CN108365461A - A kind of civil aircraft integrated avionics device - Google Patents
A kind of civil aircraft integrated avionics device Download PDFInfo
- Publication number
- CN108365461A CN108365461A CN201810138334.3A CN201810138334A CN108365461A CN 108365461 A CN108365461 A CN 108365461A CN 201810138334 A CN201810138334 A CN 201810138334A CN 108365461 A CN108365461 A CN 108365461A
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- CN
- China
- Prior art keywords
- slot
- block
- cavity
- power supply
- supply part
- 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
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
- H01R13/52—Dustproof, splashproof, drip-proof, waterproof, or flameproof cases
- H01R13/5213—Covers
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
- H01R13/639—Additional means for holding or locking coupling parts together, after engagement, e.g. separate keylock, retainer strap
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- Connector Housings Or Holding Contact Members (AREA)
Abstract
The invention discloses a kind of civil aircraft integrated avionics devices,Including body,The power supply part being fixedly mounted in the body back end surface and the avionic device to be connected with the power supply part,Peace access slot is equipped in the power supply part back end surface,Lock sliding slot is equipped in the peace access slot front inner wall,The first cavity is equipped in the power supply part on the upside of the lock sliding slot,The second cavity for upwardly extending setting is equipped in the power supply part on front side of first cavity,The first rotation slot being extended to front side is equipped in the power supply part on the upside of first cavity,Extending end is connected setting with second cavity on front side of first rotation slot,The first slippage slot for upwardly extending setting is equipped in the second cavity inner roof wall,The second slippage slot being extended to front side is equipped in the power supply part back end surface on the upside of the peace access slot.
Description
Technical field
The present invention relates to air equipment technical field, specially a kind of civil aircraft integrated avionics device.
Background technology
The structure type of modular chassis is usually used in avionic device in aviation field, and avionic device makes
It could be used with being required for inserting a plug into Power Block after energization, however the Power Block of existing avionic device is basic
It is all mounted in body, Power Block is directly connect with power supply, and the plug of avionic device is inserted directly into Power Block
Can be powered use, although operation is very easy for this inserting mode, since there is no settings to appoint between plug and Power Block
What locking structure easily causes connection to loosen so that can not normally power to electric avionic device, and while loosening
The danger for easily causing electric shock, to passenger's person, there are larger security risks.
Invention content
It is in the prior art for overcoming the purpose of the present invention is to provide a kind of civil aircraft integrated avionics device
Drawbacks described above.
A kind of civil aircraft integrated avionics device according to the present invention, including body, it is fixedly mounted on the body
Power supply part in back end surface and the avionic device to be connected with the power supply part, the power supply part
It is equipped with peace access slot in back end surface, lock sliding slot, the power supply on the upside of the lock sliding slot are equipped in the peace access slot front inner wall
It is equipped with the first cavity in component, the second sky for upwardly extending setting is equipped in the power supply part on front side of first cavity
Chamber, is equipped with the first rotation slot being extended to front side in the power supply part on the upside of first cavity, described first turn
Extending end is connected setting with second cavity on front side of dynamic slot, and the second cavity inner roof wall is interior equipped with upwardly extending setting
The first slippage slot, it is described peace access slot on the upside of the power supply part back end surface in be equipped with to front side be extended second slide
Move slot, extending end is connected setting, first rotation slot and institute with first slippage slot on front side of second slippage slot
Transition is connected with threaded rod extended up and down between stating the first cavity, and extending end stretches into institute at the top of the threaded rod
It states in the first rotation slot and is rotatably assorted with the first rotation slot inner roof wall and connect, threaded rod bottom extending end stretches into
It is rotatably assorted in first cavity and with the first cavity inner bottom wall and connect, the threaded rod in first rotation slot
It is circumferentially installed with first bevel gear on outer surface, is slidably connected in first cavity and the threaded rod screw-thread fit
The slipping block of connection, between first cavity and the lock sliding slot on rear side of the threaded rod perforation be equipped with connectivity slot, it is described
Interlocking bar extended up and down, the interlocking bar top extending end and the slipping block are slidably connected in connectivity slot
Bottom end face secure fit connects, and power sliding block, the power sliding block rear side end are slidably connected in second cavity
It is equipped with the second rotation slot in face, is rotatably assorted in second rotation slot and is connected with second bevel gear, the second bevel gear bottom
Portion's be connected by power has the drive motor being embedded in admittedly in the second rotation slot inner bottom wall, is slidably matched in first slippage slot
Be connected with extend downwardly setting lead shifting block, it is described lead to move block bottom extending end and fix with the power sliding block top end match
It closes and connects, described lead is moved equipped with inclined-plane sliding slot in block back end surface, described to lead the interior top of first slippage slot moved at the top of block
The first spring element of sliding connection is pressed, is equipped in second slippage slot to move pushing away for block power mating connection with described lead
Splenium part is installed with connecting rope in the body back end surface on the downside of the power supply part, and the connecting rope is far from the machine
Body side be equipped with to it is described peace access slot be connected dust plug, the dust plug by keep off connect block and with it is described gear connect block
The sealing block composition being fixedly connected, the gear connect block and connect far from the sealing block side and the connecting rope other end secure fit
It connects, electronic control unit, the electronic control unit and drive motor electricity is installed on the drive motor outer wall
Property connection, the electronic control unit realizes electric by the driving to control the velocity of rotation of the drive motor
Motivation controls the velocity of rotation of the second bevel gear.
