CN108768499A - A kind of civil aviation satellite communication system and its application method - Google Patents
A kind of civil aviation satellite communication system and its application method Download PDFInfo
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- CN108768499A CN108768499A CN201810493508.8A CN201810493508A CN108768499A CN 108768499 A CN108768499 A CN 108768499A CN 201810493508 A CN201810493508 A CN 201810493508A CN 108768499 A CN108768499 A CN 108768499A
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- face
- sliding block
- screw rod
- sliding
- cone pulley
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18515—Transmission equipment in satellites or space-based relays
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18517—Transmission equipment in earth stations
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention discloses a kind of civil aviation satellite communication systems,Including outer housing and satellite communication body,Holding tank is equipped in the outer housing front end face,Guide runner is equipped in the receiving groove bottom wall,The first extended up and down cunning chamber is equipped in the outer housing on rear side of the holding tank,First cunning bottom of chamber wall extended segment is located at the rear side relative position of the guide runner,The first cunning intracavitary is slidably connected with the first sliding block,First slider top end face screw-internal thread fit is connected with the adjusting screw rod for upwardly extending setting,Extending end is connected with the first motor power being embedded in admittedly in the first cunning chamber roof at the top of the adjusting screw rod,It is installed with tooth-strip part in the first sliding block front end face,The first deep gouge is equipped in the front end face end face of first sliding block on the downside of the tooth-strip part,It is installed with the second motor in the first deep gouge roof.
Description
Technical field
The present invention relates to air equipment technical field, specially a kind of civil aviation satellite communication system and its user
Method.
Background technology
The structure type of modular chassis is usually used in satellite communication equipment in aviation field, and satellite communication equipment makes
It could be used with being required for inserting a plug into Power Block after energization, however the Power Block of existing satellite communication equipment is basic
It is all mounted in body, plug is connect by bolt with the direct lock fit of Power Block, complex for operation step, is unfavorable for tearing open
Dress and safeguard, easily cause connection loosen so that can not to electric satellite communication equipment normal power supply work, and loosen while
The danger for easily causing electric shock has that safety is not high, and to operating personnel, there are larger security risks.
Invention content
It is existing for overcoming the purpose of the present invention is to provide a kind of civil aviation satellite communication system and its application method
Drawbacks described above in technology.
A kind of civil aviation satellite communication system according to the present invention, including outer housing and satellite communication body, it is described
It is equipped with holding tank in outer housing front end face, guide runner is equipped in the receiving groove bottom wall, it is described outer on rear side of the holding tank
The first extended up and down cunning chamber is equipped in shell, first cunning bottom of chamber wall extended segment is located at the rear side phase of the guide runner
To position, the first cunning intracavitary is slidably connected with the first sliding block, and first slider top end face screw-internal thread fit connects
Be connected to the adjusting screw rod for upwardly extending setting, at the top of the adjusting screw rod extending end be embedded in described first admittedly and slide in chamber roof
First motor power be connected, be installed with tooth-strip part in the first sliding block front end face, be located on the downside of the tooth-strip part
First sliding block front end face end face in be equipped with the first deep gouge, be installed with the second motor in the first deep gouge roof,
Second motor bottom end be connected by power has the first cone pulley stretched into first deep gouge, described first slide chamber with it is described
It is rotatably assorted in part between guide runner and is connected with the first screw rod part, end, which is installed with, on rear side of the first screw rod part stretches into institute
It states in the first deep gouge and the second cone pulley to be connected with the first cone pulley power, the first screw rod part front side extends
End is stretched into the guide runner and is rotatably assorted with the front side wall of the guide runner and connect, the company of being slidably matched in the guide runner
It is connected to the slider guide being connect with the first screw rod part screw-thread fit, the satellite communication body includes that bottom end face is led with described
The interconnecting piece of slider top end secure fit connection and the main body being installed in the interconnecting piece front end face, described the
It is equipped with second in part between one cunning chamber and the holding tank and slides chamber, is connected in the second cunning chamber roof and is equipped with to front side
Extended the first sliding groove, extending end is connected setting with the holding tank on front side of the first sliding groove, first cunning
Chamber and it is described second cunning chamber between part in equipped with rear side end with it is described first slide chamber front side end be connected setting second sink
Slot is rotatably assorted in second deep gouge and is connected with driving gear, third cone pulley is installed in the driving gear front end face,
It is rotatably assorted in part between second deep gouge and the second cunning chamber and is connected with front and back the second extended screw rod part,
End is installed with to stretch into and be connected in second deep gouge and with the third cone pulley power on rear side of the second screw rod part
4th cone pulley, the second screw rod part front side extending end, which stretches into described second and slides intracavitary and slide chamber front side wall with described second, to be turned
Dynamic to be connected, described second, which slides intracavitary, is equipped with top-pushing mechanism, is set by power supply slot in the holding tank roof, the slider guide
The touch sensor to be oppositely arranged with the left and right sides inner wall of the guide runner, institute are respectively equipped in the end face of the left and right sides
It states touch sensor to be electrically connected with second motor, when the slider guide or so end face touches the left and right sides respectively
When the touch sensor, at this point, sending signal by the touch sensor and controlling second motor stalls.
