CN110290337B - Universal television convenient to adjust for aircraft - Google Patents
Universal television convenient to adjust for aircraft Download PDFInfo
- Publication number
- CN110290337B CN110290337B CN201910504951.5A CN201910504951A CN110290337B CN 110290337 B CN110290337 B CN 110290337B CN 201910504951 A CN201910504951 A CN 201910504951A CN 110290337 B CN110290337 B CN 110290337B
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- supporting seat
- liquid crystal
- crystal display
- bottom plate
- fuselage
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- 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
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- 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
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- Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Devices For Indicating Variable Information By Combining Individual Elements (AREA)
Abstract
The invention discloses a universal television for an aircraft, which is convenient to adjust and comprises a back side plate and an aircraft body, wherein the surface end of the rear side of the aircraft body is provided with the back side plate, the back side plate is connected with the surface end of the rear side of the machine body through a screw, the back side plate is fixedly connected with the machine body through a screw, the front end of the machine body is provided with a rectangular liquid crystal display screen at the axis of the surface side, the invention adopts the structure that a fixed cover and a connecting gasket are arranged inside a rotating shaft in the equipment, this allows a better rotation under the action of the fixed cover and the connection pad, which allows the service life of the device to be increased and the operation to be simpler, and the end of the fixed rod, which is far away from the end of the limiting block, is provided with the threaded column, so that the fixed cover cannot rotate with the fixed rod, and the fixed cover can be connected with the fixed rod more closely.
Description
Technical Field
The invention belongs to the technical field of aerospace and aviation, and particularly relates to a universal television for an aircraft, which is convenient to adjust.
Background
The airplane display equipment is equipment for providing comprehensive monitoring and cockpit display control system with optimized situational awareness for pilots, and reduces the number of accidents of civil aviation. Improvements in avionics equipment and cockpit human-machine interfaces are necessary.
The prior television technology for the general airplane has the following problems: the display screen is usually fixed when the existing universal aircraft television displays, so that the position of the display screen needs to be adjusted before installation, and the display screen can be observed clearly under the action of light when a driver uses the television, so that the display screen is inconvenient to use, some display screens can rotate, but the friction force between the display screens can be reduced under frequent rotation, and the phenomenon of falling caused by insufficient friction force can occur in the rotation after a long time.
Disclosure of Invention
The invention aims to provide a universal television for an airplane, which is convenient to adjust, and aims to solve the problems that the existing television for the universal airplane in the background art is usually fixedly installed, and the poor rotating effect can be caused due to the reduction of friction force under the condition that the television can rotate for a plurality of times for a long time.
In order to achieve the purpose, the invention provides the following technical scheme: a television convenient to adjust for a general airplane comprises a back side plate and a body, wherein the back side plate is arranged at the surface end of the rear side of the body, the back side plate is connected at the surface end of the rear side of the body through screws, the back side plate is fixedly connected with the body through screws, a liquid crystal display screen of a rectangular body is arranged at the axis center of the surface side of the front end of the body, the liquid crystal display screen is connected at the axis center of the surface side of the front end of the body through bonding, the body is connected with the liquid crystal display screen through bonding, a bottom plate is arranged at the lower end of the body, the body is connected at the surface side of the upper end of the bottom plate through sleeving, the body is connected with the bottom plate through sleeving, an operation key is arranged at one side of the upper side of the axis center of the bottom plate, the operation key is connected at the surface of, the utility model discloses a bottom plate, including operating key, bottom plate, axis, switch, power switch, bottom plate, liquid crystal display, switch, bottom plate, operating key and bottom plate are connected through cup jointing, the axle center department of the upper end of the inside of operating key is provided with switch, switch connects the center department at the inboard of operating key, switch is connected through cup jointing with the bottom plate, the table side of the lower extreme of bottom plate is provided with the axis of rotation, the axis of rotation is through cup jointing the table side of connecting at the lower extreme of bottom plate, the axis of rotation is connected through cup jointing with the bottom plate, liquid crystal.
