CN108562189A - A kind of sounding rocket emitter - Google Patents
A kind of sounding rocket emitter Download PDFInfo
- Publication number
- CN108562189A CN108562189A CN201810229541.XA CN201810229541A CN108562189A CN 108562189 A CN108562189 A CN 108562189A CN 201810229541 A CN201810229541 A CN 201810229541A CN 108562189 A CN108562189 A CN 108562189A
- Authority
- CN
- China
- Prior art keywords
- vertical arm
- emitter
- trunnion seat
- slewing equipment
- sounding rocket
- Prior art date
- 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.)
- Granted
Links
Classifications
-
- 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 provides a kind of sounding rocket emitter, hanging filling under which uses, and spiral lift, which rises, to be erected, and perpendicular, revolute function, easy to operate, high reliability are played with full-automatic.The sounding rocket emitter includes pedestal, slewing equipment, spiral lift, plays vertical arm, auxiliary support apparatus and cross-brace device.Wherein slewing equipment is mounted on pedestal, and slewing equipment can be rotated relative to ground, and the emitter is made to have azimuth automatic regulating function；Trunnion seat is fixed on slewing equipment, plays vertical arm and trunnion seat pin joint, is being played rocket horizontal loading below vertical arm using hanging under machinery, and the perpendicular transmitting of rocket is realized by spiral lift.
Description
Technical field
The present invention relates to a kind of rocket projectors, and in particular to a kind of sounding rocket emitter.
Background technology
Traditional sounding rocket takes support type to emit, and rocket is seated in guide rail finder groove by the horizontal pop-up of sliding block
Interior, guide rail has been screwed to by bolt in vertical arm.Rocket needs crane lifting rocket when loading.
Traditional rocket launching executing agency is the hydraulic cylinder in hydraulic system, and vertical arm has been pushed to complete perpendicular action.It needs
It is equipped with hydraulic system, and load and direction change can occur for hydraulic cylinder in countdown, transmitting is caused to shake, held
Fragile equipment.
Traditional rocket, which rises, to be erected using quadrant observation pitch angle variation, when close to pitch angle is emitted, using artificial behaviour
The mode for making to finely tune reaches transmitting pitch angle；Rocket directive is determined using transit survey；Do not have automatic regulating function.
Invention content
In view of this, the present invention provides a kind of full-automatic air sounding rocket projector, hanging dress under which uses
Fill out, spiral lift rise it is perpendicular, have it is full-automatic play perpendicular, revolute function, it is easy to operate, precision is high, reliability is high.
The sounding rocket emitter includes：Pedestal, spiral lift, plays vertical arm and trunnion seat at slewing equipment；
The foundation plate of the pedestal and launching level ground is affixed；The trunnion seat is mounted on described by slewing equipment
On pedestal, one end of described vertical arm and the journal stirrup pin joint in the trunnion seat；The trunnion seat and play vertical arm can be
It is rotated around vertical direction under the drive of the slewing equipment, to change the azimuth of emitter；
The spiral lift is bolt and nut matching mechanism, and one end of screw rod is hinged with vertical arm is played, and is set at the end
It is equipped with the motor for driving the screw rod rotation；The other end is connected with nut, the upper journal of the nut and trunnion seat
It is hinged；
Hanging filling under sounding rocket to be launched uses, the i.e. length direction along described vertical arm have been mounted on vertical arm
Lower section；It rotates under the drive of spiral lift, is aimed at any angle between so that emitter is realized 0 ° to 90 °.
The slewing equipment includes：Upper flange, rotary disk and lower flange, the rotary disk include rotating part and fixed part
Point；The rotating part of the rotary disk is connected by upper flange and trunnion seat；Fixed part is connected by lower flange and pedestal
It connects.
Further include cross-brace device, the cross-brace device has been supported on the one end of lower section far from pedestal of vertical arm；
When described vertical arm is in horizontality, one end is filled by journal stirrup and trunnion seat pin joint, the other end by the cross-brace
Set support.
