CN110290337A - A kind of general-purpose aircraft TV convenient for adjusting - Google Patents
A kind of general-purpose aircraft TV convenient for adjusting Download PDFInfo
- Publication number
- CN110290337A CN110290337A CN201910504951.5A CN201910504951A CN110290337A CN 110290337 A CN110290337 A CN 110290337A CN 201910504951 A CN201910504951 A CN 201910504951A CN 110290337 A CN110290337 A CN 110290337A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- liquid crystal
- support base
- crystal display
- centimetres
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N21/00—Selective content distribution, e.g. interactive television or video on demand [VOD]
- H04N21/40—Client devices specifically adapted for the reception of or interaction with content, e.g. set-top-box [STB]; Operations thereof
- H04N21/41—Structure of client; Structure of client peripherals
- H04N21/414—Specialised client platforms, e.g. receiver in car or embedded in a mobile appliance
- H04N21/41422—Specialised client platforms, e.g. receiver in car or embedded in a mobile appliance located in transportation means, e.g. personal vehicle
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N5/00—Details of television systems
- H04N5/64—Constructional details of receivers, e.g. cabinets or dust covers
Abstract
The invention discloses a kind of general-purpose aircraft TVs convenient for adjusting, including dorsal plate and fuselage, the table end of the rear side of the fuselage is provided with dorsal plate, the dorsal plate is connected by screw at the table end of the rear side of fuselage, the dorsal plate is fixedly connected with fuselage by screw, the liquid crystal display of a cuboid is provided at the axle center of the table side of the front end of the fuselage, pass through the composite structure for being internally provided with fixed lid and attachment spacers of rotation axis in the device in the present invention, it can make preferably be rotated under the action of fixed lid is with attachment spacers in this way, the service life of the equipment can be made to be improved and operationally also relatively simple in this way, and the end of one end of the separate limited block of fixed link is provided with threaded post, fixed lid can be made not rotate between fixed link in this way, from And it can to can connect between fixed lid and fixed link more close.
Description
Technical field
The invention belongs to space flight and aviation correlative technology fields, and in particular to a kind of general-purpose aircraft TV convenient for adjusting.
Background technique
Aircraft shows that equipment is directed to pilot and provides the comprehensively monitoring and cockpit display control for optimizing context-aware
The equipment of system reduces the accident quantity of civil aviation.Avionics airborne equipment and cockpit man-machine interface must be improved.
Existing general-purpose aircraft is had the following problems with TV tech: existing general-purpose aircraft is with TV when being shown
Usually all be the display screen is fixed, needs just need to adjust before the mounting good position in this way, and make in driver
With when the use of display screen may be brought not in this way since the effect of light is so that cannot clearly be observed
Just, some display screens may be rotated, but the frictional force between it may be such that under frequent rotation reduces, for a long time
May be such that later leads to that there is a phenomenon where topple over occurring frictional force deficiency in rotation.
Summary of the invention
The purpose of the present invention is to provide a kind of general-purpose aircraft TVs convenient for adjusting, to solve in above-mentioned background technique
The existing general-purpose aircraft TV proposed is usually all to be fixedly mounted, when some TVs may be rotated but is long although
Between multiple rotation under may be such that the reduction due to frictional force leads to the bad problem of effect that rotates.
To achieve the above object, the invention provides the following technical scheme: a kind of general-purpose aircraft TV convenient for adjusting, packet
Dorsal plate and fuselage are included, the table end of the rear side of the fuselage is provided with dorsal plate, and the dorsal plate is connected by screw in fuselage
Rear side table end, the dorsal plate is fixedly connected by screw with fuselage, set at the axle center of the table side of the front end of the fuselage
It is equipped with the liquid crystal display of a cuboid, the liquid crystal display passes through bonding connection in the table side axle center of the front end of fuselage
Place, the fuselage and liquid crystal display are provided with bottom plate by bonding connection, the lower end of the fuselage, and the fuselage passes through socket
It is connected to the table side of the upper end of bottom plate, the fuselage and bottom plate to connect by socket, the table of the upside at the axle center of the bottom plate
Face is provided with operation key close to the side of liquid crystal display, and the operation key is connected to one close to liquid crystal display by socket
The surface of the upper end of the bottom plate of side, the operation key and bottom plate pass through socket connection, the axis of the upper end of the inside of the operation key
Power switch is provided at the heart, the power switch is connected at the center of the inside of operation key, the power switch and bottom plate
It is connected by socket, the table side of the lower end of the bottom plate is provided with rotation axis, and the rotation axis is connected to bottom plate by socket
The table side of lower end, the rotation axis and bottom plate are electrically connected by socket connection, the liquid crystal display and power switch, described
Operation key and power switch are electrically connected.
