CN108177747A CN 108177747 A CN108177747 A CN 108177747A CN 201711400421 A CN201711400421 A CN 201711400421A CN 108177747 A CN108177747 A CN 108177747A
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- air deflector
- water conservancy
- conservancy diversion
- angle
- panel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G1/00—Arrangements of guns or missile launchers; Vessels characterised thereby
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B71/00—Designing vessels; Predicting their performance
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
The invention discloses a kind of naval vessel sourceless seism rocket projectile fixed transmission air deflectors and its design method, the design method of the air deflector to specifically include following steps：Obtain the emission parameter of emitter；It is emulated to obtain its wake flame spray regime according to the emission parameter of emitter；The guide face size of air deflector is determined according to the wake flame spray regime of emitter；Determine the channelization angle of air deflector guide face；Effluent face is set, air deflector model is built according to guide face size and its channelization angle, the angle of inclination in effluent face, adjustment is optimized to the structure of air deflector.The injection stream of emitter playpipe can be smoothly oriented in atmospheric environment by the air deflector of the present invention, and the sideways diffusion coverage of injection stream can be controlled, efficiently solve the problems, such as that washing away repeatedly for injection stream can damage Ship Structure and its surrounding warship face equipment.
Description
Present patent application be on November 9th, 2017 application No. is 201711098007.1 patent of invention《A kind of warship
Ship sourceless seism rocket projectile fixed transmission air deflector and its design method》Divisional application
Technical field
The present invention relates to MISSILE LAUNCHING technical fields, are led more particularly to a kind of naval vessel sourceless seism rocket projectile fixed transmission
Flow device and its design method.
Background technology
Guided missile, rocket projectile and other arm discharge devices would generally be installed, due to by warship plane materiel material on ship deck
And space limitation, the high temperature and high speed jet-flow that guided missile and rocket projectile heat emission rear engine generate can be applied directly to hull
Structure and surrounding appliance arrangement generate more serious impact and thermal ablation to Ship Structure and surrounding appliance arrangement.
During middle-size and small-size ship design, due to being restricted by ship-borne ambient condition, sourceless seism emitter is usually placed in
The more complicated warship face region of environment, neighbouring Ship Structure employ the relatively low aluminum alloy materials of fusing point.Sourceless seism is sent out
When injection device continuously emits, the combustion gas stream that rocket projectile motor injection generates washes away ship-borne ambient repeatedly, will generate safety
It influences, therefore safety prevention measure need to be taken during master-plan.
The warship face equipment on large and medium-sized naval vessel is typically located at the warship face region not had an impact to ambient enviroment, while hull
Structure has the ability that combustion gas stream is washed away repeatedly when carrying rocket projectile continuously emits, therefore only to deck table after general arm discharge
Coating materials carry out repair process；It is resistance to by brushing to the middle-size and small-size naval vessel using the relatively low Aluminium alloy structural material of fusing point
The single that high-temperature coatings can only resist combustion gas stream washes away.
Invention content
The purpose of the present invention is overcome the deficiencies in the prior art, design a kind of naval vessel sourceless seism rocket projectile fixed transmission
Air deflector and its design method, the washing away repeatedly for injection stream for efficiently solving emitter can be to Ship Structure and its surrounding warship
The problem of face equipment damages.
In order to achieve the above objectives, the technical solution adopted in the present invention is：
A kind of design method of naval vessel sourceless seism rocket projectile fixed transmission air deflector, specifically includes following steps：
Step 1：Obtain the emission parameter of emitter and wake flame jet angle；
Step 2：It is emulated to obtain its wake flame spray regime according to the emission parameter of emitter；
Step 3：The guide face size of air deflector is determined according to the wake flame spray regime of emitter；
Step 4：Determine the channelization angle of air deflector guide face；
Step 5：The arranged on left and right sides of guide face is turned-out respectively to fold an acclivitous effluent face, the effluent face
Elongated surfaces should be located at surrounding warship face equipment top；
Step 6：According to guide face size and its channelization angle, the angle of inclination in effluent face, air deflector model is built, to setting
The wake flame injection stream for having the emitter of air deflector is emulated, and obtains the temperature cloud picture of ship-borne ambient and pressure cloud atlas, according to
The temperature and pressure situation of temperature cloud picture and pressure nephanalysis warship face different zones, according to analysis result adjust guide face and/
Or the arrange parameter in effluent face.