In the trunnion seat, the opposite side for playing vertical arm is equipped with for when described vertical arm is in vertical state pair
It carries out the auxiliary support apparatus of Auxiliary support.
Advantageous effect：
(1) hanging filling emission mode is compared with traditional support type filling under the emitter uses, and avoids execution
The impact of load is born by mechanism, is not necessarily to crane lifting, saves the activity duration, reduces manpower and materials cost.
(2) pitch angle, azimuth tune can distally be automatically controlled by using electric screw elevator driven type to play perpendicular, slewing equipment
Section and locking, for pitching precision up to 0.1 °, launcher beam overall length 12m, can meet 3 tons of rockets of quality plays perpendicular transmitting.
(3) it plays vertical arm with trunnion seat to be connected, be connected by slewing equipment between trunnion seat and pedestal, slewing equipment phase
Ground can be rotated, thus emitter has azimuth automatic regulating function, avoids legacy transmission tool face azimuth
The problem of needing integral demounting to reset when adjustment；And slewing equipment uses integrated form device for revolving and driving, inclines with small, anti-
Cover the strong feature of ability.
(4) it plays vertical arm and uses variable cross-section truss structure, light weight, rigidity is big；Segmented splices guide rail and uses integral installation,
Solve the problems, such as Large Complicated Structural Component compatibility of deformation and great cantilever long guideway load deformation problems.Guide Rail Design, which mounts, to be connect
Mouthful, it is adapted to small rockets launch and mounts requirement.
(5) horizontality and the peace under vertical state are realized by the way that cross-brace device and auxiliary support apparatus are reliable respectively
Full protection, reducing vibration when transmitting influences executing agency.
(6) trunnion seat weight body, inside are filled with clump weight, slewing equipment can be reduced in trunnion seat rear design
The tilting moment given by vertical arm is played, prevents emitter sideways.
(7) important feature part is designed with gas diversion protective cover on emitter, can effectively prevent high temperature and high speed combustion gas
Structural member destroys caused by stream impact.
Description of the drawings
Fig. 1 is the structural schematic diagram of the emitter；
Fig. 2 is the schematic diagram that the emitter plays vertical state.
Wherein：1- plays vertical arm, the manual tackles of 2-, 3- cross-braces device, 4- rockets, 5- spiral lifts, 6- ears
Shaft stool, 7- slewing equipments, 8- combustion gas protective plate, 9- pedestals, 10- auxiliary support apparatus.
Specific implementation mode
The present invention will now be described in detail with reference to the accompanying drawings and examples.
The present embodiment provides a kind of sounding rocket emitters of full-automatic high precision, are not more than for launch quality
3000kg, effective meteorological sounding altitude 350km and sounding rocket below.
As depicted in figs. 1 and 2, which includes pedestal 9, slewing equipment 7, spiral lift 5, rises and erect
Arm 1, auxiliary support apparatus 10, trunnion seat 6 and cross-brace device 3.
Wherein pedestal 8 and 6 main part of trunnion seat is formed using cast steel casting, and ultrasonic examination, essence are carried out after casting
Processing.The truss mechanism that vertical arm 1 is combined using steel pipe and channel steel is played, and is aided with the welding such as reinforcing rib, time processing after welding
It forms；The guide rail risen in vertical arm 1 is spliced by three short lead rails, is finished after pin dress.
The emitter is integrally assemblied on foundation plate, and foundation plate is embedded in launching level ground.When assembled in situ,
Pedestal 9 is fixed on foundation plate with bolt, 9 position of pedestal, wherein access hole center are placed according to basic directive
Corresponding reinforcing rib is basic directive.