Preferably, the constitution of axis of rotation is including fixed lid, connection gasket, dead lever and stopper, both ends respectively are provided with a dead lever about the stopper, two one side that the stopper was kept away from to the dead lever respectively is provided with a connection gasket, two it keeps away from two to connect the gasket one side of dead lever respectively is provided with a fixed lid, the axis of rotation passes through the dead lever and is connected through cup jointing with the fuselage.
Preferably, the fixed cover comprises an end cover, a main body, a sliding groove and a thread groove, the main body is arranged at the right end of the end cover, the sliding groove is arranged on the inner side of the right end of the main body, the thread groove is arranged on the inner side of the sliding groove, and the fixed cover is rotatably connected with the fixed rod through the thread groove.
Preferably, the connection gasket comprises a convex block, a body, a through hole and a friction washer, the body is arranged at the right end of the convex block, the friction washer is arranged at the right end of the body, the through hole is formed in the axis of the inner side of the body, and the connection gasket is connected with the fixed cover through the convex block in an inserting mode.
Preferably, the constitution of dorsal scale board is including wiring end, first supporting seat, second supporting seat and plate body, the left and right sides of the inboard lower extreme of plate body respectively is provided with a second supporting seat, two the lower extreme of second supporting seat respectively is provided with a first supporting seat, first supporting seat is connected through cup jointing with the second supporting seat, the table side of the lower extreme of the inside of plate body is provided with the wiring end, the dorsal scale board passes through the plate body and passes through screw fixed connection with the fuselage.
Preferably, first supporting seat and second supporting seat are platelike trapezoidal body structure, first supporting seat and second supporting seat are provided with two altogether first supporting seat and second supporting seat are the equidistant left and right sides that sets up at the table end of plate body, two respectively of symmetry with the second supporting seat first supporting seat is connected through cup jointing with the second supporting seat.
Preferably, the dead lever is the cylinder structure, the dead lever is provided with two altogether, two the dead lever is the table side of symmetry equidistant setting at the left and right sides both ends of stopper respectively, two the length of dead lever is for being six centimetres, two the end department that the dead lever kept away from the one end of stopper respectively is provided with a cylinder structure of taking the thread circle, two the cross-sectional diameter of dead lever is three centimetres.
Preferably, the body is the hollow tourus structure in inside, the cross-sectional diameter of the excircle of body is four centimetres, the inside of body is provided with the through-hole, the cross-sectional diameter of through-hole is three centimetres, the body is provided with two altogether, two the body is the equidistant setting in both sides of symmetry respectively the inboard that is close to the stopper of fixed lid.
Preferably, the liquid crystal display is of a rectangular structure, the length of the liquid crystal display is ten centimeters, the width of the liquid crystal display is eight centimeters, the wall thickness of the liquid crystal display is eight millimeters, and the liquid crystal display is electrically connected with the power switch.
Preferably, the sliding groove is of a hollow annular structure, the largest cross-sectional diameter of the sliding groove is five centimeters, and the smallest cross-sectional diameter of the sliding groove is four-point five centimeters.
Preferably, the bump is of a ring body structure with a hollow inner part, the largest cross-sectional diameter of the bump is four-point nine centimeters, and the smallest cross-sectional diameter of the bump is four-point four centimeters
Compared with the prior art, the invention provides the universal television for the airplane, which is convenient to adjust and has the following beneficial effects:
(1) according to the invention, the combined structure of the fixed cover and the connecting gasket is arranged in the rotating shaft of the equipment, so that the machine body sleeved in the upper end of the bottom plate can better rotate under the action of the fixed cover and the connecting gasket, the problem of reduction of friction force due to long-time rotation is avoided, the service life of the equipment is prolonged, and the operation is simpler;
(2) according to the invention, the threaded column is arranged at the end of one end of the fixed rod, which is far away from the limiting block, and the threaded groove is arranged in the fixed cover, so that the fixed rod can be rotatably connected with the fixed cover through threads, the connecting gasket is arranged between the fixed cover and the fixed rod, the sliding groove is arranged in the fixed cover, which is close to the fixed rod, and the convex block connected with the sliding groove is arranged at one end of the connecting gasket, which is close to the sliding groove Poor rotating effect.
