CN113028207A - Novel quick-release display fixing structure for aviation simulator - Google Patents
Novel quick-release display fixing structure for aviation simulator Download PDFInfo
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- CN113028207A CN113028207A CN202110219734.9A CN202110219734A CN113028207A CN 113028207 A CN113028207 A CN 113028207A CN 202110219734 A CN202110219734 A CN 202110219734A CN 113028207 A CN113028207 A CN 113028207A
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- display
- quick
- release
- simulator
- handle
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- 238000000034 method Methods 0.000 claims abstract description 19
- 238000010030 laminating Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/041—Allowing quick release of the apparatus
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/005—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles integral with the apparatus or articles to be supported
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Devices For Indicating Variable Information By Combining Individual Elements (AREA)
Abstract
The invention belongs to the technical field of aviation simulators, and particularly relates to a novel quick-release display fixing structure for an aviation simulator. The novel quick-release display fixing structure for the aviation simulator comprises a display arranged in a frame of the display, and also comprises at least 2 display quick-release handles which are arranged in a central symmetry manner; a simulator display frame is arranged on the simulator cabin plate, and the display is clamped in the simulator display frame through a display frame; a locking pin is arranged on the side wall of the display frame of the simulator and corresponds to the arc-shaped convex nozzle structure on the display quick-release handle, and an ejection block is arranged below the locking pin. In the process of opening and closing the display quick-release handle, the ejection block plays a supporting role as a fulcrum, so that the display can be ejected out to realize quick detachment, and the use is more convenient.
Description
Technical Field
The invention belongs to the technical field of aviation simulators, and particularly relates to a novel quick-release display fixing structure for an aviation simulator.
Background
The existing display for the aviation simulator has large volume and heavy weight. When the display is installed, the display is fixed with the engine room through screws, and the display body has a considerable weight in the dismounting process. The display is embedded on the simulator after being installed, the display is basically parallel to the surface of the simulator after being installed, the display is easy to install, and the display cannot be taken out due to the action of gravity and no protruding dismounting port when being dismounted. The quick-release display fixing structure in the prior art has no structure capable of realizing quick release, and instrument parts can be damaged by tools such as crowbars.
Disclosure of Invention
The invention provides a novel quick-release display fixing structure for an aviation simulator, which solves the technical problems that the existing quick-release display fixing structure is inconvenient to disassemble and the display cannot be disassembled quickly.
In order to achieve the purpose, the invention has the specific technical scheme that the novel quick-release display fixing structure for the aviation simulator comprises at least 2 display quick-release handles which are arranged in central symmetry; the display quick-release handle is connected with the display frame through a rotating shaft; the quick-release handle of the display comprises a horizontal handle part and a W-shaped release part which are integrally arranged, the outer side end of the W-shaped release part is of an arc-shaped convex nozzle structure which is bent upwards, and the arc-shaped part of the arc-shaped convex nozzle structure is provided with a fixing groove; a rotating shaft is fixedly arranged on the middle bulge of the W-shaped dismounting part; the outer side end of the horizontal handle part is provided with a sliding chute, a sliding block is arranged in the sliding chute, and the bottom of the sliding block is provided with a clamping screw; one side of the bottom of the sliding chute is connected with one end of a limiting spring, and the other end of the limiting spring abuts against the side face of the sliding block; the simulator cabin plate is provided with a display quick-release handle clamping groove, the bottom of the display quick-release handle clamping groove is provided with a clamping groove corresponding to the sliding block and the clamping screw, and a clamping boss is arranged in the clamping groove; the bottom nut of the clamping screw can be clamped into the bottom of the clamping boss to realize clamping; a simulator display frame is arranged on the simulator cabin plate, and the display is clamped in the simulator display frame through a display frame; a locking pin is arranged on the side wall of the display frame of the simulator and corresponds to the arc-shaped convex nozzle structure on the display quick-release handle, and an ejection block is arranged below the locking pin.
Furthermore, when the horizontal handle part of the display quick-release handle is kept parallel to the display, the height of the outer surface of the horizontal handle part is consistent with that of the outer surface of the display frame.