Further technical solution, on rear side of the driving gear maximum circumscribed circle stretch into described first slide intracavitary and with it is described
Tooth-strip part power is connected.
Further technical solution, the top-pushing mechanism include sliding connection setting it is described second slide intracavitary and with
Second sliding block of the second screw rod part screw-thread fit connection and sliding connection be arranged in the first sliding groove and with
The propulsion arm of the second sliding block secure fit connection, the propulsion arm front side end are installed with sloped roof briquetting.
Further technical solution is installed with flexible power supply block in the power supply groove top wall.
Further technical solution, the interconnecting piece back end surface is interior to be equipped with second sliding slot, interconnecting piece roof end face
It is interior to be equipped with the third sliding slot for extending downwardly setting, it is connected equipped with guide groove in the third sliding slot front side wall, the third is slided
It is slidably connected with lock slide in slot, conductive trough is equipped in the lock slide top end surface, the lock slide bottom end is solid
Equipped with inclined-plane sliding block, the guide runner being connect with the lock slide secure fit is slidably connected in the guide groove,
Top pressure is connected with top pressure spring in the guide groove on the upside of the guide runner.
Further technical solution, third sliding slot rear side end are oppositely arranged with the first sliding groove front side end.
Description of the drawings
Fig. 1 is a kind of civil aviation satellite communication system outside overall structure diagram in the present invention；
Fig. 2 is a kind of civil aviation satellite communication system internal structure schematic diagram in the present invention.
Specific implementation mode
With reference to Fig. 1-2, the present invention is described in detail.
Referring to Fig.1-2, a kind of civil aviation satellite communication system according to an embodiment of the invention, including outer housing 6 with
And satellite communication body 7,6 front end face of the outer housing is interior to be equipped with holding tank 61, and slide guide is equipped in 61 bottom wall of the holding tank
Slot 64, the outer housing 6 of 61 rear side of the holding tank is interior to be equipped with the first extended up and down cunning chamber 62, and described first slides chamber
62 bottom wall extended segments are located at the rear side relative position of the guide runner 64, and first is slidably connected in the first cunning chamber 62
Sliding block 621, first sliding block, 621 top end surface screw-internal thread fit is connected with the adjusting screw rod 624 for upwardly extending setting, described
624 top extending end of adjusting screw rod is connected with 625 power of first motor being embedded in admittedly in the first cunning 62 roof of chamber,
It is installed with tooth-strip part 623 in first sliding block, 621 front end face, is located at first sliding block of 623 downside of the tooth-strip part
It is equipped with the first deep gouge 622 in 621 front end face end face, the second motor 626, institute are installed in 622 roof of the first deep gouge
Stating 626 bottom end be connected by power of the second motor has the first cone pulley 627 stretched into first deep gouge 622, and described first slides
It is rotatably assorted in part between chamber 62 and the guide runner 64 and is connected with the first screw rod part 642, after the first screw rod part 642
Side end is installed with the second cone stretched into first deep gouge 622 and to be connected with 627 power of the first cone pulley
Wheel 628, the 642 front side extending end of the first screw rod part stretch into the guide runner 64 and with the front side wall of the guide runner 64
Be rotatably assorted connection, is slidably connected in the guide runner 64 and is led with what 642 screw-thread fit of the first screw rod part was connect
Sliding block 641, the satellite communication body 7 include the company that bottom end face is connect with 641 top end secure fit of the slider guide
Socket part 71 and the main body 72 being installed in 71 front end face of the interconnecting piece, described first slides chamber 62 and the holding tank 61
Between part in be equipped with second slide chamber 65, it is described second cunning 65 roof of chamber in be connected equipped with to front side be extended first
Sliding slot 66,66 front side extending end of the first sliding groove are connected setting with the holding tank 61, and described first slides chamber 62 and institute
It states to be equipped with rear side end in the part between the second cunning chamber 65 and slide 62 front side end of chamber with described first and be connected the second deep gouge of setting
