CN104142092B - Rocket launching umbilical tower - Google Patents
Rocket launching umbilical tower Download PDFInfo
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- CN104142092B CN104142092B CN201410339987.XA CN201410339987A CN104142092B CN 104142092 B CN104142092 B CN 104142092B CN 201410339987 A CN201410339987 A CN 201410339987A CN 104142092 B CN104142092 B CN 104142092B
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- tower
- umbilical
- umbilical tower
- rocket launching
- cube
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Abstract
Rocket launching umbilical tower of the present invention is related to a kind of rocket launching equipment.Its purpose is to provide a kind of bearing capacity strong umbilical tower.Rocket launching umbilical tower of the present invention, the umbilical tower is box tall and slender structure, the base of the umbilical tower is trapezoidal pedestal, which is provided with multistage cube tower body, the trapezoidal pedestal is spirally connected with described cube of tower body, it is also adopted by being spirally connected between described cube of tower body each tower section, reinforcement gusset and reinforcement sand frame are additionally provided with inside the umbilical tower, the deep floor includes transversely stiffened plate and longitudinally reinforced floor, the reinforcement sand frame coordinates with the perforate on the umbilical tower, to increase the intensity that perforate goes out, umbilical tower is the box tall and slender structure of lower thick upper thin, ensure that the intensity of umbilical tower, rigidity and stability, tower body is three sections of structures being fixedly connected, it is easy to the transport of umbilical tower, lifting and installation, reinforcement sand frame is provided with the position that hole is offered on umbilical tower, prevent local buckling.
Description
Technical field
The present invention relates to a kind of rocket launching part, more particularly to a kind of rocket launching auxiliary equipment.
Background technology
New generation's carrier rocket launching site is located in seashore, and to adapt to local weather conditions, carrier rocket uses " new three
Hang down " survey hair flow：The assembling and test of rocket and related system are completed in technical preparation building, rocket is then transported to transmitting battle array
Ground, needs to use umbilical tower, umbilical tower to be arranged on movable launch platform during rocket transition, and umbilical tower is mainly used in holding
Carry swing rod and miscellaneous equipment, in rocket body is transported to the transportation of launching site by technical preparation building carry filling supply air line,
The equipment such as satellite cable, air-conditioning duct, equipment is constant with terrestrial interface state in keeping transportation；Umbilical tower before rocket launching
On swing rod swing, the connector for having come off, pipeline etc. are swung into safety zone, be that rocket takes off and concedes escape way, but
The design of umbilical tower is limited by movable launch platform space, and umbilical tower is an elongated tall and slender structure, and rigidity is poor, after stand under load
It is easily deformed, causes main shaft upper bracket displacement, main shaft clamping stagnation may be caused, trigger motion failure, the lighter can causes relevant zero
Part is damaged, and severe one even makes swing rod to complete oscillating motion.
The content of the invention
The technical problem to be solved in the present invention is to provide the rocket launching that a kind of bearing capacity is strong, intensity is high, rigidity is high and uses
Umbilical tower.
Rocket launching umbilical tower of the present invention, the umbilical tower is box tall and slender structure, and the base of the umbilical tower is ladder
Shape pedestal, which is provided with multistage cube tower body, and the trapezoidal pedestal is fixedly connected with described cube of tower body, and described cube of tower body is each
Also it is fixedly connected between individual tower section, the trapezoidal pedestal of the umbilical tower is equipped with deep floor and reinforcement with the inside of each tower section
Insert, the deep floor includes transversely stiffened plate and longitudinally reinforced floor, and the reinforcement insert is fixedly mounted on the navel
On the inwall of the tapping on each section of cube tower body with tower 1, to increase the intensity of tapping.
Rocket launching umbilical tower of the present invention, wherein the umbilical tower is made of Q345 shape steel plates, the steel plate thickness
Not less than 10mm.
Rocket launching umbilical tower of the present invention, wherein the transversely stiffened plate is T-shaped or L-type structure floor, the horizontal stroke
To deep floor 500mm high, the longitudinally reinforced floor is the trapezium structure plate with opening.
Rocket launching umbilical tower of the present invention, wherein being connected by the double bolt of inner flange between described each tower section
Connect, rigid protective set is provided with the outside of the bolt.
Rocket launching umbilical tower of the present invention, wherein be additionally provided with top cover at the top of the umbilical tower, the top cover with it is described
Umbilical tower is fixedly connected, and the top cover is trapezoid boss shape, and its inclined-plane is 15 degree with the angle of horizontal plane, the surrounding of the top cover
It is additionally provided with multiple inside with the umbilical tower and connects several ventilating openings, is provided with separation net at described each ventilating opening, institute
State and be additionally provided with the outside of top cover lightning rod and wind speed detector.
Rocket launching umbilical tower of the present invention, wherein being provided with multiple illuminating lamps, the umbilical cord in the umbilical tower base
Tower base is provided with access door away from the one side of rocket, is provided with the access door for controlling umbilical tower intraoral illumination lamp
Light switch.