Furthermore, the inner side end of the horizontal handle part of the display quick-release handle is a convex inclined surface, and the surface of the frame of the display, which is combined with the inner side end of the display quick-release handle, is also an inclined surface, and the inclined angles of the inclined surfaces are consistent.
Further, the quick detach handle of display is 2 and sets up the diagonal position at the display.
Further, the display quick-release handles are 4 and are arranged at 4 corners of the display.
Furthermore, the display quick-release handle is in an open state, the end of the arc-shaped convex nozzle structure is positioned on one side of the clamping groove relative to the locking pin, and the rotating shaft is positioned on the upper side of the locking pin; the display quick-release handle is in a closed state, and the end head of the arc-shaped convex nozzle structure is positioned on the other side of the clamping groove relative to the locking pin; in the process of opening and closing the display quick-release handle, the ejection block serves as a fulcrum to play a supporting role.
Further, the length of the ejector block is greater than the diameter of the locking pin.
Further, the distance between the ejection block and the locking pin is larger than the height of the arc-shaped convex nozzle structure.
Furthermore, the bottom of the clamping screw is of an arc-shaped structure protruding downwards.
Compared with the prior art, the technical scheme of the invention has the beneficial effects that: after the quick-release display fixing structure is locked, the quick-release display fixing structure can be still quickly detached under the condition that the quick-release display fixing structure and the display frame are located on the same plane. In the working and disassembling process, the horizontal handle part of the display quick-disassembling handle rotates upwards, the W-shaped disassembling part also rotates around the rotating shaft, and the arc-shaped convex mouth structure of the W-shaped disassembling part moves downwards and then abuts against the ejection block, so that a crow bar structure which surrounds the rotating shaft and takes the ejection block as a fulcrum is formed; when the display quick-release handle is completely opened, the end head of the arc-shaped convex nozzle structure is positioned on one side of the clamping groove relative to the locking pin, and the rotating shaft is positioned on the upper side of the locking pin; the display quick-release handle is in a closed state, and the end head of the arc-shaped convex nozzle structure is positioned on the other side of the clamping groove relative to the locking pin; in the process of opening and closing the display quick-release handle, the ejection block plays a supporting role as a fulcrum, so that the display can be ejected out to realize quick detachment, and the use is more convenient.
Drawings
Fig. 1 is a schematic perspective view of a fixing structure of a quick release display for the novel aviation simulator.
Fig. 2 is a vertical section view of the novel quick release display fixing structure for the aviation simulator when locked.
Fig. 3 is a vertical section view of the fixing structure of the quick-release display for the novel aviation simulator when the fixing structure is opened.
Fig. 4 is a schematic top view of a quick-release display fixing structure for the novel aviation simulator.
Fig. 5 is a structure view of the quick release handle of the display.
Description of reference numerals: 1. a simulator deck; 2. a display bezel; 3. a display; 4. the display quick-release handle; 4.1, a sliding block; 4.2, a limiting spring; 4.3, a chute; 4.4, a clamping screw; 4.5, a horizontal handle part; 4.6, a W-shaped detaching part; 4.7, fixing grooves; 4.8, an arc convex nozzle structure; 5. a clamping groove; 5.1, a clamping boss; 6. a locking pin; 7. a rotating shaft; 8. ejecting a block; 9. the display quick-release handle clamping groove; 10. the simulator displays a frame.
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 some, not all, embodiments of the present invention. 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.
The terms "first" and "second," and the like, in the description and in the claims of embodiments of the present invention are used for distinguishing between different objects and not for describing a particular order of the objects. For example, the first parameter set and the second parameter set, etc. are used to distinguish different parameter sets, rather than to describe a particular order of parameter sets.
In the description of the embodiments of the present invention, the meaning of "a plurality" means two or more unless otherwise specified. For example, a plurality of elements refers to two elements or more.
The term "and/or" herein is an association relationship describing an associated object, and means that there may be three relationships, for example, a display panel and/or a backlight, which may mean: there are three cases of a display panel alone, a display panel and a backlight at the same time, and a backlight alone. The symbol "/" herein denotes a relationship in which the associated object is or, for example, input/output denotes input or output.