Further technical solution, the avionic device include connecting component and electronic equipment body, the company
The peace that relay part includes grafting body, is fixedly mounted on the grafting body left end face connects block and is fixedly mounted on the grafting body
The conducting wire of right-hand end, the conducting wire are connect far from the grafting body side end with the electronic equipment body secure fit, institute
It states peace and connects block and be installed with locking part far from grafting body side, locking hole is equipped in the locking part, the locking part is separate
The peace connects is installed with conductive head on one side end face of block.
Further technical solution, the interior confession being equipped with to be connected with the conductive head of lock sliding slot front inner wall
Electric slot.
Further technical solution, the maximum circumscribed circle in first bevel gear front side stretches into second cavity, described
On rear side of second bevel gear maximum circumscribed circle stretch out the power sliding block back end surface it is outer and to the first bevel gear power
It is connected.
Further technical solution, the push part include front and back extension and are slidably matched company with second slippage slot
The pushing block connect, pushing block front side extending end are installed with inclined-plane sliding block, and extending end stretches out on rear side of the pushing block
The power supply part back end surface, the second slippage slot inner roof wall is interior to be equipped with third slippage slot, is slided in the third slippage slot
It is dynamic to be connected with the convex block that bottom end is connect with the pushing block top end surface secure fit, it is described on front side of the convex block
The second spring element is equipped in third slippage slot.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, it is easy to operate, lock cunning is set in access slot front inner wall by pacifying
Slot is locked in the power supply part on the upside of sliding slot and sets the first cavity, set in the power supply part on front side of the first cavity and upwardly extend setting
Second cavity, sets the first rotation slot being extended to front side in the power supply part on the upside of the first cavity, on front side of the first rotation slot
Extending end is connected setting with the second cavity, the first slippage slot for upwardly extending setting is set in the second cavity inner roof wall, peace connects
The second slippage slot being extended to front side, the second slippage slot front side extending end are set in power supply part back end surface on the upside of slot
Be connected setting with the first slippage slot, the screw thread that transition mating connection is extended up and down between the first rotation slot and the first cavity
Bar, threaded rod top extending end, which is stretched into the first rotation slot and is rotatably assorted with the first rotation slot inner roof wall, to be connect, threaded rod
Bottom extending end is stretched into the first cavity and is rotatably assorted with the first cavity inner bottom wall and connect, the threaded rod in the first rotation slot
Circumferential fixed first bevel gear on outer surface, the sliding that the interior sliding connection of the first cavity is connect with threaded rod screw-thread fit
Block, between the first cavity on rear side of threaded rod and lock sliding slot perforation set connectivity slot, in connectivity slot sliding connection extend up and down
The interlocking bar of setting, interlocking bar top extending end connect with slipping block bottom end face secure fit, slide and match in the second cavity
Connection power sliding block is closed, the second rotation slot is set in power sliding block back end surface, be rotatably assorted the second cone of connection in the second rotation slot
Gear, second bevel gear bottom be connected by power is embedded in the drive motor in the second rotation slot inner bottom wall admittedly, in the first slippage slot
What sliding connection extended downwardly setting leads shifting block, leads and moves block bottom extending end and power sliding block top end secure fit
Connection leads to move in block back end surface setting inclined-plane sliding slot, leads and moves top pressure sliding connection the in the first slippage slot at the top of block
One spring element, set in the second slippage slot to lead the push part moved block power and be connected, automatically control lock to realize
Determine installment work, improves the working efficiency and stability of data connection.