Preferably, the emission parameter of the emitter includes the outlet diameter of rocket engine playpipe, outlet
Expand half-angle；The emission parameter according to emitter emulate to obtain its wake flame spray regime the specific steps are：
Step 2.1：Determine the arrangement of emitter, the arrangement includes a variety of emission states, each transmitting
State corresponds to unique launch angle；
Step 2.2：The launch angle of emitter is adjusted, analog simulation goes out emitter under each emission state successively
Wake flame injection stream；
Step 2.3：Wake flame injection stream under each emission state is merged, obtains the total injection stream of wake flame；
Step 2.4：The injection cross section of the total injection stream of wake flame above deck is simulated, the injection cross section is to emit
The wake flame spray regime of device.
Preferably, the tool of wake flame injection stream of the emitter under a certain emission state is emulated in the step 2.2
Body step is：
Step 3.1：Determine the current launch angle of emitter and its fixed elevation of each playpipe；
Step 3.2：According to the outlet diameter of the current launch angle of emitter and a playpipe, export expansion half-angle
And fixed elevation, the boundary streamline using the extended line on its export expansion boundary as its wake flame simulate the pipe inspection of the playpipe
Stream；
Step 3.3：Step 3.2 is repeated, simulates the pipe inspection stream of each playpipe；
Step 3.4：The pipe inspection stream of each playpipe is merged, obtains emitter under current emission state
Wake flame injection stream.
Preferably, the area of the guide face should be greater than wake flame spray regime.
Preferably, the guide face includes the first guide face and the second guide face, the first guide face and the second water conservancy diversion
Face is mutually connected；
The channelization angle α of first guide face should meet relationship：α<90°-λ1, wherein, channelization angles of the α for the first guide face, λ1For
Angle between the playpipe of fixed elevation maximum of the emitter under emission maximum angle state and level ground；
The channelization angle β of second guide face should meet relationship：β<90°-λ2, wherein, channelization angles of the β for the second guide face, λ2For
Angle between the playpipe of fixed elevation minimum of the emitter under minimum launch angle state and level ground.
Preferably, the angle between the effluent face and guide face is not less than 20 °.
A kind of naval vessel sourceless seism rocket projectile fixed transmission air deflector, including baffle, the baffle is led including first
Flow faceplate, the second water conservancy diversion panel, support plate, the first water conservancy diversion panel and the first guide face being mutually connected with the first water conservancy diversion panel
Plate is obliquely installed, the arranged on left and right sides of the first water conservancy diversion panel and the second water conservancy diversion panel it is turned-out fold one it is acclivitous
Effluent panel, the support plate be fixed on vertically respectively on effluent panel and the trailing flank of the second water conservancy diversion panel on.
Preferably, multiple equally distributed lightening holes are offered in the support plate.
Preferably, the distance between the air deflector and the outlet of emitter playpipe are 300mm-500mm, water conservancy diversion
Device is fixed on ship deck, transit joint is provided between air deflector and ship deck, the transit joint is by aluminium sheet and steel
Plate forms, and is fixed between aluminium sheet and steel plate by gluing.
Preferably, the channelization angle α of the first water conservancy diversion panel guide face meets relationship：α<90°-λ1, wherein, α is
The channelization angle of first water conservancy diversion panel, λ1The playpipe for the fixed elevation maximum for being emitter under emission maximum angle state with
Angle between level ground；The channelization angle β of second guide face should meet relationship：β<90°-λ2, wherein, β is the second guide face
The channelization angle of plate, λ2The playpipe for the fixed elevation minimum for being emitter under minimum launch angle state and level ground it
Between angle；Angle between the effluent panel and the first water conservancy diversion panel or the second water conservancy diversion panel is not less than 20 °.