Rocket launching umbilical tower of the present invention, wherein being provided with several emergency lights in the umbilical tower.
Rocket launching umbilical tower of the present invention and prior art service tower difference are that umbilical tower of the present invention is box
Tall and slender structure, it is ensured that the bottom strength of umbilical tower, rigidity and stability, while alleviating the weight on tower body top；Umbilical tower
By be spirally connected connection, tower body segmental structure consequently facilitating umbilical tower between base and cube tower body, between each section of cube tower body
Transport, lifting and installation；Deep floor and reinforcement insert are internally provided with the umbilical tower, local buckling, enhancing office is prevented
The intensity in portion, and then improve the bearing capacity of whole tower body.
It is attached by the double bolt of inner flange between each section of umbilical tower in rocket launching umbilical tower of the present invention, is passed through
The pretightning force that bolt applies is controlled so as to ensure the reliability of the connection between each section；Bolt is protected in rigid protective set,
So as to be effectively isolated the salt mist environment of surrounding；The thickness of steel plate is not less than 10mm, because umbilical tower is chronically at marine atmosphere ring
In the middle of border, it is to avoid air and salt air corrosion through moisture has influence on the intensity of steel plate, extend the service life of tower body；Umbilical tower
Tower top be designed to surrounding be inclined plane form, so as to prevent rainwater from entering into tower, ventilating opening go out to set separation net prevent
Only birds or other debris are entered into tower；Light switch and emergency light, the peace of the equipment being easy in umbilical tower are set
Illumination needs when filling, overhaul and safeguarding.
Umbilical tower of the invention is described further below in conjunction with the accompanying drawings.
Brief description of the drawings
Fig. 1 is the front view of rocket launching umbilical tower of the present invention；
Fig. 2 is the distribution map of deep floor in rocket launching umbilical tower of the present invention；
Fig. 3 is the tower top front view of rocket launching umbilical tower of the present invention.
Specific embodiment
As shown in Figure 1, Figure 2 and Figure 3, rocket launching umbilical tower 1 of the present invention is box tall and slender structure, the bottom of umbilical tower 1
Seat is trapezoidal pedestal, which is provided with three sections of cubes of tower bodies, between trapezoidal pedestal and cube tower body, between each tower section in
The double bolt of flange is attached, and rigid protective set is provided with the outside of bolt, and umbilical tower 1 is inclined towards the one side of rocket
Face, the distance of inclined plane to rocket is more and more remote from top to bottom, and the trapezoidal pedestal of umbilical tower 1 also sets with each section of inside of tower body
There are reinforcement gusset and reinforcement insert, deep floor includes transversely stiffened plate 2 and longitudinally reinforced floor 3, and transversely stiffened plate 2 is
T-shaped or L-type structure floor, floor 500mm high sets one per 3m, and longitudinally reinforced floor 3 is the trapezium structure with opening
Plate, reinforcement insert patch is welded on the inwall of the tapping on each section of cube tower body of the umbilical tower 1, to increase the strong of tapping
Degree.The position that tower body internal weld seams, seam etc. have corrosion risk after tower body inwall reinforcement is all protected in longitudinally reinforced floor
Within, any surface finish of tower body inwall is this ensures that thered, imperforation can be prevented effectively from deep floor and inner wall of tower closing space
By the corrosion of humid air and salt fog.Umbilical tower 1 is made of Q345 shape steel plates, and steel plate thickness is made according to distribution of force situation etc.
Intensity Design, steel plate thickness is not less than 10mm, and the top of umbilical tower 1 is additionally provided with top cover 4, and top cover 4 is trapezoid boss shape, its inclined-plane
It is 15 degree with the angle of horizontal plane, the surrounding of top cover 4 is additionally provided with multiple several ventilating openings 41 connected with the inside of umbilical tower 1,
Separation net is provided with each ventilating opening 41, the outside of top cover 4 is additionally provided with lightning rod and wind speed detector.The base of umbilical tower 1
Inside be provided with multiple illuminating lamps, the base of umbilical tower 1 is provided with access door away from the one side of rocket, be provided with access door for
Control the light switch of the intraoral illumination lamp of umbilical tower 1, the used time can not remove and be recovered to inside umbilical tower 11 for lightning rod and anemoclinograph.
Several emergency lights are additionally provided with inside umbilical tower 1.
Embodiment described above is only that the preferred embodiment of the present invention is described, not to model of the invention
Enclose and be defined, on the premise of design spirit of the present invention is not departed from, those of ordinary skill in the art are to technical side of the invention
Various modifications and improvement that case is made, all should fall into the protection domain of claims of the present invention determination.