Description of the drawings
Fig. 1 is organism internal structure schematic diagram in the present invention；
Fig. 2 is power supply part internal structure schematic diagram in the present invention；
Fig. 3 is the overall structure diagram of avionic device in the present invention；
Fig. 4 is power supply part rearview in the present invention.
Specific implementation mode
With reference to Fig. 1-Fig. 4, the present invention is described in detail.
- Fig. 4 referring to Fig.1, a kind of civil aircraft integrated avionics device according to an embodiment of the invention, including body
5, the power supply part 6 being fixedly mounted in 5 back end surface of the body and the boat to be connected with the power supply part 6
Empty electronic equipment, 6 back end surface of the power supply part is interior to be equipped with peace access slot 61, is equipped with to lock in 61 front inner wall of peace access slot and slide
Slot 62, is equipped with the first cavity 63 in the power supply part 6 of the lock sliding slot 62 upside, first cavity, 63 front side it is described
It is equipped with the second cavity 65 for upwardly extending setting in power supply part 6, is set in the power supply part 6 of first cavity, 63 upside
The first extended rotation slot 66 of oriented front side, first rotation slot, 66 front side extending end and 65 phase of the second cavity
Connection setting, is equipped with the first slippage slot 68 for upwardly extending setting in 65 inner roof wall of the second cavity, on the peace access slot 61
The second slippage slot 67 being extended to front side, second slippage slot 67 are equipped in 6 back end surface of the power supply part of side
Front side extending end is connected setting with first slippage slot 68, between first rotation slot 66 and first cavity 63
Transition is connected with threaded rod 661 extended up and down, and 661 top extending end of the threaded rod stretches into described first turn
It is rotatably assorted in dynamic slot 66 and with 66 inner roof wall of the first rotation slot and connect, 661 bottom extending end of the threaded rod stretches into
It is rotatably assorted in first cavity 63 and with 63 inner bottom wall of the first cavity and connect, it is described in first rotation slot 66
First bevel gear 662 is circumferentially installed on 661 outer surface of threaded rod, be slidably connected in first cavity 63 with it is described
First cavity 63 of the slipping block 631 of 661 screw-thread fit of threaded rod connection, 661 rear side of the threaded rod is slided with the lock
Perforation is equipped with connectivity slot 64 between slot 62, and interlocking bar 641 extended up and down is slidably connected in the connectivity slot 64,
641 top extending end of the interlocking bar is connect with 631 bottom end face secure fit of the slipping block, in second cavity 65
It is slidably connected with power sliding block 651, is equipped with the second rotation slot 652 in 651 back end surface of the power sliding block, described second
It is rotatably assorted in rotation slot 652 and is connected with second bevel gear 653,653 bottom be connected by power of the second bevel gear has to be embedded in admittedly
Drive motor 654 in second rotation slot, 652 inner bottom wall is slidably connected in first slippage slot 68 downwards
Extended leading moves block 681, and the shifting 681 bottom extending end of block of leading is matched with the fixation of 651 top end of the power sliding block
Connection is closed, described lead is equipped with inclined-plane sliding slot 684 in shifting 681 back end surface of block, described to lead first cunning for moving 681 top of block
It moves top pressure in slot 68 and is slidably connected the first spring element 682, be equipped in second slippage slot 67 to lead shifting block with described
The push part that 681 power are connected is installed with connecting rope in 5 back end surface of the body of the downside of the power supply part 6
692, the connecting rope 692 is equipped with the dust plug 69 to be connected with the peace access slot 61, institute far from 5 side of the body
It states dust plug 69 to be connect block 691 by gear and connect the sealing block 692 that block 691 is fixedly connected with the gear and form, the gear connects block 691
It is connect with 692 other end secure fit of the connecting rope far from 692 side of the sealing block, 654 outer wall of the drive motor
On be installed with electronic control unit 6541, the electronic control unit 6541 is electrically connected with the drive motor 654, described
Electronic control unit 6541 is realized to control the velocity of rotation of the drive motor 654 by the drive motor
654 control the velocity of rotation of the second bevel gear 653.
