CN212112408U - Gesture response readily removable structural design device - Google Patents
Gesture response readily removable structural design device Download PDFInfo
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- CN212112408U CN212112408U CN202020997919.3U CN202020997919U CN212112408U CN 212112408 U CN212112408 U CN 212112408U CN 202020997919 U CN202020997919 U CN 202020997919U CN 212112408 U CN212112408 U CN 212112408U
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Abstract
The utility model discloses a gesture response readily removable structural design device, including aircraft nose and gesture module assembly. Further comprising: the fixed block is fixedly connected to the machine head; the support, gesture module assembly can dismantle the connection on the support, can dismantle the connection between support and the fixed block. The utility model discloses a connection can be dismantled on the support to the gesture module assembly, can dismantle the connection between support and the fixed block, can demolish whole support from the fixed block, demolish gesture module assembly from the support again, and the convenience is maintained or is changed gesture module assembly, and the installation technology is good, is difficult for causing the damage to gesture module assembly's structure. And utilize the elasticity of support to kick-back for support and fixed block interference fit can be to the front end direction application of force of gesture module assembly to the aircraft nose, make gesture module assembly closely laminate on the front end inboard of aircraft nose, play the technological effect that gesture module assembly sensitivity is good.
Description
Technical Field
The utility model belongs to the technical field of the gesture response, concretely relates to easy removable structural design device of gesture response.
Background
The gesture sensing module may recognize various gesture signals of a person, such as waving a hand, hovering, and the like. In order to detect the recognition accuracy of the gesture sensing module, a manual test is usually adopted, that is, a human hand swings or hovers in front of the gesture sensing module. However, an accurate standard cannot be determined by manual testing, the angle changes to a certain extent due to the swinging speed of each hand, and human physical strength and energy are limited, so that fatigue of people is caused by long-time testing, and human errors occur in the testing; and the accuracy and reliability of the gesture sensing module cannot be accurately determined by simple testing in a short time. Therefore, the identification accuracy of the gesture sensing module cannot be accurately tested at present.
In view of the above technical problems, chinese patent No. 2019.02.20 discloses a gesture sensing test apparatus and method, wherein a gesture sensing module recognizes a gesture signal and sends the gesture recognition result to a control board. The application of the visible gesture sensing module belongs to the mature prior art in the field.
In the field of integrated cookers and other household appliances, a gesture module assembly is generally fixed on a machine head of the household appliance by a silica gel adhesive, but the gesture module assembly has the technical problems of inconvenient maintenance and replacement and poor manufacturability; if adopt the screw directly to fix gesture module assembly on the aircraft nose of domestic appliance, although maintenance change convenience, gesture module assembly and the inboard laminating of the front end of aircraft nose are not inseparable, lead to sensitivity poor.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the above-mentioned technical problem that exists among the prior art, provide a gesture response readily removable structural design device, the maintenance is changed conveniently, and the mounting process is good, is difficult for causing the damage to the structure of gesture module assembly, and the inboard laminating of front end of gesture module assembly and aircraft nose is inseparable moreover, and sensitivity is good.
In order to solve the technical problem, the utility model discloses a following technical scheme:
the utility model provides an easy removable structural design device of gesture response, includes the aircraft nose and installs the gesture module assembly on the aircraft nose, and its characterized in that still includes: the fixed block is fixedly connected to the machine head; the support, the connection can be dismantled on the support to the gesture module assembly, utilizes the elasticity resilience of support for support and fixed block interference fit can dismantle the connection between support and the fixed block, makes the gesture module assembly closely laminate on the front end inboard of aircraft nose.
The utility model discloses a connection can be dismantled on the support to the gesture module assembly, can dismantle the connection between support and the fixed block, can demolish whole support from the fixed block, demolish gesture module assembly from the support again, and the convenience is maintained or is changed gesture module assembly, and the installation technology is good, is difficult for causing the damage to gesture module assembly's structure. And utilize the elasticity of support to kick-back for support and fixed block interference fit can be to the front end direction application of force of gesture module assembly to the aircraft nose, make gesture module assembly closely laminate on the front end inboard of aircraft nose, play the technological effect that gesture module assembly sensitivity is good.
Further, the support is provided with side pressing plates, the support and the side pressing plates are formed through a sheet metal machining process, and the support has the effects of light weight, high strength, low cost, large-scale mass production and the like. The side pressure plate is L-shaped, the side pressure plate and the fixed block are in interference fit, the side pressure plate and the fixed block are fixed through screws, the side pressure plate is a metal sheet and has certain elasticity, the fixed block is fixedly connected to the handpiece, when the side pressure plate is tightly attached to the fixed block, the side pressure plate and the fixed block are in interference fit through elastic resilience of the side pressure plate, and when force is applied to the front end of the handpiece by the gesture module assembly, the gesture module assembly can be tightly attached to the inner side of the front end of the handpiece, and the technical effect that the gesture module assembly is good in sensitivity is achieved.
Furthermore, the side of support is equipped with the mounting panel, and the both sides of gesture module assembly are equipped with the otic placode, and the otic placode passes through screw fixed connection on the mounting panel, realizes that gesture module assembly can dismantle the connection on the support, twists the screw in-process moreover, and the difficult structure that destroys gesture module assembly.