Slewing equipment 7 is installed by lower flange in 9 upper surface of pedestal, the slewing equipment 7 uses integrated form revolution driving
Device, including upper flange, rotary disk and lower flange, the rotary disk is using single driving rotary disk comprising on rotary
Portion and fixed lower part.The rotary top of rotary disk and the lower surface of upper flange connect, top and the trunnion branch of upper flange
The lower surface connection of seat 6；The lower surface for the lower part that rotary disk cannot rotate is connected with the upper surface of lower flange, under lower flange
Surface is connect with pedestal 9, is worm gear structure inside the rotary disk, drives worm screw rotation, worm screw to drive by servo motor
Turbine rotation, to realize the rotation of rotary disk, and then drive trunnion seat and thereon play vertical arm and rocket turns round together, i.e.,
Realize that upper journal can be rotated with opposite base (ground).The integrated form revolution driving is integrated with worm and gear deceleration, pivoting support
Function, have the characteristics that small, resistance to capsizing is strong.
When installation, it is ensured that the axis of servo motor is parallel to basic directive in slewing equipment 7, and trunnion seat 6 passes through upper method
Orchid is mounted on the top of the slewing equipment 7, it is ensured that (journal stirrup has been that vertical arm connects with trunnion seat to journal stirrup after described after trunnion seat
The journal stirrup connect, the center line for playing vertical arm are parallel with the journal stirrup direction) direction is consistent with basic directive.When initial, play vertical arm 1 and be in
Horizontality, plays one end of vertical arm 1 by journal stirrup and 6 pin joint of trunnion seat, and the bottom of the other end passes through 3, cross-brace device
The security protection under horizontality is realized in support.Spiral lift 5 is bolt and nut matching mechanism, one end of screw rod with rise it is perpendicular
Arm 1 is hinged, and the end is provided with the motor for driving the screw rod rotation；The other end is connected with nut, the nut
It is hinged with the upper journal of trunnion seat 6.When motor drives screw rod to rotate forward, nut is moved in a straight line along screw rod, screw rod
Become smaller at a distance from one end for being connected of vertical arm and nut with rising, since nut is hinged on upper journal, distance becomes smaller reality
On be that screw rod pull-up plays vertical arm, has completed perpendicular rise and has acted.When reversion, screw rod with rise one end for being connected of vertical arm and nut away from
From becoming larger, lowering action is completed.
In the trunnion seat 6, auxiliary support apparatus 10 is installed in the opposite side for playing vertical arm 1, when emitter is in
When vertical state, auxiliary support apparatus 10 has realized the security protection under vertical state.
The side that auxiliary support apparatus 10 is installed in the trunnion seat 6 is provided with shaft stool weight body, and inside is filled with
Clump weight.
The operation principle of the emitter is：
When emitting sounding rocket using the emitter, control system is used to carry out initial orientation footmark first fixed.Then
Hanging filling under rocket is carried out with docking unwheeling and manual tackles, i.e., is horizontally arranged at sounding rocket installation to be launched
Play the lower section of vertical arm 1.
Then emitter pitch angle and azimuthal adjustment are carried out respectively：When emitter pitch angle adjusts, spiral shell is controlled
The leading screw rotation for playing perpendicular motor work, driving in spiral lift in elevator is revolved, has been pulled by fixed copper nut perpendicular
Arm has completed perpendicular action.When pitch angle is close to required value, pitch angle Adjustment precision is improved by feedback modifiers.Emitter orientation
When angle adjusts, the turning motor work in slewing equipment is controlled, vertical arm and trunnion seat has been driven while having turned round, completes transmitting dress
Azimuth adjustment is set, azimuth Adjustment precision is improved by feedback modifiers.After pitch angle and azimuth are adjusted to required value,
Device, which is controlled, by hair emits sounding rocket.
When needing to carry out sounding rocket windage yaw amendment, rising in the turning motor and spiral lift in slewing equipment is perpendicular
Motor works at the same time, and vertical arm and trunnion seat has been driven to be turned round while playing perpendicular, completes the adjustment of emitter sighting angle, improves
Adjustment precision and adjustment time.
In conclusion the above is merely preferred embodiments of the present invention, being not intended to limit the scope of the present invention.
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in the present invention's
Within protection domain.