63, it is rotatably assorted in second deep gouge 63 and is connected with driving gear 631, be installed in 631 front end face of driving gear
Third cone pulley 633 is rotatably assorted and is connected with front and back extension in the part between second deep gouge 63 and the second cunning chamber 65
The second screw rod part 651 being arranged, the 651 rear side end of the second screw rod part be installed with stretch into second deep gouge 63 and with institute
The 4th cone pulley 632 of 633 power of third cone pulley mating connection is stated, the 651 front side extending end of the second screw rod part stretches into described
It is rotatably assorted in second cunning chamber 65 and with the second cunning 65 front side wall of chamber and connect, pusher is equipped in the second cunning chamber 65
Structure is set in 61 roof of the holding tank by power supply slot 67, be respectively equipped in the left and right sides end face of the slider guide 641 to
The touch sensor 6410 that the left and right sides inner wall of the guide runner 64 is oppositely arranged, the touch sensor 6410 and institute
The electric connection of the second motor 626 is stated, when the contact that 641 or so end face of the slider guide touches the left and right sides respectively passes
When sensor 6410, stop operating at this point, being sent signal by the touch sensor 6410 and being controlled second motor 626.
Valuably or illustratively, the maximum circumscribed circle of the rear side of the driving gear 631 stretch into described first slide in chamber 62 and
It is connected with 623 power of the tooth-strip part, to realize the rotation work for automatically controlling driving gear 63 by tooth-strip part 623.
Valuably or illustratively, the top-pushing mechanism include sliding connection setting it is described second slide chamber 65 in and
The second sliding block 652 and sliding connection setting being connect with 651 screw-thread fit of the second screw rod part are slided described first
The propulsion arm 661 connecting in slot 66 and with 652 secure fit of the second sliding block, 661 front side end of the propulsion arm are installed with
Sloped roof briquetting 662 automatically controls the drive connection work of propulsion arm 661 and interconnecting piece 71 to realize.
Valuably or illustratively, it is installed with flexible power supply block 671 in 67 roof of power supply slot, to improve
For the stability of electrical connection.
Valuably or illustratively, second sliding slot 710 is equipped in 71 back end surface of the interconnecting piece, the interconnecting piece 71 pushes up
It is equipped with the third sliding slot 711 for extending downwardly setting in wall end face, is connected equipped with guide groove in 711 front side wall of third sliding slot
712, it is slidably connected with lock slide 713 in the third sliding slot 711, conduction is equipped in 713 top end surface of the lock slide
Slot 715,713 bottom end of the lock slide are installed with inclined-plane sliding block 714, are slidably connected in the guide groove 712
The guide runner 716 being connect with 713 secure fit of the lock slide, in the guide groove 712 of the upside of the guide runner 716
Top pressure is connected with top pressure spring 717, to realize the execution work for being electrically connected and locking.
Valuably or illustratively, 711 rear side end of the third sliding slot is opposite with 66 front side end of the first sliding groove
Setting.
When original state, slider guide 641 is located at the most forward position in guide runner 64, connects at this point, being driven by slider guide 641
Socket part 71 is utmostly located at the forward position in holding tank 61, meanwhile, drive main body 72 utmostly to stretch by interconnecting piece 71
Go out outside the front end face of outer housing 6, at this point, pressure on top surface of the guide runner 716 by top pressure spring 717, makes guide runner 716
Lowest position in guide groove 712, meanwhile, drive 713 end face of lock slide to be located at third sliding slot 711 by guide runner 716
It is interior, at this point, drive the inclined-plane sliding block 714 of bottom utmostly to stretch into second sliding slot 710 by lock slide 713, meanwhile, first slides
Block 621 is located at the lowest position in the first cunning chamber 62, at this point, making the first cone pulley 627 and the second cone pulley in the first deep gouge 622
628 power are connected, meanwhile, the second sliding block 652 is located at the last side position in the second cunning chamber 65, at this point, by the second sliding block
652 drive propulsion arms 661 and the sloped roof briquetting 662 of 661 front side end of propulsion arm are fully located in the first sliding groove 66.
