CN109185608A - A kind of onboard satellite communication equipment shock-proof machine frame - Google Patents
A kind of onboard satellite communication equipment shock-proof machine frame Download PDFInfo
- Publication number
- CN109185608A CN109185608A CN201811270532.1A CN201811270532A CN109185608A CN 109185608 A CN109185608 A CN 109185608A CN 201811270532 A CN201811270532 A CN 201811270532A CN 109185608 A CN109185608 A CN 109185608A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- satellite communication
- fixed
- fixture block
- communication equipment
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M5/00—Engine beds, i.e. means for supporting engines or machines on foundations
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention discloses a kind of onboard satellite communication equipment shock-proof machine frames, including mounting seat, communication agent and crisscross fixer plate, support frame is fixedly connected at the top of mounting seat, installing frame is fixedly connected with by link block between the opposite side of four support frames, the bottom of communication agent is fixedly connected with the first threaded rod, the bottom thread of the first screw thread rod outer surface is connected with thread barrel, the bottom thread of the screw thread tube inner surface is connected with the second threaded rod, and second the bottom end of threaded rod be fixedly connected with fixed block, the bottom of the fixed block is fixedly connected with waning moon fixture block, the present invention relates to satellite communication technical field of auxiliary equipment.The onboard satellite communication equipment shock-proof machine frame, it is coupled the setting of pedestal, support frame, installing frame, waning moon fixture block, buckle ring and crisscross fixer plate, allow device to buffer the vibration from fuselage while fixed, reduces the shaking degree of equipment, save space.
Description
Technical field
The present invention relates to satellite communication technical field of auxiliary equipment, specially a kind of onboard satellite communication equipment damping machine
Frame.
Background technique
Satellite communication is exactly to forward radio wave as relay station using artificial earth satellite, to realize two or more
Communication between a earth station, artificial earth satellite according to radio signal amplify the presence or absence of, forwarding capability, it is active artificial
Point of earth satellite and passive artificial earth satellite.Since the signal that passive artificial earth satellite reflects is too weak without practical valence
Value, then people are dedicated to active artificial earth satellite-telecommunication satellite of the research with amplification, frequency conversion forwarding capability to realize
Satellite communication, wherein there is superior function, benefit around the period of the terrestrial equator operation synchronous satellite equal with earth rotation period
Main satellite communication being had become with the communication of synchronous satellite, satellite communication there are various features, wherein communication distance is remote,
And expense is unrelated with communication distance；Broadcast mode work, can carry out multiple access communication, in general, other kinds of means of communication is only
It is able to achieve point-to-point communication, and satellite is worked with broadcast mode, in the whole region of satellite antenna wave cover
Any point earth station can be set, these earth stations can share a telecommunication satellite to realize bilateral or multilateral communication,
Carry out multiple access communication；Message capacity is big, is applicable in multiple business transmission；It can be monitored with internal loopback；Seamless coverage ability；
Wide area complex network topologies constitute ability；Security reliability.
The last one information island of Internet service --- aircraft passenger compartment is gradually solved by Airborne Satellite Communication System,
So that the feeler of internet climbs up meters altitude, air passengers gradually get rid of finally flight it is very long on the way, uninteresting and and generation every
The exhausted days of hardship start the journey a good life for experiencing cloud amusement, shopping and Always Online".
Since aircraft can generate vibration during flight, satellite communication equipment is caused to shake, influences the propagation of signal,
So needing to carry out damping to satellite communication equipment, existing shock-absorption device is exactly to install a spring pedestal, and such setting exists
The degree that aircraft shakes during running is larger, needs biggish space to be disposed, occupies more space in this way, unfavorable
It arranges in the entirety of aircraft space.
Summary of the invention
In view of the deficiencies of the prior art, it the present invention provides a kind of onboard satellite communication equipment shock-proof machine frame, solves existing
Some onboard satellite communication equipment shock-absorption devices degree for shaking during aircraft is run is larger, need biggish space into
Row placement, occupies more space in this way, is unfavorable for the problem of aircraft space is integrally arranged.