Drawings
Fig. 1 is a schematic diagram of a general-purpose television for an aircraft according to the present invention;
FIG. 2 is a schematic view of a rotating shaft according to the present invention;
FIG. 3 is a schematic view of the fixing cover structure of the present invention;
FIG. 4 is a schematic view of a connection pad of the present invention;
FIG. 5 is a schematic view of the backside plate of the present invention;
in the figure: 1. a rotating shaft; 11. a fixed cover; 111. an end cap; 112. a main body; 113. a chute; 114. a thread groove; 12. connecting a gasket; 121. a bump; 122. a body; 123. a through hole; 124. a friction washer; 13. fixing the rod; 14. a limiting block; 2. a power switch; 3. an operation key; 4. a base plate; 5. a back side plate; 51. a terminal; 52. a first support base; 53. a second support seat; 54. a plate body; 6. a liquid crystal display screen; 7. a fuselage.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a convenient-to-adjust television for a general airplane comprises a back side plate 5 and a body 7, wherein the back side plate 5 is arranged at the surface end of the rear side of the body 7, the back side plate 5 comprises a wiring terminal 51, a first supporting seat 52, a second supporting seat 53 and a plate body 54, the left side and the right side of the lower end of the inner side of the plate body 54 are respectively provided with one second supporting seat 53, the lower ends of the two second supporting seats 53 are respectively provided with one first supporting seat 52, the first supporting seat 52 is connected with the second supporting seat 53 in a sleeved mode, the first supporting seat 52 and the second supporting seat 53 are of a plate-shaped trapezoid structure, the first supporting seat 52 and the second supporting seat 53 are arranged in two numbers, the two first supporting seats 52 and the second supporting seat 53 are arranged on the left side and the right side of the surface end of the plate body 54 in a symmetrical and equidistant mode through the arrangement of the two first supporting seats 52 and the second supporting seat 53, the two first supporting seats 52 are connected with the second supporting seat 53 in a sleeved mode, the wiring end 51 is arranged on the surface side of the lower end of the inner portion of the plate body 54, the wiring end 51 is arranged, so that power wiring can be connected better under the action of the wiring end 51, and better work can be achieved, the dorsal plate 5 is fixedly connected with the machine body 7 through the plate body 54 through screws, the dorsal plate 5 is connected to the surface end of the rear side of the machine body 7 through screws, the dorsal plate 5 is fixedly connected with the machine body 7 through screws,
a convenient-to-adjust television for a general airplane comprises a rectangular liquid crystal display screen 6 arranged at the axis of the front surface side of a body 7, the liquid crystal display screen 6 is of a rectangular structure, the length of the liquid crystal display screen 6 is ten centimeters, the width of the liquid crystal display screen 6 is eight centimeters, so that the liquid crystal display screen 6 can have a better watching effect, the wall thickness of the liquid crystal display screen 6 is eight millimeters, the liquid crystal display screen 6 is electrically connected with a power switch 2, the liquid crystal display screen 6 is connected at the axis of the front surface side of the body 7 through bonding, the body 7 is connected with the liquid crystal display screen 6 through bonding, a bottom plate 4 is arranged at the lower end of the body 7, the body 7 is connected at the upper end of the bottom plate 4 through sleeving, the body 7 is connected with the bottom plate 4 through sleeving, an operating key 3 is arranged at one side, close to the liquid crystal display screen 6, of the, the operation key 3 is connected on the surface of the upper end of the bottom plate 4 on one side close to the liquid crystal display screen 6 through a sleeve, the operation key 3 is connected with the bottom plate 4 through a sleeve, a power switch 2 is arranged at the axis of the upper end