Valuably or illustratively, the avionic device includes connecting component 7 and electronic equipment body 8, described
The peace that connecting component 7 includes grafting body 74, is fixedly mounted on 74 left end face of grafting body connects block 71 and is fixedly mounted on
The conducting wire 72 of 74 right-hand end of grafting body, the conducting wire 72 is far from 74 side end of grafting body and the electronic equipment machine
8 secure fit of body connects, and the peace connects block 71 and is installed with locking part 73 far from 74 side of grafting body, in the locking part 73
Equipped with locking hole 731, the locking part 73 connects far from the peace and is installed with conductive head 732 on 71 1 side end face of block, to convenient
It is conductively connected work.
Valuably or illustratively, it is equipped in 62 front inner wall of lock sliding slot and connects to coordinate with the conductive head 732
The power supply slot 621 connect.
Valuably or illustratively, the maximum circumscribed circle in 662 front side of the first bevel gear stretches into second cavity 65,
It is outer and to described first that the maximum circumscribed circle of the rear side of the second bevel gear 653 stretches out 651 back end surface of power sliding block
662 power of bevel gear is connected, and automatically controls power drive work to realize, can realize and automatically control locking and unlock
Control work.
Valuably or illustratively, the push part includes front and back extension and is slidably matched with second slippage slot 67
The pushing block 671 of connection, 671 front side extending end of the pushing block are installed with inclined-plane sliding block 672, after the pushing block 671
Side extending end stretches out 6 back end surface of power supply part, and third slippage slot is equipped in 67 inner roof wall of the second slippage slot
673, bottom end and 671 top end surface secure fit of the pushing block are slidably connected in the third slippage slot 673
The convex block 674 of connection, the third slippage slot 673 of 674 front side of the convex block is interior to be equipped with the second spring element 675, to pass through
Pressing control realizes that first bevel gear 662 and the be connected by power of second bevel gear 653 work, easy to operate, improves data connection
Working efficiency and stability.
When original state, slipping block 631 is located at the top position in the first cavity 63, at this point, being driven by slipping block 631
641 top section of interlocking bar utmostly stretches into the first cavity 63, meanwhile, keep 641 bottom end of interlocking bar utmostly separate
It locks in sliding slot 62, at this point, convex block 674 is made convex block 674 be located in third slippage slot 673 by 675 pressure on top surface of the second spring element
Last side position, meanwhile, drive 671 rear side end of pushing block utmostly to stretch out 6 back end surface of power supply part by convex block 674
Outside, at this point, driving the inclined-plane sliding block 672 of front side end to be fully inserted into the second slippage slot 67 by pushing block 671, meanwhile, it leads
Block 681 is moved by 682 pressure on top surface of the first spring element, makes to lead and moves 681 bottom end of block and utmostly stretch into the first slippage slot 68,
Meanwhile power sliding block 651 being made to be located at the lowest position in the second cavity 65, at this point, keeping second bevel gear 653 utmostly remote
From first bevel gear 662, meanwhile, so that 684 backside top of inclined-plane sliding slot is in relative position with inclined-plane sliding block 672, at this point,
The sealing block 692 on dust plug 69 is set to be fully located in peace access slot 61, meanwhile, so that gear is connect the front side end of block 691 and power supply part 6
Face abuts against.