In the embodiments of the present invention, words such as "exemplary" or "for example" are used to mean serving as examples, illustrations or descriptions. Any embodiment or design described as "exemplary" or "e.g.," an embodiment of the present invention is not necessarily to be construed as preferred or advantageous over other embodiments or designs. Rather, use of the word "exemplary" or "such as" is intended to present concepts related in a concrete fashion.
The existing display for the aviation simulator has large volume and heavy weight. The display is required to be basically parallel to the surface of the simulator after being installed, and meanwhile, the display is embedded on the simulator after being installed, so that the display is very inconvenient to disassemble. The tools such as a crow bar are used for dismounting, and instrument parts are easy to damage. In order to solve the problems, the invention provides a novel quick-release display fixing structure for an aviation simulator. In addition, a locking pin is arranged on the side wall of a simulator display frame of the simulator cabin plate and corresponds to the arc-shaped convex nozzle structure on the display quick-release handle, and an ejection block is arranged below the locking pin. When the display quick-release handle is completely opened, the end head of the arc-shaped convex nozzle structure is positioned on one side of the clamping groove relative to the locking pin, and the rotating shaft is positioned on the upper side of the locking pin; the display quick-release handle is in a closed state, and the end head of the arc-shaped convex nozzle structure is positioned on the other side of the clamping groove relative to the locking pin; the display quick detach handle is opened and is closed the in-process, and ejecting piece plays the supporting role as the fulcrum to the realization realizes dismantling fast display frame with the ejecting simulator display frame of display and display frame, and it is more convenient to use, has solved a bit because display weight is big, and peripheral inseparable technical problem who can't dismantle of laminating again with simulator display frame.
The working principle and the working process are as follows: in the installation, make display quick detach handle 4 be in the on-state, then put into simulator display frame 10 with display 3, then press the horizontal handle portion 4.5 of display quick detach handle 4 downwards, make it rotate around pivot 7, and then in rotating the fixed slot 4.7 and the laminating of locking round pin 6 on the arc protruding mouth structure 4.8 upper portion of in-process W shape dismantlement portion 4.6, and then in rotating the in-process, make locking round pin 6 card go into fixed slot 4.7, display quick detach handle 4 uses pivot 7 to form the crow bar structure for the pointing with the laminating point of fixed slot 4.7 and locking round pin 6 as the axle, realize the block of fixed slot 4.7 and locking round pin 6 after the rotation is accomplished. The display frame 2 applies downward pressure to the display 3, so that the display frame 2 is clamped with the clamping simulator display frame 10. When the display quick detach handle 4 got into display quick detach handle draw-in groove 9, slider 4.1 received the extrusion, then with spacing spring 4.2 cooperation, realized blocking 5.1 bottoms with the nut card of the screens screw 4.4 of slider 4.1 bottom, realization block. Simultaneously, the arc-shaped convex nozzle structure 4.8 of the W-shaped disassembling part 4.6 moves to the left side of the bottom of the locking pin 6, so that the locking pin 6 is clamped into the fixing groove 4.7 to realize clamping, and further, the complete locking of the display 3 is realized. In the disassembly process, the sliding block 4.1 is shifted in the opposite direction, then the horizontal handle part 4.5 of the display quick-disassembly handle 4 is pulled upwards, the display quick-disassembly handle 4 rotates around the rotating shaft 7 reversely, further the fixing groove 4.7 on the upper part of the arc-shaped convex nozzle structure 4.8 of the W-shaped disassembly part 4.6 rotates along with the rotation, when the arc-shaped convex nozzle structure 4.8 rotates to the left side position of the locking pin 6, the complete separation of the display quick-disassembly handle 4.8 and the locking pin 6 is realized, in addition, in the rotation process, the arc-shaped convex nozzle structure 4.8 supports against the ejection block 8, further the rotating shaft 7 is used as the rotating shaft, the ejection block 8 is used as a fulcrum, further, a prying bar relation is formed, the upward prying force of the display 3 is realized, finally, the quick-disassembly process of the display handle 4 is realized, meanwhile, an upward ejecting force is given to the. The disassembly is more convenient, the efficiency is higher, and the damage to the instrument and equipment is avoided.