Preferably, the composition of the rotation axis includes fixed lid, attachment spacers, fixed link and limited block, the limit
The left and right ends of block are each provided with a fixed link, and two fixed links are each provided with a connection far from the side of limited block
Gasket, two attachment spacers are each provided with a fixed lid far from the side of two fixed links, and the rotation axis is logical
It crosses fixed link and fuselage and passes through socket connection.
Preferably, the composition of the fixed lid includes end cap, main body, sliding slot and thread groove, and the right end of the end cap is set
It is equipped with main body, sliding slot is provided on the inside of the right end of the main body, thread groove, the fixed lid are provided on the inside of the sliding slot
It is connect with fixed link by screw thread rotation by thread groove.
Preferably, the composition of the attachment spacers includes convex block, ontology, through-hole and friction washer, the right side of the convex block
End is provided with ontology, and the right end of the ontology is provided with friction washer, and one is provided at the axle center of the inside of the ontology and is led to
Hole, the attachment spacers pass through plug connection, the torus structure of the convex block and inner hollow, institute by convex block and fixed lid
The maximum diameter of section for stating convex block is 4 points 9 centimetres, and the smallest diameter of section of the convex block is 4 points 4 centimetres.
Preferably, the composition of the dorsal plate includes terminals, the first support base, the second support base and plate body, described
Second support base is each provided at left and right sides of the lower end of the inside of plate body, the lower end of two second support bases is each
First support base, first support base and the second support base is provided with to connect by socket, the inside of the plate body
The table side of lower end is provided with terminals, and the dorsal plate is fixedly connected with fuselage by screw by plate body.
Preferably, first support base and the second support base are the prismatoid structure of plate, first support base with
There are two second support base is arranged altogether, two first support bases and the second support base are in symmetrically to be set in qually spaced in plate respectively
The left and right sides at the table end of body, two first support bases and the second support base pass through socket connection.
Preferably, the fixed link is cylindrical structure, and the fixed link is provided with two altogether, two fixed links point
Cheng not be set in qually spaced in the table side of the left and right ends of limited block symmetrically, the length of two fixed links be six centimetres,
The end point of two one end of the fixed link far from limited block is each provided with the cylindrical structure of a threaded circle, two institutes
The diameter of section for stating fixed link is three centimetres.
Preferably, the ontology is the torus structure of inner hollow, and the diameter of section of the outer circle of the ontology is four lis
Rice, the ontology are internally provided with through-hole, and the diameter of section of the through-hole is three centimetres, there are two the ontology is arranged altogether,
Two ontologies are in the inside for being symmetrically set in qually spaced in the close limited block of the fixed lid of two sides respectively.
Preferably, the liquid crystal display is the structure of cuboid, and the length of the liquid crystal display is ten centimetres, described
The width of liquid crystal display is eight centimetres, and the wall thickness of the liquid crystal display is eight millimeters, and the liquid crystal display is opened with power supply
It closes and is electrically connected.
Preferably, the sliding slot is the torus structure of inner hollow, and the maximum diameter of section of the sliding slot is five lis
Rice, the smallest diameter of section of the sliding slot are 4 points 5 centimetres.
Compared with prior art, the present invention provides a kind of general-purpose aircraft TV convenient for adjusting, have following beneficial
Effect:
(1), pass through the combination for being internally provided with fixed lid and attachment spacers of rotation axis in the device in the present invention
Structure can allow in this way in fixation lid and make the fuselage being socketed inside bottom plate upper end more preferable under the action of attachment spacers
Carry out rotate, and will not be caused by prolonged rotation so that the problem of frictional force reduces, can make this in this way
The service life of equipment is improved and operationally also relatively simple；
(2), threaded post is provided with by the end of one end of the separate limited block in fixed link in the present invention, and solid
Surely what is covered is internally provided with thread groove, can make connect by screw thread rotation between fixed link and fixed lid in this way, and
And it is provided with attachment spacers between fixed lid and fixed link, in the fixed sliding slot that is internally provided with covered close to fixed link, connection
Gasket is provided with the convex block connecting with sliding slot close to one end of sliding slot, can make when being rotated in this way, attachment spacers exists
Fixed lid will not be made to rotate by convex block when rotation, fixed lid can be made not send out between fixed link in this way
Raw rotation, so that be can connect between fixed lid and fixed link is more close, to solve existing logical
It is usually all to be fixedly mounted with aircraft TV, some TVs although may be rotated but prolonged multiple rotation
Under may be such that the reduction due to frictional force leads to the bad problem of effect that rotates.