It rotates in use, controlling the first cone pulley 627 by the second motor 626 when needing to power, is driven by the first cone pulley 627
Second cone pulley 628 and the rotation of the first screw rod part 642, and then drive slider guide 641 gradually towards guide runner by the first screw rod part 642
Rear direction sliding in 64, meanwhile, drive satellite communication body 7 gradually to stretch into holding tank 61 by slider guide 641, until leading
Sliding block 641 slides into the last side position in guide runner 64, at this point, driving satellite communication body 7 to be fully inserted by slider guide 641
In holding tank 61, meanwhile, so that 711 top end of third sliding slot is in relative position with power supply 67 bottom end of slot and then passes through
Controlling first motor 625 drives adjusting screw rod 624 to rotate, and drives the first sliding block 621 gradually to slide chamber towards first by adjusting screw rod 624
Top-direction sliding in 62, at this point, the first cone pulley 627 in the first deep gouge 622 is made to be detached from and be gradually distance from the second cone pulley
628, meanwhile, drive driving gear 631 and third cone pulley 633 to rotate by tooth-strip part 623, and then driven by third cone pulley 633
Second screw rod part 651 rotates, and drives the second sliding block 652 to slide the front side direction in chamber 65 towards second by the second screw rod part 651 and slide
It is dynamic, at this point, driving the sloped roof briquetting 662 on propulsion arm 661 and propulsion arm 661 gradually to stretch into second by the second sliding block 652
In sliding slot 710, and sloped roof briquetting 662 is made to slide cooperating with 714 top pressure of inclined-plane sliding block, and then realizes there is inclined-plane sliding
Block 714 drives lock slide 713 and the guide runner 716 being fixedly connected with lock slide 713 to overcome the pressure on top surface of top pressure spring 717
And gradually towards the top-direction sliding in guide groove 712, meanwhile, so that 713 top end of lock slide is gradually stretched into power supply slot 67,
Until when the top end surface of propulsion arm 661 and the bottom end face top pressure of inclined-plane sliding block 714 are slidably connected, at this point, inclined-plane
Sliding block 714 is fully inserted into third sliding slot 711, meanwhile, so that 713 top end of lock slide is utmostly stretched into power supply slot 67
It is interior, and then the power supply block 671 in power supply slot 67 is made utmostly to stretch into conductive trough 715.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, it is easy to operate, the first cone pulley is controlled by the second motor and is turned
It is dynamic, drive the second cone pulley and the first screw rod part to rotate by the first cone pulley, and then the gradual court of slider guide is driven by the first screw rod part
Rear direction sliding in guide runner, meanwhile, drive satellite communication body gradually to stretch into holding tank by slider guide, until slide guide
Block slides into the last side position in guide runner, at this point, driving satellite communication body to be fully inserted into holding tank by slider guide, together
When, so that third sliding slot top end is in relative position with power supply trench bottom end, then, tune is driven by controlling first motor
Section screw rod rotation, the top-direction for driving the first sliding block gradually to slide intracavitary towards first by adjusting screw rod is slided, at this point, making first to sink
The first cone pulley in slot is detached from and is gradually distance from the second cone pulley, meanwhile, drive driving gear and third cone pulley to turn by tooth-strip part
It is dynamic, and then the rotation of the second screw rod part is driven by third cone pulley, and drive the second sliding block to slide intracavitary towards second by the second screw rod part
Front side direction is slided, at this point, driving the sloped roof briquetting on propulsion arm and propulsion arm gradually to stretch into the second cunning by the second sliding block
In slot, and sloped roof briquetting is made to slide cooperating with inclined-plane sliding block top pressure, and then realizes have sliding block in inclined-plane that lock is driven to slide
Block and the guide runner being fixedly connected with lock slide overcome the pressure on top surface of top pressure spring and gradually towards the top sides in guide groove
To sliding, meanwhile, so that lock slide top end is gradually stretched into power supply slot, until the top end surface of propulsion arm and inclined-plane sliding block
The sliding connection of bottom end face top pressure when, at this point, inclined-plane sliding block is fully inserted into third sliding slot, meanwhile, make lock slide
Top end utmostly stretches into power supply slot, and then the power supply block in power supply slot is made utmostly to stretch into conductive trough, to real
Now automatically control locking and safety for be electrically connected work, reduce manual steps, substantially increase dismounting repair
Efficiency, meanwhile, improve the safety for electrical plug, in addition, by the power of the first cone pulley and the second cone pulley be detached from, prevent by
It causes to wear to external force factor, meanwhile, work is connect with the locking of power supply slot by lock slide, further increases the firm of locking
Property.
Those skilled in the art can define, can in the case of not departing from overall spirit and the design of the present invention
To make the various modifications for above example.It each falls within protection scope of the present invention.The protection scheme of the present invention
It is subject to claims appended hereto.