Claims (5)
1. a kind of rocket launching umbilical tower, it is characterised in that：The umbilical tower (1) is box tall and slender structure, the umbilical tower
(1) base is trapezoidal pedestal, which is provided with multistage cube tower body, and the trapezoidal pedestal is fixedly connected with described cube of tower body,
Also it is fixedly connected between described cube of tower body each tower section, the trapezoidal pedestal of the umbilical tower (1) is equal with the inside of each tower section
Deep floor and reinforcement insert are provided with, the deep floor includes transversely stiffened plate (2) and longitudinally reinforced floor (3), described
Transversely stiffened plate (2) is T-shaped or L-type structure floor, the transversely stiffened plate 500mm high, the setting one per 3m, described vertical
It is the trapezium structure plate with opening to deep floor (3), the reinforcement insert is fixedly mounted on each section of the umbilical tower (1)
On the inwall of the tapping on cube tower body, to increase the intensity of tapping, top cover is additionally provided with the top of the umbilical tower (1)
(4), the top cover (4) is fixedly connected with the umbilical tower (1), and the top cover (4) is trapezoid boss shape, its inclined-plane and horizontal plane
Angle be 15 degree, the surrounding of the top cover (4) be additionally provided with it is multiple connect several ventilating openings (41) with umbilical tower inside,
Described each ventilating opening (41) place is provided with separation net, and lightning rod and wind speed detector are additionally provided with the outside of the top cover.
2. rocket launching umbilical tower according to claim 1, it is characterised in that：The umbilical tower (1) uses Q345 types
Steel plate is made, and the steel plate thickness is not less than 10mm.
3. rocket launching umbilical tower according to claim 2, it is characterised in that：By interior method between described each tower section
Blue double bolt is attached, and rigid protective set is provided with the outside of the bolt.
4. rocket launching umbilical tower according to claim 3, it is characterised in that：Set in umbilical tower (1) base
There are multiple illuminating lamps, umbilical tower (1) base is provided with access door, is provided with the access door away from the one side of rocket
Light switch for controlling umbilical tower (1) intraoral illumination lamp.
5. rocket launching umbilical tower according to claim 4, it is characterised in that：The umbilical tower (1) is if interior be provided with
Dry emergency light.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410339987.XA CN104142092B (en) | 2014-07-17 | 2014-07-17 | Rocket launching umbilical tower |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410339987.XA CN104142092B (en) | 2014-07-17 | 2014-07-17 | Rocket launching umbilical tower |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104142092A CN104142092A (en) | 2014-11-12 |
| CN104142092B true CN104142092B (en) | 2017-06-16 |
Family
ID=51851349
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410339987.XA Active CN104142092B (en) | 2014-07-17 | 2014-07-17 | Rocket launching umbilical tower |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104142092B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106288953B (en) * | 2016-11-07 | 2017-10-03 | 北京航天发射技术研究所 | A kind of light thermal-insulation ventilation unit for carrier rocket flat pad |
| CN106972473A (en) * | 2017-05-25 | 2017-07-21 | 北京航天发射技术研究所 | A kind of lightening arresting method of rocket movable launch platform |
| US10974853B1 (en) | 2018-11-13 | 2021-04-13 | United Launch Alliance, L.L.C. | White room modular system for launch vehicles |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4932607A (en) * | 1988-08-19 | 1990-06-12 | Martin Marietta Corporation | Universal erection and processing system for launching a space vehicle |
| CN100570108C (en) * | 2005-04-21 | 2009-12-16 | 结构混凝土&钢公司 | Prefabricated modular tower |
| CN202431452U (en) * | 2011-12-12 | 2012-09-12 | 广东明阳风电产业集团有限公司 | Tower structure used for supporting fan |
| CN103542770A (en) * | 2012-07-10 | 2014-01-29 | 北京航天发射技术研究所 | Large launch platform with built-in water channel for protection and manufacturing method thereof |
| CN103712522A (en) * | 2012-09-29 | 2014-04-09 | 北京航天发射技术研究所 | Rocket launching system with water spraying, cooling and denoising functions |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8209913B2 (en) * | 2011-02-01 | 2012-07-03 | Mitsubishi Heavy Industries, Ltd. | Tubular structure and wind turbine generator |
-
2014
- 2014-07-17 CN CN201410339987.XA patent/CN104142092B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4932607A (en) * | 1988-08-19 | 1990-06-12 | Martin Marietta Corporation | Universal erection and processing system for launching a space vehicle |
| CN100570108C (en) * | 2005-04-21 | 2009-12-16 | 结构混凝土&钢公司 | Prefabricated modular tower |
| CN202431452U (en) * | 2011-12-12 | 2012-09-12 | 广东明阳风电产业集团有限公司 | Tower structure used for supporting fan |
| CN103542770A (en) * | 2012-07-10 | 2014-01-29 | 北京航天发射技术研究所 | Large launch platform with built-in water channel for protection and manufacturing method thereof |
| CN103712522A (en) * | 2012-09-29 | 2014-04-09 | 北京航天发射技术研究所 | Rocket launching system with water spraying, cooling and denoising functions |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104142092A (en) | 2014-11-12 |
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