The positive beneficial effect of the present invention：
1st, the guide face of air deflector of the invention is capable of the injection stream of emitter playpipe and is smoothly oriented in atmospheric environment,
And since the both sides of guide face are provided with effluent face so that air deflector can control the sideways diffusion coverage of injection stream, have
Effect solves the problems, such as that washing away repeatedly for injection stream can damage Ship Structure and its surrounding warship face equipment.
2nd, the distance between air deflector and the outlet of emitter playpipe are 300mm-500mm, and the setting of air deflector will not
The normal use of emitter is influenced, handling rocket projectile will not be influenced, weapon penetrates preceding preparation, equips detection and maintenance etc.
Work.
3rd, since air deflector is made of steel material, Ship Structure is aluminum material, by air deflector and Ship Structure
Between transit joint is set, efficiently solve between steel air deflector and aluminum Ship Structure transition connection.
Description of the drawings
Fig. 1 is the stereogram of the present invention.
Fig. 2 is the lateral view of the present invention.
Fig. 3 be Fig. 2 in A-A to sectional view.
Fig. 4 is the B direction views in Fig. 3.
Fig. 5 is the use state diagram of the present invention.
The concrete meaning of figure label is：1 it is transit joint, 2 be support plate, 3 be the first water conservancy diversion panel, 4 is second to lead
Flow faceplate, 5 be effluent panel, 6 be lightening hole.
Specific embodiment
Understand to make the object, technical solutions and advantages of the present invention clearer, it is specific below by what is shown in attached drawing
Embodiment describes the present invention.However, it should be understood that these descriptions are merely illustrative, and it is not intended to limit the model of the present invention
It encloses.In addition, in the following description, the description to known features and technology is omitted, to avoid unnecessarily obscuring the present invention's
Concept.
Embodiment one illustrates present embodiment, naval vessel sourceless seism rocket projectile fixed transmission of the invention with reference to Fig. 1-Fig. 5
The combustion gas stream of engine emission is to the damaging influence on naval vessel itself and neighbouring equipment when air deflector is to solve rocket bomb transmitting
And a kind of security fence device designed, it is particularly suitable for the middle-size and small-size naval vessel of warship face characteristics of compact layout and aluminium-alloy hull knot
The light ship of structure.The injection stream of emitter playpipe can not only be smoothly oriented in atmospheric environment by the air deflector of the application,
And the sideways diffusion coverage of injection stream can be controlled, while it does not interfere with emitter and periphery warship in application
The normal use of ship equipment, shape, size have also been dissolved into the global design on naval vessel.
Specifically, the naval vessel sourceless seism rocket projectile fixed transmission air deflector, including baffle, the baffle includes
Support plate 2, the first water conservancy diversion panel 3 and the second water conservancy diversion panel 4.The first water conservancy diversion panel 3 and the second water conservancy diversion panel 4, which tilt, to be set
It puts, the second water conservancy diversion panel 4 is connected with 1 phase of the first water conservancy diversion panel, the arranged on left and right sides of the first water conservancy diversion panel 3 and the second water conservancy diversion panel 4
It is turned-out to fold an acclivitous effluent panel 5.Support plate 2 be respectively welded the outside that is fixed on effluent panel 5 and
The rear side of second water conservancy diversion panel 4.
The support plate 2 of left and right sides and rear side, the first water conservancy diversion panel 3 and the second water conservancy diversion panel 4 collectively form the air deflector
Water conservancy diversion frame.And first the channelization angle α of water conservancy diversion panel 3 meet relationship：α<90°-λ1, wherein, α is leading for the first water conservancy diversion panel
Flow angle, λ1Folder between the playpipe for the fixed elevation maximum for being emitter under emission maximum angle state and level ground
Angle.The channelization angle β of second water conservancy diversion panel 4 should meet relationship：β<90°-λ2, wherein, channelization angles of the β for the second water conservancy diversion panel, λ2For
Angle between the playpipe of fixed elevation minimum of the emitter under minimum launch angle state and level ground.Therefore,
The air deflector of the application is made of two diversion sections.
During the naval vessel sourceless seism rocket projectile fixed transmission air deflector is designed, design method specifically includes
Following steps：
Step 1：The emission parameter of emitter is obtained, the outlet that the emission parameter includes rocket engine playpipe is straight
The parameters such as diameter, export expansion half-angle.