inside the operation key 3, the power switch 2 is connected at the center of the inner side of the operation key 3, the power switch 2 is connected with the bottom plate 4 through a sleeve, a rotating shaft 1 is arranged on the surface side of the lower end of the bottom plate 4, the rotating shaft 1 comprises a fixed cover 11, a connecting gasket 12, a fixed rod 13 and a limited block 14, the left end and the right end of the limited block 14 are respectively provided with a fixed rod 13, one side of each fixed rod 13 far away from the limited block 14 is respectively provided with a connecting gasket 12, and the connecting gasket 12 is arranged, so that under the action of the connecting gasket 12, a better rotating effect can be achieved,
a convenient-to-adjust universal television for an airplane comprises two connecting gaskets 12, wherein one side of each connecting gasket 12, which is far away from two fixing rods 13, is provided with a fixing cover 11, the connecting gaskets 12 comprise a convex block 121, a body 122, a through hole 123 and a friction gasket 124, the right end of the convex block 121 is provided with the body 122, the body 122 is of a hollow circular ring structure, the section diameter of the excircle of the body 122 is four centimeters, the inside of the body 122 is provided with the through hole 123, so that the section diameter of the through hole 123 is the same as that of the fixing rods 13, better sleeving effect can be achieved, the section diameter of the through hole 123 is three centimeters, the two bodies 122 are arranged, the two bodies 122 are symmetrically arranged on the inner sides, close to a limiting block 14, of the fixing covers 11 on the two sides at equal intervals, the right end of the body 122 is provided with the friction gasket 124, thus, the connecting gasket 12 can be better contacted with the friction washer 124 when rotating, so that the connecting gasket can not fall down when rotating to a proper position, a through hole 123 is arranged at the axis of the inner side of the body 122, the connecting gasket 12 is in plug connection with the fixed cover 11 through the bump 121, the fixed cover 11 comprises an end cover 111, a main body 112, a sliding chute 113 and a thread groove 114, the right end of the end cover 111 is provided with the main body 112, the inner side of the right end of the main body 112 is provided with the sliding chute 113, the sliding chute 113 is of a hollow annular structure, the largest cross-sectional diameter of the sliding chute 113 is five centimeters, the smallest cross-sectional diameter of the sliding chute 113 is four-five centimeters, the bump 121 is of a hollow annular structure, the largest cross-sectional diameter of the bump 121 is four-nine centimeters, the smallest cross-sectional diameter of the bump 121 is four-four centimeters, through the arrangement of the, therefore, the convex block 121 can be better sleeved and connected with the sliding chute 113, the inner side of the sliding chute 113 is provided with a thread groove 114, the fixed cover 11 is rotatably connected with the fixed rod 13 through the thread groove 114,
the utility model provides a general TV for aircraft convenient to adjust, including axis of rotation 1 through dead lever 13 with fuselage 7 through cup jointing and be connected, dead lever 13 is the cylinder structure, dead lever 13 is provided with two altogether, two dead levers 13 are the equidistant table side that sets up both ends about stopper 14 respectively, setting through two dead levers 13, so can be so that better carry out work, the length of two dead levers 13 is for being six centimetres, the end department of the one end that stopper 14 was kept away from to two dead levers 13 respectively is provided with the cylinder structure of a threaded circle, the cross-sectional diameter of two dead levers 13 is three centimetres, axis of rotation 1 is through cup jointing the table side of connecting the lower extreme at bottom plate 4, axis of rotation 1 is connected through cup jointing with bottom plate 4, liquid crystal display 6 and 2 electric connection of switch, manipulating key 3 and 2 electric connection of switch.