While power is being supplied, dust plug 69 is taken out completely first from peace access slot 61, avionic device 7 is then moved to confession
The relative position of electrical components 6, meanwhile, so that locking part 73 is completely in relative position with lock sliding slot 62, then to power supply
6 side of part move avionic device 7, until locking part 73 be fully inserted into lock sliding slot 62 in when, at this point, make locking hole 731 with
Connectivity slot 64 is in relative position, by pressing pushing block 671, makes pushing block 671 that convex block 674 be driven to overcome the second spring element
675 pressure on top surface and gradually the front side direction sliding in third slippage slot 673, push away at this point, stretching into inclined-plane by inclined-plane sliding block 672
It is slidably connected in sliding slot 684 and with 684 top pressure of inclined-plane sliding slot, meanwhile, it is led by the drive of inclined-plane sliding block 672 and moves block 681
Top-direction sliding of 682 pressure on top surface of the first spring element gradually in the first slippage slot 68 is overcome, at this point, moving 681 band of block by leading
The gradually top-direction sliding in the second cavity 65 of dynamic power sliding block 651, until power sliding block 651 slides into the second cavity 65
Interior top position, at this point, making power sliding block 651 that second bevel gear 653 be driven to connect with the cooperation of 662 power of first bevel gear
It connects, then drives second bevel gear 653 to rotate by controlling drive motor 654, the first cone tooth is driven by second bevel gear 653
662 rotation of wheel, at this point, drive threaded rod 661 to rotate by first bevel gear 662, meanwhile, slipping block 631 is driven by threaded rod 661
The gradually bottom direction sliding in the first cavity 63, at this point, driving interlocking bar 641 gradually along connectivity slot 64 by slipping block 631
Interior bottom direction sliding, while 641 bottom end of interlocking bar gradually stretches into locking hole 731, until slipping block 631 slides into
When lowest position in the first cavity 63, then unclamps pushing block 671 and locking can be completed.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, it is easy to operate, lock cunning is set in access slot front inner wall by pacifying
Slot is locked in the power supply part on the upside of sliding slot and sets the first cavity, set in the power supply part on front side of the first cavity and upwardly extend setting
Second cavity, sets the first rotation slot being extended to front side in the power supply part on the upside of the first cavity, on front side of the first rotation slot
Extending end is connected setting with the second cavity, the first slippage slot for upwardly extending setting is set in the second cavity inner roof wall, peace connects
The second slippage slot being extended to front side, the second slippage slot front side extending end are set in power supply part back end surface on the upside of slot
Be connected setting with the first slippage slot, the screw thread that transition mating connection is extended up and down between the first rotation slot and the first cavity
Bar, threaded rod top extending end, which is stretched into the first rotation slot and is rotatably assorted with the first rotation slot inner roof wall, to be connect, threaded rod
Bottom extending end is stretched into the first cavity and is rotatably assorted with the first cavity inner bottom wall and connect, the threaded rod in the first rotation slot
Circumferential fixed first bevel gear on outer surface, the sliding that the interior sliding connection of the first cavity is connect with threaded rod screw-thread fit
Block, between the first cavity on rear side of threaded rod and lock sliding slot perforation set connectivity slot, in connectivity slot sliding connection extend up and down
The interlocking bar of setting, interlocking bar top extending end connect with slipping block bottom end face secure fit, slide and match in the second cavity
Connection power sliding block is closed, the second rotation slot is set in power sliding block back end surface, be rotatably assorted the second cone of connection in the second rotation slot
Gear, second bevel gear bottom be connected by power is embedded in the drive motor in the second rotation slot inner bottom wall admittedly, in the first slippage slot
What sliding connection extended downwardly setting leads shifting block, leads and moves block bottom extending end and power sliding block top end secure fit
Connection leads to move in block back end surface setting inclined-plane sliding slot, leads and moves top pressure sliding connection the in the first slippage slot at the top of block
One spring element, set in the second slippage slot to lead the push part moved block power and be connected, automatically control lock to realize
Determine installment work, improves working efficiency and stability for electrical connection.
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 (5)
1. a kind of civil aircraft integrated avionics device, including body, the confession that is fixedly mounted in the body back end surface
Electrical components and avionic device to be connected with the power supply part, it is characterised in that：After the power supply part
It is equipped with peace access slot in side end face, lock sliding slot, the power supply on the upside of the lock sliding slot are equipped in the peace access slot front inner wall
It is equipped with the first cavity in part, the second cavity for upwardly extending setting is equipped in the power supply part on front side of first cavity,
The first rotation slot being extended to front side, first rotation slot are equipped in the power supply part on the upside of first cavity
Front side extending end is connected setting with second cavity, is equipped in the second cavity inner roof wall and upwardly extends the of setting
One slippage slot, the power supply part back end surface pacified on the upside of access slot is interior to be equipped with the second sliding being extended to front side
Slot, extending end is connected setting with first slippage slot on front side of second slippage slot, first rotation slot with it is described
Transition is connected with threaded rod extended up and down between first cavity, and threaded rod top extending end stretches into described