Step 2：It is emulated to obtain its wake flame spray regime according to the emission parameter of emitter.
The wake flame spray regime that emulation obtains emitter is as follows：
Step 2.1：Determine the arrangement of emitter, the arrangement includes a variety of emission states, each transmitting
State corresponds to unique launch angle；In this example, it is assumed that emitter has 3 kinds of emission states, respectively 22 °, 32 ° and
40 ° of angles of departure.
Step 2.2：The launch angle of emitter is adjusted, analog simulation goes out emitter under each emission state successively
Wake flame injection stream；
Specifically, first, the current launch angle of emitter and its fixed elevation of each playpipe are determined, it is assumed that transmitting
There are 3 playpipes on device, the fixed elevation of first playpipe is a, and the fixed elevation of second playpipe is b, and third is a
The fixed elevation of playpipe is c, and a<b<C, and assume current emitter launch angle be 32 °.Then, it is filled according to transmitting
Current launch angle and the outlet diameter of a certain playpipe, export expansion half-angle and the fixed elevation put, with its export expansion
The extended line on boundary simulates the pipe inspection stream of the playpipe for the boundary streamline of its wake flame, i.e., along the launch angle of emitter
Extended line is made in direction from the jet exit of the first playpipe by its half angle value of expansion, and the region which is formed can generation
The pipe inspection stream of the first playpipe of table.Then, then successively simulate the pipe inspection stream of the second playpipe and third playpipe.Again will
The pipe inspection stream of these three playpipes merges, and obtains wake flame injection stream of the emitter under 32 ° of angle of departure states.
The launch angle of emitter is adjusted, simulates emitter respectively according to above-mentioned steps in 22 ° and 40 ° of angles of departure
Wake flame injection stream under state.
Step 2.3：Wake flame injection stream under each emission state is merged, obtains the total injection stream of wake flame；It will send out
Wake flame injection stream of the injection device under 22 °, 32 ° and 40 ° these three emission states merges, and obtains the total injection stream of its wake flame.
Step 2.4：The injection cross section of the total injection stream of wake flame above deck is simulated, the injection cross section is to emit
The wake flame spray regime of device.
Step 3：The guide face size of air deflector is determined according to the wake flame spray regime of emitter, the size of guide face should
More than wake flame spray regime, the guide face includes the first guide face and the second guide face, the first guide face and the second guide face
Mutually it is connected.
Step 4：Determine the channelization angle of air deflector guide face；
The track that flows to of combustion gas stream is analyzed according to Hydrodynamics Theory, in order to by the wake flame injection stream of emitter
It is smoothly oriented in atmospheric environment, the channelization angle α of the first guide face should meet relationship：α<90°-λ1, wherein, α is the first guide face
Channelization angle (i.e. the angle of the first guide face and horizontal plane), λ1It is faced upward for fixation of the emitter under emission maximum angle state
Angle between the playpipe of angle maximum and level ground；The channelization angle β of second guide face should meet relationship：β<90°-λ2,
In, channelization angles (i.e. the angle of second guide face and horizontal plane) of the β for the second guide face, λ2It is emitter in the minimum angle of departure
Angle between the playpipe of fixed elevation minimum under degree state and level ground.
Step 5：The arranged on left and right sides of guide face is turned-out respectively to fold an acclivitous effluent face.
When the wake flame of emitter is acted on the guide face of air deflector, the flow direction of combustion gas stream along water conservancy diversion in addition to facing upward
Movement, while can also carry out discrete type diffusion along guide face.Sideways diffusion to avoid combustion gas stream influences ship-borne ambient and (emits
Warship face equipment around device), the track that flows to of combustion gas stream is analyzed it is found that guide face both sides according to Hydrodynamics Theory
Effluent face lateral inclination angle it is smaller, then laterally dispersion combustion gas stream generate edge upwarp type face cross component force it is bigger, cause
The lateral flow of combustion gas stream is happier.Otherwise when lateral inclination angle is excessive, the lateral thrust that decomposites reduces, and combustion gas stream is along side
The flow in type of tilting upward face is reduced, it is possible to create part packing phenomenon, therefore the elongated surfaces in effluent face should be set positioned at surrounding warship face
Standby top.Inventor by groping for a long time, studying and a large amount of emulation experiment is found, when effluent face and guide face it
Between angle be not less than 20 ° when, the injection wake flame of transmitting tube will not impact surrounding warship face equipment.