Detailed description of the invention
Fig. 1 is general-purpose aircraft TV structural schematic diagram of the invention；
Fig. 2 is rotation shaft structure schematic diagram of the invention；
Fig. 3 is fixation lid structural schematic diagram of the invention；
Fig. 4 is lever connection spacing piece structure schematic diagram of the invention；
Fig. 5 is dorsal plate structural schematic diagram of the invention；
In figure: 1, rotation axis；11, fixed lid；111, end cap；112, main body；113, sliding slot；114, thread groove；12, it connects
Gasket；121, convex block；122, ontology；123, through-hole；124, friction washer；13, fixed link；14, limited block；2, power switch；
3, operation key；4, bottom plate；5, dorsal plate；51, terminals；52, the first support base；53, the second support base；54, plate body；6, liquid crystal
Display screen；7, fuselage.
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. 1-5 is please referred to, the present invention provides a kind of technical solution: a kind of general-purpose aircraft TV convenient for adjusting, including
Dorsal plate 5 and fuselage 7, the table end of the rear side of fuselage 7 are provided with dorsal plate 5, and the composition of dorsal plate 5 includes terminals 51, the
One support base 52, the second support base 53 and plate body 54 are each provided with one at left and right sides of the lower end of the inside of plate body 54
Two support bases 53, the lower end of two the second support bases 53 are each provided with first support base 52, the first support base 52 and second
Support base 53 passes through socket connection, the prismatoid structure of the first support base 52 and the second support base 53 for plate, the first support base
52 and second support base 53 altogether there are two settings, by the setting of two the first support bases 52 and the second support base 53, in this way may be used
So that preferably work under the action of the support of the first support base 52 and the second support base 53, two the first support bases
52 and second support base 53 respectively in be symmetrically set in qually spaced in plate body 54 table end the left and right sides, two the first support bases 52
With the second support base 53 by socket connection, the table side of the lower end of the inside of plate body 54 is provided with terminals 51, passes through terminals
51 setting can make power supply wiring can be allowed preferably to be attached under the action of terminals 51 in this way, from
And can preferably work, dorsal plate 5 is fixedly connected with fuselage 7 by screw by plate body 54, and dorsal plate 5 passes through screw
It is connected to the table end of the rear side of fuselage 7, dorsal plate 5 is fixedly connected with fuselage 7 by screw,
A kind of general-purpose aircraft TV convenient for adjusting is provided with one at the axle center of the table side of the front end including fuselage 7
The liquid crystal display 6 of cuboid, liquid crystal display 6 are the structure of cuboid, and the length of liquid crystal display 6 is ten centimetres, liquid crystal
The width of display screen 6 is eight centimetres, so that liquid crystal display 6 can have the effect preferably watched, liquid crystal
The wall thickness of display screen 6 is eight millimeters, and liquid crystal display 6 and power switch 2 are electrically connected, and liquid crystal display 6 is existed by bonding connection
At the table side axle center of the front end of fuselage 7, by bonding connection, the lower end of fuselage 7 is provided with bottom plate for fuselage 7 and liquid crystal display 6
4, fuselage 7 is connected to the table side of the upper end of bottom plate 4 by socket, and fuselage 7 and bottom plate 4, which pass through, is socketed connection, at the axle center of bottom plate 4
The surface of upside the side of liquid crystal display 6 is provided with operation key 3, operation key 3 is connected to by socket close to liquid crystal
The surface of the upper end of the bottom plate 4 of the side of display screen 6, operation key 3 and bottom plate 4 by socket connection, the inside of operation key 3 it is upper
Power switch 2 is provided at the axle center at end, power switch 2 is connected at the center of the inside of operation key 3, power switch 2 and bottom