It is rotatably assorted in first rotation slot and with the first rotation slot inner roof wall and connect, threaded rod bottom extending end stretches into institute
It states in the first cavity and is rotatably assorted with the first cavity inner bottom wall and connect, outside the threaded rod in first rotation slot
It is circumferentially installed with first bevel gear on surface, is slidably connected in first cavity and connects with the threaded rod screw-thread fit
The slipping block connect, between first cavity and the lock sliding slot on rear side of the threaded rod perforation be equipped with connectivity slot, the company
Interlocking bar extended up and down, the interlocking bar top extending end and the slipping block bottom are slidably connected in straight slot
End surface secure fit connects, and power sliding block, the power sliding block back end surface are slidably connected in second cavity
It is inside equipped with the second rotation slot, is rotatably assorted in second rotation slot and is connected with second bevel gear, the second bevel gear bottom
Be connected by power has the drive motor being embedded in admittedly in the second rotation slot inner bottom wall, the company of being slidably matched in first slippage slot
Be connected to extend downwardly setting lead shifting block, described lead moves block bottom extending end and the power sliding block top end secure fit
Connection, described lead are equipped with inclined-plane sliding slot in shifting block back end surface, described lead moves top pressure in first slippage slot at the top of block
It is slidably connected the first spring element, is equipped in second slippage slot to lead the pushing for moving block power and being connected with described
Component is installed with connecting rope in the body back end surface on the downside of the power supply part, and the connecting rope is far from the body
Side is equipped with the dust plug to be connected with the peace access slot, and the dust plug is consolidated by keeping off connecing block and connecing block with the gear
Surely the sealing block composition connected, the gear connect block and connect far from the sealing block side and the connecting rope other end secure fit
It connects, electronic control unit, the electronic control unit and drive motor electricity is installed on the drive motor outer wall
Property connection, the electronic control unit realizes electric by the driving to control the velocity of rotation of the drive motor
Motivation controls the velocity of rotation of the second bevel gear.
2. a kind of civil aircraft integrated avionics device according to claim 1, it is characterised in that：The aviation electronics
Equipment includes connecting component and electronic equipment body, and the connecting component includes grafting body, is fixedly mounted on the grafting body
The peace of left end face connects block and is fixedly mounted on the conducting wire of the grafting body right-hand end, and the conducting wire is far from the grafting body one
Side end is connect with the electronic equipment body secure fit, and the peace connects block and is installed with locking far from grafting body side
Part, the locking part is interior to be equipped with locking hole, and the locking part connects far from the peace and is installed with conductive head on one side end face of block.
3. a kind of civil aircraft integrated avionics device according to claim 2, it is characterised in that：Before the lock sliding slot
The power supply slot to be connected with the conductive head is equipped in the inner wall of side.
4. a kind of civil aircraft integrated avionics device according to claim 1, it is characterised in that：The first cone tooth
The maximum circumscribed circle in wheel front side stretches into second cavity, and maximum circumscribed circle stretches out the power and slides on rear side of the second bevel gear
Block back end surface is outer and to be connected with the first bevel gear power.
5. a kind of civil aircraft integrated avionics device according to claim 1, it is characterised in that：The push part
Including the front and back pushing block extended and be slidably connected with second slippage slot, extending end is fixed on front side of the pushing block
There is an inclined-plane sliding block, extending end stretches out the power supply part back end surface on rear side of the pushing block, in second slippage slot
It is equipped with third slippage slot in roof, bottom end and the pushing block top end are slidably connected in the third slippage slot
The convex block of face secure fit connection is equipped with the second spring element in the third slippage slot on front side of the convex block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810138334.3A CN108365461A (en) | 2018-02-10 | 2018-02-10 | A kind of civil aircraft integrated avionics device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810138334.3A CN108365461A (en) | 2018-02-10 | 2018-02-10 | A kind of civil aircraft integrated avionics device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108365461A true CN108365461A (en) | 2018-08-03 |
Family
ID=63005375
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810138334.3A Withdrawn CN108365461A (en) | 2018-02-10 | 2018-02-10 | A kind of civil aircraft integrated avionics device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108365461A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109193267A (en) * | 2018-09-27 | 2019-01-11 | 永嘉县嘉和教育科技有限公司 | A kind of locking plugs and sockets device of rotation eye-splice-type and application method |
| CN109286102A (en) * | 2018-09-27 | 2019-01-29 | 王迩笃 | A kind of portable of double-button loosens plug device and application method |
-
2018
- 2018-02-10 CN CN201810138334.3A patent/CN108365461A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109193267A (en) * | 2018-09-27 | 2019-01-11 | 永嘉县嘉和教育科技有限公司 | A kind of locking plugs and sockets device of rotation eye-splice-type and application method |
| CN109286102A (en) * | 2018-09-27 | 2019-01-29 | 王迩笃 | A kind of portable of double-button loosens plug device and application method |
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Application publication date: 20180803 |
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| WW01 | Invention patent application withdrawn after publication |