Claims (7)
1. a kind of sounding rocket emitter, which is characterized in that including：Pedestal (9), slewing equipment (7), spiral lift (5),
Play vertical arm and trunnion seat (6)；
The pedestal (9) and the foundation plate of launching level ground are affixed；The trunnion seat (6) is installed by slewing equipment (7)
On the pedestal (9), one end and the journal stirrup pin joint in the trunnion seat (6) of described vertical arm (1)；The trunnion seat
(6) it can be rotated around vertical direction under the drive of the slewing equipment (7) with vertical arm (1), to change the side of emitter
Parallactic angle；
The spiral lift (5) is bolt and nut matching mechanism, and one end of screw rod is hinged with vertical arm (1) is played, and at the end
It is provided with the motor for driving the screw rod rotation；The other end is connected with nut, and the nut is upper with trunnion seat (6)
Journal stirrup is hinged；
Hanging filling under sounding rocket to be launched uses, the i.e. length direction along described vertical arm (1) have been mounted on vertical arm (1)
Lower section；It rotates under the drive of spiral lift (5), is aimed at any angle between so that emitter is realized 0 ° to 90 °.
2. sounding rocket emitter as described in claim 1, which is characterized in that the slewing equipment includes：Upper flange returns
Turntable and lower flange, the rotary disk include rotating part and fixed part；The rotating part of the rotary disk passes through upper flange
With being connected for trunnion seat (6)；Fixed part is connect by lower flange with pedestal (9).
3. sounding rocket emitter as claimed in claim 1 or 2, which is characterized in that further include cross-brace device (3),
The cross-brace device (3) has been supported on the one end of lower section far from pedestal (9) of vertical arm (1)；Described vertical arm (1) is in water
When level state, one end is supported by journal stirrup and trunnion seat (6) pin joint, the other end by the cross-brace device (3).
4. sounding rocket emitter as claimed in claim 1 or 2, which is characterized in that in the trunnion seat (6), rise
The opposite side of vertical arm (1) is equipped with for carrying out the auxiliary of Auxiliary support to it when described vertical arm (1) is in vertical state
Support device (10).
5. sounding rocket emitter as claimed in claim 1 or 2, which is characterized in that described vertical arm (1) is steel pipe and slot
The truss structure that steel is combined.
6. sounding rocket emitter as claimed in claim 1 or 2, which is characterized in that the guide rail is spliced using segmented
Structure.
7. sounding rocket emitter as claimed in claim 1 or 2, which is characterized in that in the trunnion seat (6), rise
The opposite side of vertical arm (1) is provided with trunnion seat weight body, and clump weight is filled with inside weight body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810229541.XA CN108562189B (en) | 2018-03-20 | 2018-03-20 | A kind of sounding rocket emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810229541.XA CN108562189B (en) | 2018-03-20 | 2018-03-20 | A kind of sounding rocket emitter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108562189A true CN108562189A (en) | 2018-09-21 |
| CN108562189B CN108562189B (en) | 2019-08-23 |
Family
ID=63532811
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810229541.XA Withdrawn - After Issue CN108562189B (en) | 2018-03-20 | 2018-03-20 | A kind of sounding rocket emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108562189B (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109764749A (en) * | 2018-12-07 | 2019-05-17 | 湖北航天飞行器研究所 | Rocket weapon or transmitter emission system and method |
| CN110260713A (en) * | 2019-07-19 | 2019-09-20 | 北京航天发射技术研究所 | A kind of the revolution axis mechanism and its interconnection method of rocket launching rack |