For plate 4 by socket connection, the table side of the lower end of bottom plate 4 is provided with rotation axis 1, and the composition of rotation axis 1 includes fixed lid 11, connects
Connection pad piece 12, fixed link 13 and limited block 14, the left and right ends of limited block 14 are each provided with a fixed link 13, two fixed links
13 sides far from limited block 14 are each provided with an attachment spacers 12, by the setting of attachment spacers 12, can make in this way
Under the action of attachment spacers 12, the effect preferably rotated can be made, fixed lid 11 will not occur in this way and fix
There is a phenomenon where sliding between bar 13,
A kind of general-purpose aircraft TV convenient for adjusting, including two sides of the attachment spacers 12 far from two fixed links 13
It is each provided with a fixed lid 11, the composition of attachment spacers 12 includes convex block 121, ontology 122, through-hole 123 and friction washer
124, the right end of convex block 121 is provided with ontology 122, and ontology 122 is the torus structure of inner hollow, the outer circle of ontology 122
Diameter of section is four centimetres, and ontology 122 is internally provided with through-hole 123, can make the diameter of section of through-hole 123 in this way and consolidate
The diameter of section of fixed pole 13 is identical, can make the effect being preferably socketed in this way, and the diameter of section of through-hole 123 is three lis
Rice, ontology 122 is altogether there are two settings, and two ontologies 122 are respectively in the close of the fixation lid 11 for being symmetrically set in qually spaced in two sides
The inside of limited block 14, the right end of ontology 122 are provided with friction washer 124, in this way can be with by the setting of friction washer 124
Allowing can preferably be contacted when being rotated with friction washer 124, so that turning to suitably
A through-hole 123 will not be provided at the axle center of the inside of ontology 122 there is a phenomenon where toppling over when position, attachment spacers 12 is logical
Convex block 121 and fixed lid 11 are crossed by plug connection, the composition of fixed lid 11 includes end cap 111, main body 112,113 and of sliding slot
Thread groove 114, the right end of end cap 111 are provided with main body 112, and sliding slot 113, sliding slot 113 are provided on the inside of the right end of main body 112
For the torus structure of inner hollow, the maximum diameter of section of sliding slot 113 is five centimetres, and the smallest section of sliding slot 113 is straight
Diameter is 4 points 5 centimetres, the torus structure of convex block 121 and inner hollow, and the maximum diameter of section of convex block 121 is four points nine
Centimetre, the smallest diameter of section of convex block 121 is 4 points 4 centimetres, by the setting of round sliding slot 113, can be made so convex
Block 121 can preferably can carry out socket connection with sliding slot 113, and the inside of sliding slot 113 is provided with thread groove 114, fixed lid
11 are connect with fixed link 13 by screw thread rotation by thread groove 114,
A kind of general-purpose aircraft TV convenient for adjusting, including rotation axis 1 pass through set in succession by fixed link 13 and fuselage 7
It connects, fixed link 13 is cylindrical structure, and fixed link 13 is provided with two altogether, and two fixed links 13 are in symmetrical spaced set respectively
Table side in the left and right ends of limited block 14 can make preferably to work in this way by the setting of two fixed links 13,
To be six centimetres, the end point of two one end of fixed link 13 far from limited block 14 is each provided with the length of two fixed links 13
The cylindrical structure of one threaded circle, the diameter of section of two fixed links 13 are three centimetres, and rotation axis 1 is connected to by socket
The table side of the lower end of bottom plate 4, rotation axis 1 and bottom plate 4 are electrically connected by socket connection, liquid crystal display 6 and power switch 2,
Operation key 3 and power switch 2 are electrically connected.