In order to achieve the above object, the present invention is achieved by the following technical programs: a kind of onboard satellite communication equipment subtracts
Rack, including mounting seat, communication agent and crisscross fixer plate are shaken, is fixedly connected with support at the top of the mounting seat
Frame, and installing frame is fixedly connected with by link block between the opposite side of four support frames, the bottom of the communication agent is solid
Surely it is connected with the first threaded rod, the bottom thread of the first screw thread rod outer surface is connected with thread barrel, table in the thread barrel
The bottom thread in face is connected with the second threaded rod, and the bottom end of the second threaded rod is fixedly connected with fixed block, the fixed block
Bottom is fixedly connected with waning moon fixture block, and the bottom of the installing frame is rotatably connected to buckle ring by link block, and buckle ring
The curved surfaces of inner surface and waning moon fixture block are clamped, and the surface of the crisscross fixer plate and the bottom end of waning moon fixture block offer
First threaded hole, and be fixedly connected between the inner surface of two the first threaded holes by screw.
Preferably, the first groove is offered at the top of the installing frame, the inner surface of first groove slidably connects
Limit plate, the bottom of the limit plate are fixedly connected with elastic telescopicing rod, and the bottom end of the elastic telescopicing rod mandril is fixedly connected
There is snap-gauge, and the outer surface of elastic telescopicing rod is arranged with spring, the second groove is offered at the top of the fixed block, and second is recessed
The inner surface of slot and the outer surface of snap-gauge are slidably connected.
Preferably, the front and rear sides of the installing frame and the two sides of limit plate offer the second threaded hole, and two
It is fixedly connected between the inner surface of two threaded holes by screw.
Preferably, the inner surface of the installing frame is fixedly connected with elastic cushion, and the inner surface of elastic cushion and fixed block
Outer surface is flexibly connected.
Preferably, the outer surface of the thread barrel is arranged with fixed fixture block, and the fixed fixture block includes fixed frame, buffer layer
And resistant layer, the inner surface of the fixed frame are fixedly connected with buffer layer, the inner surface of the buffer layer is fixedly connected with resistance
Layer, and the outer surface of the inner surface of resistant layer and thread barrel is clamped.
Preferably, the bottom of the mounting seat is fixedly connected with elastic-friction pad, and the two sides of mounting seat and elasticity
The two sides of friction pad offer mounting hole.
Beneficial effect
The present invention provides a kind of onboard satellite communication equipment shock-proof machine frames.Have compared with prior art following beneficial
Effect:
(1), the onboard satellite communication equipment shock-proof machine frame, by being fixedly connected with support frame at the top of mounting seat,
And installing frame is fixedly connected with by link block between the opposite side of four support frames, the bottom of communication agent is fixedly connected with
First threaded rod, the bottom thread of the first screw thread rod outer surface are connected with thread barrel, the bottom thread connection of screw thread tube inner surface
There is the second threaded rod, the bottom end of the second threaded rod is fixedly connected with fixed block, and the bottom of fixed block is fixedly connected with waning moon fixture block,
The bottom of installing frame is rotatably connected to buckle ring, the inner surface of buckle ring and the curved surfaces card of waning moon fixture block by link block
It connects, the surface of crisscross fixer plate and the bottom end of waning moon fixture block offer the first threaded hole, and two the first threaded holes is interior
It is fixedly connected between surface by screw, is coupled pedestal, support frame, installing frame, waning moon fixture block, buckle ring and cross and fixes
The setting of frame plate allows device to buffer the vibration from fuselage while fixed, reduces the shaking degree of equipment, saves
Saved space, solve existing onboard satellite communication equipment shock-absorption device during aircraft operation the degree shaken compared with
Greatly, it needs biggish space to be disposed, occupies more space in this way, be unfavorable for the problem of aircraft space is integrally arranged.
(2), the onboard satellite communication equipment shock-proof machine frame, by offering the first groove at the top of installing frame, first
The inner surface of groove slidably connects limit plate, and the bottom of limit plate is fixedly connected with elastic telescopicing rod, elastic telescopicing rod mandril
Bottom end be fixedly connected with snap-gauge, the outer surface of elastic telescopicing rod is arranged with spring, the second groove is offered at the top of fixed block,
The inner surface of second groove and the outer surface of snap-gauge are slidably connected, and cooperate the first groove, limit plate, elastic telescopicing rod, snap-gauge, bullet
The setting of spring and the second groove can buffer impact force of the equipment in upward vibration, reduce the shaking degree of equipment once again, make
It obtains equipment and keeps a stable state.