Claims (7)
1. a kind of civil aviation satellite communication system, including outer housing and satellite communication body, it is characterised in that：The shell
It is equipped with holding tank in body front end face, guide runner, the outer housing on rear side of the holding tank are equipped in the receiving groove bottom wall
Interior to be equipped with the first extended up and down cunning chamber, first cunning bottom of chamber wall extended segment is located at the rear side of the guide runner with respect to position
It sets, the first cunning intracavitary is slidably connected with the first sliding block, and first slider top end face screw-internal thread fit is connected with
Upwardly extend the adjusting screw rod of setting, at the top of the adjusting screw rod extending end be embedded in admittedly described first slide in chamber roof the
One motor power is connected, and tooth-strip part is installed in the first sliding block front end face, the institute being located on the downside of the tooth-strip part
It states and is equipped with the first deep gouge in the front end face end face of the first sliding block, the second motor is installed in the first deep gouge roof, it is described
Second motor bottom end be connected by power has the first cone pulley stretched into first deep gouge, and described first slides chamber and the slide guide
It is rotatably assorted in part between slot and is connected with the first screw rod part, end, which is installed with, on rear side of the first screw rod part stretches into described the
In one deep gouge and the second cone pulley to be connected with the first cone pulley power, the first screw rod part front side extending end
It stretches into the guide runner and is rotatably assorted with the front side wall of the guide runner and connect, be slidably connected in the guide runner
The slider guide being connect with the first screw rod part screw-thread fit, the satellite communication body include bottom end face and the slider guide
The interconnecting piece of top end secure fit connection and the main body being installed in the interconnecting piece front end face, described first slides
It is equipped with second in part between chamber and the holding tank and slides chamber, being connected to be equipped with to front side in the second cunning chamber roof extends
The first sliding groove of setting, extending end is connected setting with the holding tank on front side of the first sliding groove, the first cunning chamber and
Chamber front side end is slided in part between the second cunning chamber with described first equipped with rear side end to be connected the second deep gouge of setting, institute
It states to be rotatably assorted in the second deep gouge and is connected with driving gear, third cone pulley is installed in the driving gear front end face, it is described
It is rotatably assorted in part between second deep gouge and the second cunning chamber and is connected with front and back the second extended screw rod part, it is described
End is installed with the 4th for stretching into and being connected in second deep gouge and with the third cone pulley power on rear side of second screw rod part
Cone pulley, the second screw rod part front side extending end stretch into the second cunning intracavitary and match with the second cunning chamber front side wall rotation
Connection is closed, described second, which slides intracavitary, is equipped with top-pushing mechanism, is set by power supply slot, the left and right of the slider guide in the holding tank roof
The touch sensor to be oppositely arranged with the left and right sides inner wall of the guide runner is respectively equipped in both sides of the face, it is described to connect
Touch sensor is electrically connected with second motor, when the slider guide or so end face is touched respectively described in the left and right sides
When touch sensor, at this point, sending signal by the touch sensor and controlling second motor stalls.
2. a kind of civil aviation satellite communication system according to claim 1, it is characterised in that：On rear side of the driving gear
Maximum circumscribed circle, which stretches into described first, to be slided intracavitary and is connected with the tooth-strip part power.
3. a kind of civil aviation satellite communication system according to claim 2, it is characterised in that：The top-pushing mechanism includes
Sliding connection be arranged in the second cunning intracavitary and the second sliding block for being connect with the second screw rod part screw-thread fit and
It is slidably connected the propulsion arm for being arranged in the first sliding groove and being connect with the second sliding block secure fit, the pushing tow
Bar front side end is installed with sloped roof briquetting.
4. a kind of civil aviation satellite communication system according to claim 3, it is characterised in that：In the power supply groove top wall
It is installed with flexible power supply block.
5. a kind of civil aviation satellite communication system according to claim 4, it is characterised in that：The interconnecting piece rear side end
It is equipped with second sliding slot in face, the third sliding slot for extending downwardly setting, the third sliding slot are equipped in interconnecting piece roof end face
It is connected in front side wall equipped with guide groove, lock slide, the lock slide top end is slidably connected in the third sliding slot
Conductive trough is equipped in face, the lock slide bottom end is installed with inclined-plane sliding block, is slidably connected in the guide groove
The guide runner being connect with the lock slide secure fit, top pressure is connected in the guide groove on the upside of the guide runner
There is top pressure spring.