| CN110274520A (en) * | 2019-06-13 | 2019-09-24 | 蓝箭航天空间科技股份有限公司 | Perpendicular device and rocket launching auxiliary system are played for rocket launching |
| CN110332852A (en) * | 2019-07-19 | 2019-10-15 | 北京航天发射技术研究所 | Buffer unit and buffer control method for rocket flexible cable Erecting System |
| CN110360882A (en) * | 2019-07-19 | 2019-10-22 | 北京航天发射技术研究所 | A kind of rocket off-shore launching platform frame and the method for playing perpendicular rocket |
| CN110949228A (en) * | 2018-12-20 | 2020-04-03 | 中国人民解放军63921部队 | Multistage rocket transport erecting vehicle |
| CN110962722A (en) * | 2018-12-20 | 2020-04-07 | 中国船舶重工集团应急预警与救援装备股份有限公司 | Space truss type rocket erecting arm |
| CN110963421A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Multifunctional rocket transport erecting vehicle |
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| RU2232968C1 (en) * | 2002-11-10 | 2004-07-20 | Открытое акционерное общество "Конструкторское бюро специального машиностроения" | Shipboard rocket launcher and method for its deployment |
| CN102680261A (en) * | 2012-05-10 | 2012-09-19 | 冉磊 | Rotary inclined test bed device |
| CN203271242U (en) * | 2013-04-28 | 2013-11-06 | 湖北三江航天万峰科技发展有限公司 | Spiral tower body lifting device |
| CN105605977A (en) * | 2016-02-02 | 2016-05-25 | 北京航天发射技术研究所 | High-load multifunctional firing platform |
| CN106428655A (en) * | 2015-08-13 | 2017-02-22 | 贵州航天天马机电科技有限公司 | Self-adaptive propulsion mounting system for erecting frame of launch vehicle |
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2018
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Patent Citations (5)
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| RU2232968C1 (en) * | 2002-11-10 | 2004-07-20 | Открытое акционерное общество "Конструкторское бюро специального машиностроения" | Shipboard rocket launcher and method for its deployment |
| CN102680261A (en) * | 2012-05-10 | 2012-09-19 | 冉磊 | Rotary inclined test bed device |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109764749B (en) * | 2018-12-07 | 2022-03-25 | 湖北航天飞行器研究所 | Method for launching a rocket weapon or launcher launching system |
| CN109764749A (en) * | 2018-12-07 | 2019-05-17 | 湖北航天飞行器研究所 | Rocket weapon or transmitter emission system and method |
| CN110963421A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Multifunctional rocket transport erecting vehicle |
| CN110949228A (en) * | 2018-12-20 | 2020-04-03 | 中国人民解放军63921部队 | Multistage rocket transport erecting vehicle |
| CN110962722A (en) * | 2018-12-20 | 2020-04-07 | 中国船舶重工集团应急预警与救援装备股份有限公司 | Space truss type rocket erecting arm |
| CN110274520A (en) * | 2019-06-13 | 2019-09-24 | 蓝箭航天空间科技股份有限公司 | Perpendicular device and rocket launching auxiliary system are played for rocket launching |
| CN110274520B (en) * | 2019-06-13 | 2020-09-01 | 蓝箭航天空间科技股份有限公司 | Erecting device for rocket launching and rocket launching auxiliary system |
| CN110332852A (en) * | 2019-07-19 | 2019-10-15 | 北京航天发射技术研究所 | Buffer unit and buffer control method for rocket flexible cable Erecting System |
| CN110360882A (en) * | 2019-07-19 | 2019-10-22 | 北京航天发射技术研究所 | A kind of rocket off-shore launching platform frame and the method for playing perpendicular rocket |
| CN110260713B (en) * | 2019-07-19 | 2021-08-17 | 北京航天发射技术研究所 | Rotating shaft mechanism of rocket launching stand and butt joint method thereof |
| CN110360882B (en) * | 2019-07-19 | 2021-08-27 | 北京航天发射技术研究所 | Rocket marine launching rack and rocket erecting method |
| CN110332852B (en) * | 2019-07-19 | 2021-08-27 | 北京航天发射技术研究所 | Buffer device for rocket flexible steel cable erecting system and buffer control method |
| CN110260713A (en) * | 2019-07-19 | 2019-09-20 | 北京航天发射技术研究所 | A kind of the revolution axis mechanism and its interconnection method of rocket launching rack |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108562189B (en) | 2019-08-23 |
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