(3), the onboard satellite communication equipment shock-proof machine frame, is arranged with fixed fixture block by the outer surface in thread barrel, Gu
Determining fixture block includes fixed frame, buffer layer and resistant layer, and the inner surface of fixed frame is fixedly connected with buffer layer, the inner surface of buffer layer
It is fixedly connected with resistant layer, and the outer surface of the inner surface of resistant layer and thread barrel is clamped, cooperation fixed frame, buffer layer and resistance
The setting of layer can carry out clamping to thread barrel, avoid because equipment concussion makes thread barrel and the first threaded rod and the second spiral shell
The case where connection between rasp bar is loosened, is acutely shaken so as to cause equipment.
Detailed description of the invention
Fig. 1 is external structure schematic diagram of the invention；
Fig. 2 is the top view of structure of the invention；
Fig. 3 is the bottom view of structure of the invention；
Fig. 4 is the structural schematic diagram of waning moon fixture block of the present invention；
Fig. 5 is the structural schematic diagram of the fixed fixture block of the present invention；
Fig. 6 is the structural schematic diagram of limit plate of the present invention.
In figure: 1-mounting seat, 2-communication agents, 3-crisscross fixer plates, 4-support frames, 5-installing frames, 6-
First threaded rod, 7-thread barrels, the 8-the second threaded rod, 9-fixed blocks, 10-waning moon fixture blocks, 11-buckle rings, 12-the first
Threaded hole, the 13-the first groove, 14-limit plates, 15-elastic telescopicing rods, 16-snap-gauges, 17-springs, the 18-the second groove,
19-the second threaded hole, 20-elastic cushions, 21-fixed fixture blocks, 22-fixed frames, 23-buffer layers, 24-resistant layers, 25-
Elastic-friction pad, 26-mounting holes.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-6 is please referred to, the present invention provides a kind of technical solution: a kind of onboard satellite communication equipment shock-proof machine frame, including
Mounting seat 1, communication agent 2 and crisscross fixer plate 3, crisscross fixer plate 3 position to fixed block 9, cooperate simultaneously
The setting of buckle ring 11 can carry out certain vibration buffering to fixed block 9, and the top of mounting seat 1 is fixedly connected with support
Frame 4, and installing frame 5 is fixedly connected with by link block between the opposite side of four support frames 4, the bottom of communication agent 2 is solid
Surely it is connected with the first threaded rod 6, the bottom thread of 6 outer surface of the first threaded rod is connected with thread barrel 7, and the surface of thread barrel 7 is opened
Equipped with frictional groove, the bottom thread of 7 inner surface of thread barrel is connected with the second threaded rod 8, the first threaded rod 6, thread barrel 7 and second
The quantity of threaded rod 8 is both provided with four, cooperates the setting of the first threaded rod 6, thread barrel 7 and the second threaded rod 8, can pass through
Thread barrel 7 is rotated to adjust the distance between communication agent 2 and fixed block 9, and the bottom end of the second threaded rod 8 is fixedly connected with
Determine block 9, the bottom of fixed block 9 is fixedly connected with waning moon fixture block 10, and the height of waning moon fixture block 10 is different, wherein apart from each other one
Height at a distance of closer a pair of of waning moon fixture block 10 is lower than to the height of waning moon fixture block 10, while buckle ring 11 has adjusted accordingly
Highly, it ensure that balance of the device when installing crisscross fixer plate 3, the bottom of installing frame 5 is rotatablely connected by link block
There is buckle ring 11, buckle ring 11 and waning moon fixture block 10 are both provided with four, ensure that the uniform stressed of fixed block 9, increase device
Stability, and the curved surfaces of the inner surface of buckle ring 11 and waning moon fixture block 10 are clamped, the surface of crisscross fixer plate 3 and residual
The bottom end of month fixture block 10 offers the first threaded hole 12, and is fixed between the inner surface of two the first threaded holes 12 by screw
Connection, is coupled the setting of pedestal 1, support frame 4, installing frame 5, waning moon fixture block 10, buckle ring 11 and crisscross fixer plate 3,
Allow device to buffer the vibration from fuselage while fixed, reduce the shaking degree of equipment, save space, solves
The degree that existing onboard satellite communication equipment shock-absorption device shakes during aircraft operation of having determined is larger, needs biggish
Space is disposed, and occupies more space in this way, is unfavorable for the problem of aircraft space is integrally arranged, and the top of installing frame 5 is opened
Equipped with the first groove 13, the inner surface of the first groove 13 slidably connects limit plate 14, and the bottom of limit plate 14 is fixedly connected with
Elastic telescopicing rod 15, the bottom end of 15 mandril of elastic telescopicing rod are fixedly connected with snap-gauge 16, and the appearance surface cover of elastic telescopicing rod 15