Step 6：According to guide face size and its channelization angle, the angle of inclination in effluent face, air deflector model is built, to setting
The wake flame injection stream for having the emitter of air deflector is emulated, and obtains the temperature cloud picture of ship-borne ambient and pressure cloud atlas, according to
The temperature and pressure situation of temperature cloud picture and pressure nephanalysis warship face different zones, according to analysis result adjust guide face and/
Or the arrange parameter (size, the channelization angle of guide face or the angle of inclination of inclined surface that adjust guide face) in effluent face, so as to
Adjustment is optimized to the structure of air deflector.
Embodiment two, the difference lies in offer multiple uniform the present embodiment in the support plate 2 with embodiment one
The lightening hole 6 of distribution, the lightening hole 6 opened up had not only interfered with the structural-load-carrying capacity of air deflector, but also can mitigate its weight, made it
Shape, weight, size have been dissolved into the master-plan on naval vessel, to meet naval vessel overall weight and carrying in terms of design will
It asks, other specific embodiments are identical with embodiment one, specifically repeat no more.
Embodiment three, the difference lies in air deflector needs the present embodiment during use with embodiment one or two
It is fixed on ship deck, since air deflector is made of steel material, Ship Structure is aluminum material, therefore, is led using
During flowing device, the transition being considered as between steel air deflector and aluminum Ship Structure connects, therefore, in air deflector and naval vessel
One transit joint 1 is set between deck.The transit joint 1 is made of an aluminium sheet and a steel plate, aluminium sheet and steel plate it
Between be fixed by gluing.The aluminum deck of transit joint 1 is mutually fixed with Ship Structure, and the bottom plate of steel facing and air deflector is mutually solid
It is fixed.In order to not influence the normal use of emitter, at the same nor affect on handling rocket projectile, weapon penetrate it is preceding prepare, equipment detection
And the work such as maintenance are normally carried out, and during use, air deflector are fixed on range transmission device playpipe and is gone out
At the position of mouth 300mm-500mm., other specific embodiments are identical with embodiment one or two, specifically repeat no more.
Finally it should be noted that：The above embodiments are merely illustrative of the technical scheme of the present invention and are not intended to be limiting thereof；To the greatest extent
The present invention is described in detail with reference to preferred embodiments for pipe, those of ordinary skills in the art should understand that；Still
It can modify to the specific embodiment of the present invention or equivalent replacement is carried out to some technical characteristics；Without departing from this hair
The spirit of bright technical solution should all cover in the claimed technical solution range of the present invention.
Claims (4)
1. a kind of naval vessel sourceless seism rocket projectile fixed transmission air deflector, which is characterized in that including baffle, the baffle packet
Include the first water conservancy diversion panel, the second water conservancy diversion panel being mutually connected with the first water conservancy diversion panel, support plate, the first water conservancy diversion panel and
Two water conservancy diversion panels are obliquely installed, the arranged on left and right sides of the first water conservancy diversion panel and the second water conservancy diversion panel it is turned-out fold one to
Upper inclined effluent panel, the support plate be fixed on vertically respectively on effluent panel and the trailing flank of the second water conservancy diversion panel on.
2. naval vessel sourceless seism rocket projectile fixed transmission air deflector according to claim 1, which is characterized in that the support
Multiple equally distributed lightening holes are offered on plate.
3. naval vessel sourceless seism rocket projectile fixed transmission air deflector according to claim 1, which is characterized in that the water conservancy diversion
The distance between device and emitter playpipe outlet is 300mm-500mm, and air deflector is fixed on ship deck, air deflector with
Transit joint is provided between ship deck, the transit joint is made of aluminium sheet and steel plate, passes through glue between aluminium sheet and steel plate
It is viscous to be fixed.