The working principle of the invention and process for using: it after the present invention installs, first checks for such machine and whether can
It works normally, checks that the plug on electric wire is finished with whether socket connect, if there is abnormal noise, should close immediately such
Machine waits the maintenance of professional, when the TV that carry out the general-purpose aircraft is in use, first take the television equipment
Out, packing box is taken out, and tool ready for use is placed on to the side of the television equipment, and usual when everything in readiness
Tool stablizes the position installation to be installed of the television equipment and general-purpose aircraft, at this moment passes through the wiring inside dorsal plate 5
End 51 is connect with the power supply line inside general-purpose aircraft, and is correctly attached, and when stable connection, at this moment presses power switch
2, the liquid crystal display 6 inside such fuselage 7 will show content to appear, at this moment can pass through operation key 3, liquid crystal display
Screen 6 model AOC AG332FCX, operated step by step according to the prompt inside liquid crystal display 6, when driver into
Row the television equipment viewing when may due to light refraction so that viewing it is ineffective, in this way can be by with one
Hand pinches fuselage 7, and the fuselage 7 can moving by front and back, can be under the action of rotation axis 1, so that fuselage 7 can be with
The adjustment that angle is preferably carried out under the action of the first support base 52 inside dorsal plate 5 and the second support base 53, passes through two
The setting of a first support base 52 and the second support base 53 can make in this way in the first support base 52 and the second support base 53
It preferably works under the action of support, and the left side of the one end of fixed link 13 far from limited block 14 inside rotation axis 1
The end point at right both ends is provided with threaded post, and is internally provided with thread groove 114 in fixed lid 11, can make in this way
It can be connected by screw thread rotation between fixed link 13 and fixed lid 11, and be provided between fixed lid 11 and fixed link 13
Attachment spacers 12 is internally provided with sliding slot 113 close to fixed link 13 in fixed lid 11, and attachment spacers 12 is close to sliding slot 113
One end is provided with the convex block 121 connecting with sliding slot 113, can make when being rotated in this way, and attachment spacers 12 is in rotation
When fixed lid 11 will not be made to rotate by convex block 121, sliding slot 113 is the torus structure of inner hollow, sliding slot 113
Maximum diameter of section be five centimetres, the smallest diameter of section of sliding slot 113 is 4 points 5 centimetres, in convex block 121 and inside
The maximum diameter of section of empty torus structure, convex block 121 is 4 points 9 centimetres, and the smallest diameter of section of convex block 121 is
4 points 4 centimetres, convex block 121 can be allowed preferably to be socketed with sliding slot 113 in this way and connect, fixed lid can be made in this way
11 will not rotate between fixed link 13, so that can connect more between fixed lid 11 and fixed link 13
It is close, can make in this way viewing better effect turn off the power switch 2 after use finishes.
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 (10)
1. a kind of general-purpose aircraft TV convenient for adjusting, including dorsal plate (5) and fuselage (7), it is characterised in that: the fuselage
(7) the table end of rear side is provided with dorsal plate (5), and the dorsal plate (5) is connected by screw to the table in the rear side of fuselage (7)
End, the dorsal plate (5) are fixedly connected with fuselage (7) by screw, are arranged at the axle center of the table side of the front end of the fuselage (7)
There is the liquid crystal display (6) of a cuboid, the liquid crystal display (6) passes through the table of front end of the bonding connection in fuselage (7)
At the side axle heart, by bonding connection, the lower end of the fuselage (7) is provided with bottom plate for the fuselage (7) and liquid crystal display (6)
(4), the fuselage (7) is connected to the table side of the upper end of bottom plate (4) by socket, and the fuselage (7) and bottom plate (4) pass through socket
It connects, the surface of the upside at the axle center of the bottom plate (4) is provided with operation key (3), institute close to the side of liquid crystal display (6)
State the surface that operation key (3) are connected to the upper end of the bottom plate (4) close to the side of liquid crystal display (6) by being socketed, the behaviour
Make key (3) and bottom plate (4) to connect by socket, is provided with power switch at the axle center of the upper end of the inside of the operation key (3)
(2), at the center for the inside that the power switch (2) is connected to operation key (3), the power switch (2) passes through with bottom plate (4)
Socket connection, the table side of the lower end of the bottom plate (4) are provided with rotation axis (1), and the rotation axis (1) is connected to bottom by socket
The table side of the lower end of plate (4), the rotation axis (1) and bottom plate (4) pass through socket connection, the liquid crystal display (6) and power supply
It switchs (2) to be electrically connected, the operation key (3) and power switch (2) are electrically connected.
2. a kind of general-purpose aircraft TV convenient for adjusting according to claim 1, it is characterised in that: the rotation axis
(1) composition includes fixed lid (11), attachment spacers (12), fixed link (13) and limited block (14), the limited block (14)
Left and right ends be each provided with a fixed link (13), two fixed links (13) are respectively arranged far from the side of limited block (14)
There is an attachment spacers (12), two attachment spacers (12) are each provided with one far from the side of two fixed links (13)
A fixed lid (11), the rotation axis (1) pass through socket connection by fixed link (13) and fuselage (7).
3. a kind of general-purpose aircraft TV convenient for adjusting according to claim 2, it is characterised in that: the fixed lid
(11) composition includes end cap (111), main body (112), sliding slot (113) and thread groove (114), the right side of the end cap (111)
End be provided with main body (112), be provided with sliding slot (113) on the inside of the right end of the main body (112), the sliding slot (113) it is interior
Side is provided with thread groove (114), and the fixed lid (11) is connected by thread groove (114) and fixed link (13) by screw thread rotation
It connects.