Equipped with spring 17, the top of fixed block 9 offers the second groove 18, and the outer surface of the inner surface of the second groove 18 and snap-gauge 16
It is slidably connected, snap-gauge 16 and the second groove 18 are slidably connected and can carry out lateral limit to fixed block 9, increase the steady of device
Qualitative energy, cooperates the setting of the first groove 13, limit plate 14, elastic telescopicing rod 15, snap-gauge 16, spring 17 and the second groove 18,
Impact force of the equipment in upward vibration can be buffered, reduces the shaking degree of equipment once again, so that equipment keeps a stabilization
State, the front and rear sides of installing frame 5 and the two sides of limit plate 14 offer the second threaded hole 19, and two the second threaded holes
It being fixedly connected between 19 inner surface by screw, the inner surface of installing frame 5 is fixedly connected with elastic cushion 20, and elastic cushion 20
Inner surface is flexibly connected with the outer surface of fixed block 9, and elastic cushion 20 can be buffered when fixed block 9 shakes, and avoids fixing
The case where colliding between block 9 and installing frame 5, lead to equipment damage, the outer surface of thread barrel 7 are arranged with fixed fixture block 21,
Fixed fixture block 21 includes fixed frame 22, buffer layer 23 and resistant layer 24, and the inner surface of fixed frame 22 is fixedly connected with buffer layer 23,
Buffer layer 23 is manufactured by elastic material, can buffer a degree of shaking force when fixed 21 fixed thread cylinder 7 of fixture block,
So that fixed fixture block 21 is attached to 7 surface of thread barrel always, guarantees the positioning action of fixed fixture block 21, the interior table of buffer layer 23
Face is fixedly connected with resistant layer 24, and resistant layer 24 has the biggish substance manufacture of frictional force, can be by fixed fixture block 21 consolidating tightly
It is scheduled on the surface of thread barrel 7, is avoided because vibration causes to fix the case where fixture block 21 is fallen, and the inner surface and spiral shell of resistant layer 24
The outer surface of line cylinder 7 is clamped, and is cooperated the setting of fixed frame 22, buffer layer 23 and resistant layer 24, can be blocked to thread barrel 7
Tightly, avoiding loosens the connection between thread barrel 7 and the first threaded rod 6 and the second threaded rod 8 because equipment is shaken, from
And the case where causing equipment acutely to be shaken, the bottom of mounting seat 1 are fixedly connected with elastic-friction pad 25, elastic-friction pad 25 increases
Big frictional force between mounting seat 1 and fuselage, avoiding because device shakes leads to the situation of screw connection appearance activity,
And the two sides of mounting seat 1 and the two sides of elastic-friction pad 25 offer mounting hole 26.
When work, mounting hole 26 is passed through using screw, mounting seat 1 is fixed on fuselage, fixed block 9 is put into installation
In frame 5,11 sets of buckle ring are rotated on waning moon fixture block 10, screw is reused by crisscross fixer plate 3 and is fixed on waning moon fixture block 10
On, thread barrel 7 is rotated, increases the distance between communication agent 2 and fixed block 9, limit plate 14 is then filled in into the first groove 13
In, limit plate 14 is firmly pressed, screw is reused across the second threaded hole 19, limit plate 14 and installing frame 5 is fixed, turned again
Dynamic thread barrel 7 makes communication agent 2 reach the height of adaptation, then fixed fixture block 21 is stuck in 7 surface of thread barrel, when device shakes,
Fixed block 9 can squeeze elastic cushion 21 and snap-gauge 16, and snap-gauge 16 squeezes elastic telescopicing rod 15 and spring 17, carry out damping.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of onboard satellite communication equipment shock-proof machine frame, including mounting seat (1), communication agent (2) and crisscross fixer plate
(3), it is characterised in that: be fixedly connected with support frame (4) at the top of the mounting seat (1), and four support frames (4) are opposite
It is fixedly connected with installing frame (5) between side by link block, the bottom of the communication agent (2) is fixedly connected with the first screw thread
The bottom thread of bar (6), the first threaded rod (6) outer surface is connected with thread barrel (7), thread barrel (7) inner surface
Bottom thread is connected with the second threaded rod (8), and the bottom end of the second threaded rod (8) is fixedly connected with fixed block (9), the fixation
The bottom of block (9) is fixedly connected with waning moon fixture block (10), and the bottom of the installing frame (5) is rotatably connected to fastening by link block
Ring (11), and the inner surface of buckle ring (11) and the curved surfaces of waning moon fixture block (10) are clamped, the crisscross fixer plate (3)
Surface and the bottom end of waning moon fixture block (10) offer the first threaded hole (12), and the inner surface of two the first threaded holes (12) it
Between be fixedly connected by screw.