The working principle and the using process of the invention are as follows: after the invention is installed, firstly checking whether the machine can work normally, checking whether the plug and the socket on the electric wire are connected completely, if abnormal noise occurs, closing the machine immediately, waiting for maintenance of professionals, when the television of the general-purpose airplane is used, firstly taking out the television equipment, taking out the packaging box, placing the tool to be used at one side of the television equipment, and when all the tools are ready, the television equipment and the part to be installed of the general-purpose airplane are stably installed by the common tool, then the power switch 2 is pressed down, so that the liquid crystal display screen 6 in the body 7 can display the content to be appeared, at this time, the operation key 3 can be used, the model of the liquid crystal display 6 is AOC AG332FCX, the operation is performed step by step according to the prompt inside the liquid crystal display 6, when the driver watches the television, the watching effect may be not good due to the refraction of light, so that the body 7 can be held by one hand, and the body 7 can be moved back and forth by snapping, under the action of the rotating shaft 1, the body 7 can be better adjusted in angle under the action of the first supporting seat 52 and the second supporting seat 53 inside the back side plate 5, by the arrangement of the two first supporting seats 52 and the second supporting seat 53, the body can be better operated under the support action of the first supporting seat 52 and the second supporting seat 53, and the threaded columns are arranged at the left and right ends of one end of the fixing rod 13 inside the rotating shaft 1 far from the limiting block 14, and the threaded groove 114 is arranged inside the fixing cover 11, therefore, the fixed rod 13 and the fixed cover 11 can be rotatably connected through threads, the connecting gasket 12 is arranged between the fixed cover 11 and the fixed rod 13, the sliding groove 113 is arranged in the fixed cover 11 close to the fixed rod 13, the protruding block 121 connected with the sliding groove 113 is arranged at one end of the connecting gasket 12 close to the sliding groove 113, so that when the fixed cover 11 rotates, the connecting gasket 12 cannot enable the fixed cover 11 to rotate through the protruding block 121 when the fixed cover 11 rotates, the sliding groove 113 is of an internally hollow annular structure, the largest cross-sectional diameter of the sliding groove 113 is five centimeters, the smallest cross-sectional diameter of the sliding groove 113 is four-point five centimeters, the protruding block 121 is of an internally hollow annular structure, the largest cross-sectional diameter of the protruding block 121 is four-point nine centimeters, the smallest cross-sectional diameter of the protruding block 121 is four-point four centimeters, and thus the protruding block 121 and the sliding groove 113 can, therefore, the fixed cover 11 can not rotate relative to the fixed rod 13, so that the fixed cover 11 can be connected with the fixed rod 13 more tightly, the watching effect is better, and after the fixed cover is used, the power switch 2 is turned off.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a general TV for aircraft convenient to adjust, includes dorsal scale board (5) and fuselage (7), its characterized in that: the table end of the rear side of fuselage (7) is provided with dorsal plate (5), dorsal plate (5) passes through the table end of screw connection at the rear side of fuselage (7), dorsal plate (5) and fuselage (7) pass through screw fixed connection, the axle center department of the table side of the front end of fuselage (7) is provided with liquid crystal display (6) of a cuboid, liquid crystal display (6) pass through bonding connection in the table side axle center department of the front end of fuselage (7), fuselage (7) and liquid crystal display (6) pass through bonding connection, the lower extreme of fuselage (7) is provided with bottom plate (4), fuselage (7) passes through the table side of cup jointing connection in the upper end of bottom plate (4), fuselage (7) and bottom plate (4) are through cup jointing connection, the surface of the upside of the axle center department of bottom plate (4) is provided with operating key (3) near one side of liquid crystal display (6), operation key (3) are connected on the surface of the upper end of bottom plate (4) of the one side that is close to liquid crystal display (6) through cup jointing, operation key (3) are connected through cup jointing with bottom plate (4), the axle center department of the upper end of the inside of operation key (3) is provided with switch (2), switch (2) are connected in the inboard center department of operation key (3), switch (2) are connected through cup jointing with bottom plate (4), the table side of the lower extreme of bottom plate (4) is provided with axis of rotation (1), axis of rotation (1) is connected in the table side of the lower extreme of bottom plate (4) through cup jointing, axis of rotation (1) is connected through cup jointing with bottom plate (4), liquid crystal display (6) and switch (2) electric connection, operation key (3) and switch (2) electric connection, the constitution of axis of rotation (1) is including fixed cover (11), The fixing device comprises connecting gaskets (12), fixing rods (13) and limiting blocks (14), wherein the left end and the right end of each limiting block (14) are respectively provided with one fixing rod (13), one side, away from the limiting blocks (14), of each two fixing rods (13) is respectively provided with one connecting gasket (12), one side, away from each two fixing rods (13), of each two connecting gaskets (12) is respectively provided with one fixing cover (11), the rotating shaft (1) is connected with a machine body (7) through the fixing rods (13) in a sleeved mode, each fixing cover (11) comprises an end cover (111), a main body (112), a sliding groove (113) and a thread groove (114), the right end of the end cover (111) is provided with a main body (112), the inner side of the right end of the main body (112) is provided with a sliding groove (113), the sliding groove (113) is of a circular ring body structure with a hollow interior, and the, the fixed cover (11) is rotationally connected with the fixed rod (13) through a thread groove (114), the connecting gasket (12) comprises a convex block (121), a body (122), a through hole (123) and a friction gasket (124), the body (122) is arranged at the right end of the convex block (121), the friction gasket (124) is arranged at the right end of the body (122), the through hole (123) is arranged at the axis of the inner side of the body (122), the connecting gasket (12) is connected with the fixed cover (11) through the convex block (121) in an inserting manner, the back side plate (5) comprises a wiring end (51), a first supporting seat (52), a second supporting seat (53) and a plate body (54), the left side and the right side of the lower end of the inner side of the plate body (54) are respectively provided with a second supporting seat (53), and the lower ends of the two second supporting seats (53) are respectively provided with a first supporting seat (52), first supporting seat (52) are connected through cup jointing with second supporting seat (53), the table side of the lower extreme of the inside of plate body (54) is provided with wiring end (51), dorsal scale board (5) pass through plate body (54) and fuselage (7) through screw fixed connection, first supporting seat (52) are platelike trapezoidal body structure with second supporting seat (53), first supporting seat (52) are provided with two, two with second supporting seat (53) first supporting seat (52) are the left and right sides of equidistant setting in the table end of plate body (54) respectively with second supporting seat (53), two first supporting seat (52) are connected through cup jointing with second supporting seat (53).