Illustratively, the horizontal handle part 4.5 of the display quick release handle 4 has an outer surface height consistent with the outer surface height of the display frame 2 when keeping parallel with the display 3. The smoothness of the surface of the simulator is effectively guaranteed, and the simulation accuracy is improved.
Illustratively, the inner end of the horizontal handle part 4.5 of the display quick-release handle 4 is a convex 65 ° inclined plane, and the surface of the display frame 2 combined with the inner end of the display quick-release handle 4 is also a 65 ° inclined plane, and the two inclined planes are at the same angle. Thereby behind the locking, inseparabler combination can be realized to the two terminal surfaces, when satisfying the pivoted, better improvement simulator surface smoothness.
Illustratively, the display quick release handles 4 are 4 handles arranged at 4 corners of the display 3. Further improving the stability of equipment installation.
Illustratively, the length of the ejection block 8 is greater than the diameter of the locking pin 6, which effectively improves the service life, reduces the wear, and further improves the disassembly stability of the display 3.
Illustratively, the distance between the ejector block 8 and the locking pin 6 is greater than the height of the arcuate nose structure 4.8.
Exemplarily, the bottom of the clamping screw 4.4 is of an arc structure protruding downwards, so that clamping can be realized at the bottom of the clamping boss 5.1 in the locking process more conveniently.
After the quick-release display fixing structure is locked, the quick-release display fixing structure can be quickly detached under the condition that the quick-release display fixing structure and the frame 2 of the display can be kept in the same plane, in the working detachment process, the horizontal handle part 4.5 of the quick-release display handle 4 upwards rotates, the W-shaped detachment part 4.6 also rotates around the rotating shaft 7, the arc-shaped convex nozzle structure 4.8 of the W-shaped detachment part 4.6 downwards moves and then abuts against the ejection block 8, so that a crow bar structure which surrounds the rotating shaft 7 and takes the ejection block 8 as a fulcrum is formed, the display 3 is driven to integrally upwards move in the upward rotating process of the horizontal handle part 4.5 of the quick-release display handle 4, when the quick-release display handle 4 is completely opened, the end of the arc-shaped convex nozzle structure 4.8 is positioned on one side of the clamping groove 5 relative to the locking pin 6, and the rotating shaft 7 is positioned on the; the display quick-release handle 4 is in a closed state, and the end head of the arc-shaped convex nozzle structure 4.8 is positioned on the other side of the clamping groove 5 relative to the locking pin 6; in the process of opening and closing the display quick-release handle 4, the ejection block 8 plays a supporting role as a fulcrum, so that the display 3 is ejected out to realize quick detachment, and the use is more convenient.
While the present invention has been described with reference to the embodiments shown in the drawings, the present invention is not limited to the embodiments, which are illustrative and not restrictive, and it will be apparent to those skilled in the art that various changes and modifications can be made therein without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (9)
1. The utility model provides a novel aviation is quick-release display fixed knot constructs for simulator which characterized in that: the novel quick-release display fixing structure for the aviation simulator comprises at least 2 display quick-release handles which are arranged in a central symmetry manner; the display quick-release handle is connected with the display frame through a rotating shaft; the quick-release handle of the display comprises a horizontal handle part and a W-shaped release part which are integrally arranged, the outer side end of the W-shaped release part is of an arc-shaped convex nozzle structure which is bent upwards, and the arc-shaped part of the arc-shaped convex nozzle structure is provided with a fixing groove; a rotating shaft is fixedly arranged on the middle bulge of the W-shaped dismounting part; the outer side end of the horizontal handle part is provided with a sliding chute, a sliding block is arranged in the sliding chute, and the bottom of the sliding block is provided with a clamping screw; one side of the bottom of the sliding chute is connected with one end of a limiting spring, and the other end of the limiting spring abuts against the side face of the sliding block; the simulator cabin plate is provided with a display quick-release handle clamping groove, the bottom of the display quick-release handle clamping groove is provided with a clamping groove corresponding to the sliding block and the clamping screw, and a clamping boss is arranged in the clamping groove; the bottom nut of the clamping screw can be clamped into the bottom of the clamping boss to realize clamping; a simulator display frame is arranged on the simulator cabin plate, and the display is clamped in the simulator display frame through a display frame; a locking pin is arranged on the side wall of the display frame of the simulator and corresponds to the arc-shaped convex nozzle structure on the display quick-release handle, and an ejection block is arranged below the locking pin.
2. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: when the horizontal handle part of the display quick-release handle is kept parallel to the display, the height of the outer surface of the horizontal handle part is consistent with that of the outer surface of the display frame.
3. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: the inner side end of the horizontal handle part of the display quick-release handle is a convex inclined plane, and the surface of the frame of the display, which is combined with the inner side end of the display quick-release handle, is also an inclined plane, and the inclined angles of the inclined plane and the inclined plane are consistent.
4. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: the display quick detach handle is 2, sets up the diagonal position at the display.
5. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: the display quick detach handle is 4, sets up 4 angles at the display.
6. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: the display quick-release handle is in an open state, the end of the arc-shaped convex nozzle structure is positioned on one side of the clamping groove relative to the locking pin, and the rotating shaft is positioned on the upper side of the locking pin; the display quick-release handle is in a closed state, and the end head of the arc-shaped convex nozzle structure is positioned on the other side of the clamping groove relative to the locking pin; in the process of opening and closing the display quick-release handle, the ejection block serves as a fulcrum to play a supporting role.
7. The novel quick-release display fixing structure for the aviation simulator of claim 6, wherein: the length of the ejection block is greater than the diameter of the locking pin.
8. The novel quick-release display fixing structure for the aviation simulator of claim 7, wherein: the distance between the ejection block and the locking pin is larger than the height of the arc-shaped convex nozzle structure.
9. The novel quick-release display fixing structure for the aviation simulator as claimed in claim 1, wherein: the bottom of the clamping screw is of an arc structure protruding downwards.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110219734.9A CN113028207A (en) | 2021-02-26 | 2021-02-26 | Novel quick-release display fixing structure for aviation simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110219734.9A CN113028207A (en) | 2021-02-26 | 2021-02-26 | Novel quick-release display fixing structure for aviation simulator |
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| Publication Number | Publication Date |
|---|---|
| CN113028207A true CN113028207A (en) | 2021-06-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110219734.9A Pending CN113028207A (en) | 2021-02-26 | 2021-02-26 | Novel quick-release display fixing structure for aviation simulator |
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| CN104214477A (en) * | 2014-08-20 | 2014-12-17 | 中航华东光电有限公司 | Fast installing mechanism and installing method for military liquid crystal display |
| CN106659049A (en) * | 2017-03-03 | 2017-05-10 | 中航光电科技股份有限公司 | Cabinet and electric module assembly thereof |
| CN107351859A (en) * | 2017-07-28 | 2017-11-17 | 京东方科技集团股份有限公司 | A kind of display mounting assembly, car room console and railcar |
| CN209949696U (en) * | 2019-04-15 | 2020-01-14 | 新华三信息技术有限公司 | Plug assisting mechanism and electronic equipment |
| WO2020095816A1 (en) * | 2018-11-06 | 2020-05-14 | Ｎｅｃプラットフォームズ株式会社 | Electronic apparatus, and electronic component unit |
| CN211236803U (en) * | 2020-03-09 | 2020-08-11 | 中国船舶重工集团公司第七一六研究所 | Wedge-shaped locking device free of tool disassembly and assembly |
-
2021
- 2021-02-26 CN CN202110219734.9A patent/CN113028207A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5669512A (en) * | 1995-01-05 | 1997-09-23 | Hewlett-Packard Co. | Inject-eject system for rack mounted plug-in modules |
| US20130228538A1 (en) * | 2011-09-02 | 2013-09-05 | Pierre-Louis ENGELVIN | Device for inserting, extracting and locking an electronic card in a slot |
| CN104214477A (en) * | 2014-08-20 | 2014-12-17 | 中航华东光电有限公司 | Fast installing mechanism and installing method for military liquid crystal display |
| CN106659049A (en) * | 2017-03-03 | 2017-05-10 | 中航光电科技股份有限公司 | Cabinet and electric module assembly thereof |
| CN107351859A (en) * | 2017-07-28 | 2017-11-17 | 京东方科技集团股份有限公司 | A kind of display mounting assembly, car room console and railcar |
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Application publication date: 20210625 |
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