2. a kind of onboard satellite communication equipment shock-proof machine frame according to claim 1, it is characterised in that: the installing frame
(5) it is offered at the top of the first groove (13), the inner surface of first groove (13) slidably connects limit plate (14), described
The bottom of limit plate (14) is fixedly connected with elastic telescopicing rod (15), and the bottom end of elastic telescopicing rod (15) mandril is fixedly connected
Have snap-gauge (16), and the outer surface of elastic telescopicing rod (15) is arranged with spring (17), is offered at the top of the fixed block (9)
Two grooves (18), and the inner surface of the second groove (18) and the outer surface of snap-gauge (16) are slidably connected.
3. a kind of onboard satellite communication equipment shock-proof machine frame according to claim 2, it is characterised in that: the installing frame
(5) two sides of front and rear sides and limit plate (14) offer the second threaded hole (19), and two the second threaded holes (19)
It is fixedly connected between inner surface by screw.
4. a kind of onboard satellite communication equipment shock-proof machine frame according to claim 1, it is characterised in that: the installing frame
(5) inner surface is fixedly connected with elastic cushion (20), and the outer surface activity of the inner surface of elastic cushion (20) and fixed block (9) connects
It connects.
5. a kind of onboard satellite communication equipment shock-proof machine frame according to claim 1, it is characterised in that: the thread barrel
(7) outer surface is arranged with fixed fixture block (21), and the fixed fixture block (21) includes fixed frame (22), buffer layer (23) and resistance
Layer (24), the inner surface of the fixed frame (22) are fixedly connected with buffer layer (23), and the inner surface of the buffer layer (23) is fixed
It is connected with resistant layer (24), and the outer surface of the inner surface of resistant layer (24) and thread barrel (7) is clamped.
6. a kind of onboard satellite communication equipment shock-proof machine frame according to claim 1, it is characterised in that: the mounting seat
(1) bottom is fixedly connected with elastic-friction pad (25), and the two sides of mounting seat (1) and the two sides of elastic-friction pad (25) are equal
Offer mounting hole (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811270532.1A CN109185608B (en) | 2018-10-29 | 2018-10-29 | Shock absorption rack of airborne satellite communication equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811270532.1A CN109185608B (en) | 2018-10-29 | 2018-10-29 | Shock absorption rack of airborne satellite communication equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109185608A true CN109185608A (en) | 2019-01-11 |
| CN109185608B CN109185608B (en) | 2020-08-04 |
Family
ID=64944351
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811270532.1A Active CN109185608B (en) | 2018-10-29 | 2018-10-29 | Shock absorption rack of airborne satellite communication equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109185608B (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004133244A (en) * | 2002-10-11 | 2004-04-30 | Murata Mach Ltd | Image forming apparatus |
| CN204119703U (en) * | 2014-08-27 | 2015-01-21 | 南京中网卫星通信股份有限公司 | A kind of onboard satellite communication equipment shock-proof machine frame |
| CN206786279U (en) * | 2017-06-09 | 2017-12-22 | 庄仁山 | A kind of liftable projecting apparatus rack |
| CN206967852U (en) * | 2017-07-04 | 2018-02-06 | 衢州信辉塑料配件有限公司 | A kind of injection machine of convenient regulation |
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| CN207946979U (en) * | 2018-03-06 | 2018-10-09 | 姚思盈 | A kind of building comprehensive practical traning model equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109185608B (en) | 2020-08-04 |
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Application publication date: 20190111 Assignee: Ruian baileya Crafts Co.,Ltd. Assignor: Zhejiang gaochuangmeng Intellectual Property Consulting Co.,Ltd. Contract record no.: X2022330000813 Denomination of invention: A damping rack for airborne satellite communication equipment Granted publication date: 20200804 License type: Common License Record date: 20221221 |