6. a kind of civil aviation satellite communication system according to claim 5, it is characterised in that：On rear side of the third sliding slot
End is oppositely arranged with the first sliding groove front side end.
7. a kind of application method of civil aviation satellite communication system according to claim 6, this method are：Original state
When, slider guide is located at the most forward position in guide runner, at this point, being utmostly located in holding tank by slider guide band rotation connection
Forward position, meanwhile, by interconnecting piece drive main body utmostly stretch out outside the front end face of outer housing, at this point, be oriented to slide
Block is made guide runner be located at the lowest position in guide groove by the pressure on top surface of top pressure spring, meanwhile, it is driven by guide runner
Lock slide end face is located in third sliding slot, at this point, driving the inclined-plane sliding block of bottom utmostly to stretch into the second cunning by lock slide
Slot, meanwhile, the first sliding block is located at the first lowest position for sliding intracavitary, at this point, making the first cone pulley and second in the first deep gouge
Cone pulley power is connected, meanwhile, the second sliding block is located at the second last side position for sliding intracavitary, at this point, being driven by the second sliding block
Propulsion arm and the sloped roof briquetting of propulsion arm front side end are fully located in the first sliding groove；
When need power in use, by the second motor control the first cone pulley rotation, by the first cone pulley drive the second cone pulley and
First screw rod part rotates, and then drives slider guide gradually to be slided towards the rear direction in guide runner by the first screw rod part, meanwhile, by
Slider guide drives satellite communication body gradually to stretch into holding tank, until slider guide slides into the last side position in guide runner,
At this point, drive satellite communication body to be fully inserted into holding tank by slider guide, meanwhile, make third sliding slot top end and power supply slot
Bottom end is in relative position, then, drives adjusting screw rod rotation by controlling first motor, first is driven by adjusting screw rod
The top-direction sliding that sliding block gradually slides intracavitary towards first, at this point, the first cone pulley in the first deep gouge is made to be detached from and be gradually distance from
Second cone pulley, meanwhile, drive driving gear and third cone pulley to rotate by tooth-strip part, and then the second screw rod is driven by third cone pulley
Part rotates, and drives the front side direction sliding that the second sliding block slides intracavitary towards second by the second screw rod part, at this point, by the second sliding block band
Sloped roof briquetting on dynamic propulsion arm and propulsion arm gradually stretches into second sliding slot, and makes sloped roof briquetting and inclined-plane sliding block
Top pressure slides cooperating, and then realizes the guide runner for having sliding block in inclined-plane to drive lock slide and be fixedly connected with lock slide
Overcome the pressure on top surface of top pressure spring and is gradually slided towards the top-direction in guide groove, meanwhile, keep lock slide top end gradual
It stretches into power supply slot, until when the top end surface of propulsion arm and the bottom end face top pressure of inclined-plane sliding block are slidably connected, this
When, inclined-plane sliding block is fully inserted into third sliding slot, meanwhile, so that lock slide top end is utmostly stretched into power supply slot, into
And the power supply block in power supply slot is made utmostly to stretch into conductive trough.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810493508.8A CN108768499A (en) | 2018-05-22 | 2018-05-22 | A kind of civil aviation satellite communication system and its application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810493508.8A CN108768499A (en) | 2018-05-22 | 2018-05-22 | A kind of civil aviation satellite communication system and its application method |
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| Publication Number | Publication Date |
|---|---|
| CN108768499A true CN108768499A (en) | 2018-11-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810493508.8A Withdrawn CN108768499A (en) | 2018-05-22 | 2018-05-22 | A kind of civil aviation satellite communication system and its application method |
Country Status (1)
| Country | Link |
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| CN (1) | CN108768499A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111049533A (en) * | 2019-12-24 | 2020-04-21 | 浦江光特通讯技术有限公司 | Disposable distress signal transmitting equipment utilizing wireless signal transmission |
| CN113241516A (en) * | 2021-05-06 | 2021-08-10 | 广州星博信息技术有限公司 | Communication transmission device based on satellite communication technology |
-
2018
- 2018-05-22 CN CN201810493508.8A patent/CN108768499A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111049533A (en) * | 2019-12-24 | 2020-04-21 | 浦江光特通讯技术有限公司 | Disposable distress signal transmitting equipment utilizing wireless signal transmission |
| CN113241516A (en) * | 2021-05-06 | 2021-08-10 | 广州星博信息技术有限公司 | Communication transmission device based on satellite communication technology |
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Application publication date: 20181106 |