2. A universal aircraft television set for easy adjustment according to claim 1, wherein: dead lever (13) are the cylinder structure, dead lever (13) are provided with two altogether, two dead lever (13) are the table side of symmetry equidistant setting at the left and right sides both ends of stopper (14) respectively, two the length of dead lever (13) is six centimetres, two dead lever (13) are kept away from the end of the one end of stopper (14) and are respectively provided with a cylinder structure of taking the whorl circle, two the cross-sectional diameter of dead lever (13) is three centimetres.
3. A universal aircraft television set for easy adjustment according to claim 1, wherein: the body (122) is a hollow annular ring structure, the section diameter of the excircle of the body (122) is four centimeters, a through hole (123) is formed in the body (122), the section diameter of the through hole (123) is three centimeters, the body (122) is provided with two bodies, and the two bodies (122) are respectively symmetrically arranged on two sides of the fixed cover (11) at equal intervals and are close to the inner side of the limiting block (14).
4. A universal aircraft television set for easy adjustment according to claim 1, wherein: liquid crystal display (6) are the structure of cuboid, the length of liquid crystal display (6) is ten centimetres, the width of liquid crystal display (6) is eight centimetres, the wall thickness of liquid crystal display (6) is eight millimetres, liquid crystal display (6) and switch (2) electric connection.
5. A universal aircraft television set for easy adjustment according to claim 1, wherein: the largest cross-sectional diameter of the sliding groove (113) is five centimeters, and the smallest cross-sectional diameter of the sliding groove (113) is four-point five centimeters.
6. A universal aircraft television set for easy adjustment according to claim 1, wherein: the bump (121) is of a hollow annular ring structure, the largest cross-sectional diameter of the bump (121) is four-point nine centimeters, and the smallest cross-sectional diameter of the bump (121) is four-point four centimeters.
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 |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910504951.5A CN110290337B (en) | 2019-06-12 | 2019-06-12 | Universal television convenient to adjust for aircraft |
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| CN110290337A CN110290337A (en) | 2019-09-27 |
| CN110290337B true CN110290337B (en) | 2021-07-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910504951.5A Active CN110290337B (en) | 2019-06-12 | 2019-06-12 | Universal television convenient to adjust for aircraft |
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| CN108930471B (en) * | 2018-05-28 | 2020-06-26 | 东莞市轩达精密五金科技有限公司 | A multifunctional door hinge |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201628877U (en) * | 2010-01-08 | 2010-11-10 | 东莞市恒星光电科技有限公司 | Computer and television integrated machine |
| CN203559677U (en) * | 2013-10-18 | 2014-04-23 | 黎俊文 | Roller switching mechanism used on automatic reset hinge |
| CN204511126U (en) * | 2015-03-26 | 2015-07-29 | 杭州广义装饰工程有限公司 | A kind of spring hinge |
Also Published As
| Publication number | Publication date |
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| CN110290337A (en) | 2019-09-27 |
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