4. naval vessel sourceless seism rocket projectile fixed transmission air deflector according to claim 1, which is characterized in that described first
The channelization angle α of water conservancy diversion panel guide face meets relationship：α<90°-λ1, wherein, channelization angles of the α for the first water conservancy diversion panel, λ1For transmitting
Angle between the playpipe of fixed elevation maximum of the device under emission maximum angle state and level ground；
The channelization angle β of second guide face should meet relationship：β<90°-λ2, wherein, channelization angles of the β for the second water conservancy diversion panel, λ2For hair
Angle between the playpipe of fixed elevation minimum of the injection device under minimum launch angle state and level ground；
Angle between the effluent panel and the first water conservancy diversion panel or the second water conservancy diversion panel is not less than 20 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711400421.3A CN108177747B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711098007.1A CN108177746B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector and design method thereof |
| CN201711400421.3A CN108177747B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711098007.1A Division CN108177746B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector and design method thereof |
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| Publication Number | Publication Date |
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| CN108177747A true CN108177747A (en) | 2018-06-19 |
| CN108177747B CN108177747B (en) | 2020-08-04 |
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| CN201711098007.1A Active CN108177746B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector and design method thereof |
| CN201711400421.3A Active CN108177747B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector |
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| CN201711098007.1A Active CN108177746B (en) | 2017-11-09 | 2017-11-09 | Ship passive interference rocket projectile fixed launching deflector and design method thereof |
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| CN110131076B (en) * | 2019-04-23 | 2020-05-08 | 湖北三江航天江北机械工程有限公司 | Modularized forming method of fluid director |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105971769A (en) * | 2016-07-13 | 2016-09-28 | 西安航天动力测控技术研究所 | Fuel gas guide device for vertical type test run of small solid rocket engine |
| CN106247855A (en) * | 2016-09-13 | 2016-12-21 | 湖北航天技术研究院总体设计所 | A kind of liftable transmitting station of air deflector |
| CN107131794A (en) * | 2017-07-04 | 2017-09-05 | 北京理工大学 | A kind of truck-mounted missile launches double-arc shape air deflector |
| CN107144170A (en) * | 2017-07-04 | 2017-09-08 | 北京理工大学 | A kind of big cambered surface air deflector of monoblock type for Vertical Launch duplex multiple missile |
| CN107202515A (en) * | 2017-07-04 | 2017-09-26 | 北京理工大学 | One kind turns to twist research platform gas diversion device |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1357976A (en) * | 1972-01-04 | 1974-06-26 | British Aircraft Corp Ltd | Missile launchers |
| US5127609A (en) * | 1991-02-25 | 1992-07-07 | Lynn B Stanley | Jet blast deflector fence |
| FR2934041B1 (en) * | 2008-07-17 | 2011-07-01 | Dcns | ARMS SYSTEM, IN PARTICULAR FOR MISSILES, INTENDED TO BE INTEGRATED INTO A COMBAT PLATFORM AND CORRESPONDING COMBAT PLATFORM |
| CN106347702B (en) * | 2016-08-24 | 2018-07-27 | 东南大学 | A kind of gas-jetting flow-guiding plate |
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2017
- 2017-11-09 CN CN201711098007.1A patent/CN108177746B/en active Active
- 2017-11-09 CN CN201711400421.3A patent/CN108177747B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105971769A (en) * | 2016-07-13 | 2016-09-28 | 西安航天动力测控技术研究所 | Fuel gas guide device for vertical type test run of small solid rocket engine |
| CN106247855A (en) * | 2016-09-13 | 2016-12-21 | 湖北航天技术研究院总体设计所 | A kind of liftable transmitting station of air deflector |
| CN107131794A (en) * | 2017-07-04 | 2017-09-05 | 北京理工大学 | A kind of truck-mounted missile launches double-arc shape air deflector |
| CN107144170A (en) * | 2017-07-04 | 2017-09-08 | 北京理工大学 | A kind of big cambered surface air deflector of monoblock type for Vertical Launch duplex multiple missile |
| CN107202515A (en) * | 2017-07-04 | 2017-09-26 | 北京理工大学 | One kind turns to twist research platform gas diversion device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108177746B (en) | 2020-08-04 |
| CN108177747B (en) | 2020-08-04 |
| CN108177746A (en) | 2018-06-19 |
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