4. a kind of general-purpose aircraft TV convenient for adjusting according to claim 2, it is characterised in that: the attachment spacers
(12) composition includes convex block (121), ontology (122), through-hole (123) and friction washer (124), the convex block (121)
Right end is provided with ontology (122), and the right end of the ontology (122) is provided with friction washer (124), the ontology (122) it is interior
A through-hole (123) is provided at the axle center of side, the attachment spacers (12) is by convex block (121) and fixed lid (11) by inserting
It connects in succession, the torus structure of the convex block (121) and inner hollow, the maximum diameter of section of the convex block (121) is four
Nine centimetres of point, the smallest diameter of section of the convex block (121) are 4 points 4 centimetres.
5. a kind of general-purpose aircraft TV convenient for adjusting according to claim 1, it is characterised in that: the dorsal plate
(5) composition includes terminals (51), the first support base (52), the second support base (53) and plate body (54), the plate body
(54) second support base (53), two second support bases (53) are each provided at left and right sides of the lower end of inside
Lower end be each provided with first support base (52), first support base (52) and the second support base (53) by set in succession
Connect, the table side of the lower end of the inside of the plate body (54) is provided with terminals (51), the dorsal plate (5) by plate body (54) with
Fuselage (7) is fixedly connected by screw.
6. a kind of general-purpose aircraft TV convenient for adjusting according to claim 5, it is characterised in that: first support
Seat (52) and the second support base (53) are the prismatoid structure of plate, and first support base (52) and the second support base (53) are altogether
There are two settings, and two first support bases (52) and the second support base (53) are set in qually spaced in plate body in symmetrical respectively
(54) left and right sides at table end, two first support bases (52) and the second support base (53) pass through socket connection.
7. a kind of general-purpose aircraft TV convenient for adjusting according to claim 2, it is characterised in that: the fixed link
It (13) is cylindrical structure, the fixed link (13) is provided with two altogether, and two fixed links (13) are respectively between symmetrical wait
Table side away from setting in the left and right ends of limited block (14), the length of two fixed links (13) be six centimetres, two
The end point of the one end of the fixed link (13) far from limited block (14) is each provided with the cylindrical structure of a threaded circle, and two
The diameter of section of a fixed link (13) is three centimetres.
8. a kind of general-purpose aircraft TV convenient for adjusting according to claim 4, it is characterised in that: the ontology
It (122) is the torus structure of inner hollow, the diameter of section of the outer circle of the ontology (122) is four centimetres, the ontology
(122) be internally provided with through-hole (123), the diameter of section of the through-hole (123) are three centimetres, and the ontology (122) sets altogether
There are two setting, two ontologies (122) are respectively in the close limit for the fixed lid (11) for being symmetrically set in qually spaced in two sides
The inside of position block (14).
9. a kind of general-purpose aircraft TV convenient for adjusting according to claim 1, it is characterised in that: the liquid crystal display
Shield the structure that (6) are cuboid, the length of the liquid crystal display (6) is ten centimetres, and the width of the liquid crystal display (6) is
Eight centimetres, the wall thickness of the liquid crystal display (6) is eight millimeters, and the liquid crystal display (6) electrically connects with power switch (2)
It connects.
10. a kind of general-purpose aircraft TV convenient for adjusting according to claim 3, it is characterised in that: the sliding slot
It (113) is the torus structure of inner hollow, the maximum diameter of section of the sliding slot (113) is five centimetres, the sliding slot
(113) the smallest diameter of section is 4 points 5 centimetres.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910504951.5A CN110290337B (en) | 2019-06-12 | 2019-06-12 | Universal television convenient to adjust for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910504951.5A CN110290337B (en) | 2019-06-12 | 2019-06-12 | Universal television convenient to adjust for aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110290337A true CN110290337A (en) | 2019-09-27 |
| CN110290337B CN110290337B (en) | 2021-07-16 |
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ID=68003786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910504951.5A Active CN110290337B (en) | 2019-06-12 | 2019-06-12 | Universal television convenient to adjust for aircraft |
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| Country | Link |
|---|---|
| CN (1) | CN110290337B (en) |
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| CN110290337B (en) | 2021-07-16 |
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