Further, the mounting plate comprises a first fixing portion, an extending portion and a second fixing portion, the extending portion is arranged between the first fixing portion and the second fixing portion, the first fixing portion, the extending portion and the second fixing portion are of an integrated structure, the first fixing portion is fixed on the side face of the support, and screws are arranged between the second fixing portion and the ear plates. The connecting node between the mounting plate and the gesture module assembly can be separated from the bracket by a certain distance, so that the whole gesture module assembly is mounted, and screws can be conveniently screwed between the second fixing part and the ear plate.
Furthermore, the top level of aircraft nose is equipped with the apron that is the L shape, and apron and fixed block pass through the fix with screw, and the top of gesture module assembly is located to the apron, and the apron can play the fixed action with the fixed block, can play the guard action again to gesture module assembly.
Furthermore, the machine head is provided with a flanging structure for mounting the LED lamp, argon arc welding is adopted between the bottom of the fixing block and the flanging structure, the fixing effect on the fixing block is achieved, and the purpose that no crater exists outside a finished product can be achieved.
And furthermore, the hand gesture module assembly further comprises hand gesture glass, the hand gesture glass is fixedly bonded with the support, the hand gesture glass is arranged on the inner side of the front end of the machine head, the front end of the hand gesture module assembly is protected, and hand gesture signals can be recognized by the hand gesture module assembly conveniently.
Furthermore, the inboard of aircraft nose front end is equipped with and is annular bellying, and the front end of gesture module assembly and the regional correspondence setting of establishing that the bellying encloses can set up transparent material such as glass in the region that the bellying encloses the establishment, the gesture module assembly of being convenient for discerns the gesture signal.
Furthermore, the aircraft nose is equipped with the bottom sprag frame, and the bottom sprag frame supports in the bottom department of gesture module assembly, can play the supporting role to the gesture module assembly after the installation, improves the installation fastness of gesture module assembly on the support.
Further, the bottom support frame comprises a base and a bottom support plate in an L shape, the bottom support plate is welded on the top surface of the base, the base is fixed on the machine head through screws, the bottom support plate is supported at the bottom of the gesture module assembly, the bottom support frame is simple in structure, the whole gesture module assembly can be conveniently assembled and disassembled on the machine head, and the support area of the gesture module assembly can be properly increased.
The utility model discloses owing to adopted above-mentioned technical scheme, following beneficial effect has:
the utility model discloses a connection can be dismantled on the support to the gesture module assembly, can dismantle the connection between support and the fixed block, can demolish whole support from the fixed block, demolish gesture module assembly from the support again, and the convenience is maintained or is changed gesture module assembly, and the installation technology is good, is difficult for causing the damage to gesture module assembly's structure. And utilize the elasticity of support to kick-back for support and fixed block interference fit can be to the front end direction application of force of gesture module assembly to the aircraft nose, make gesture module assembly closely laminate on the front end inboard of aircraft nose, play the technological effect that gesture module assembly sensitivity is good.
Drawings
The present invention will be further explained with reference to the accompanying drawings:
fig. 1 is a schematic structural diagram of a first embodiment of the present invention;
FIG. 2 is an enlarged view of the structure at A in FIG. 1;
fig. 3 is an exploded view of a first embodiment of the present invention;
FIG. 4 is a schematic structural diagram of a bracket according to a first embodiment;
FIG. 5 is a schematic diagram illustrating a gesture module assembly according to an embodiment;
fig. 6 is a schematic structural diagram of a second embodiment of the present invention;
FIG. 7 is a schematic structural diagram of a bottom support frame in the second embodiment.
In the figure, 1 — the handpiece; 2-a gesture module assembly; 3, fixing blocks; 4-a scaffold; 5-side pressing plate; 6, mounting a plate; 7-ear plate; 8-a first fixed part; 9-an extension; 10-a second fixed part; 11-a cover plate; 12-flanging structure; 13-gesture glass; 14-a boss; 15-bottom support shelf; 16-a base; 17-bottom support plate.
Detailed Description
As shown in fig. 1 to 5, for the first embodiment of the present invention,
a gesture induction easy-to-detach structural design device comprises a machine head 1 and a gesture module assembly 2 installed on the machine head 1.
The utility model discloses installation scheme to gesture module assembly 2 designs, still includes: and the fixed block 3 is fixedly connected to the machine head 1. Support 4, gesture module assembly 2 can be dismantled and connect on support 4, utilizes the elasticity resilience of support 4 for support 4 and 3 interference fit of fixed block, can dismantle the connection between support 4 and the fixed block 3, make gesture module assembly 2 closely laminate on the front end inboard of aircraft nose 1. The utility model discloses a connection can be dismantled on support 4 to gesture module assembly 2, can dismantle the connection between support 4 and the fixed block 3, can demolish whole support 4 from fixed block 3, demolish gesture module assembly 2 from support 4 again, conveniently maintain or change gesture module assembly 2, and installation technology is good, is difficult for causing the damage to gesture module assembly 2's structure. And utilize the elasticity of support 4 to kick-back for support 4 and 3 interference fit of fixed block can be to gesture module assembly 2 to the front end direction application of force of aircraft nose 1, make gesture module assembly 2 closely laminate on the front end inboard of aircraft nose 1, play the technological effect that gesture module assembly 2 sensitivity is good.
The support 4 is provided with the side pressing plate 5, the support 4 and the side pressing plate 5 are formed through a sheet metal machining process, and the steel plate has the advantages of light weight, high strength, low cost, large-scale mass production and the like. The side pressing plate 5 is L-shaped, the side pressing plate 5 is in interference fit with the fixed block 3, the side pressing plate 5 and the fixed block 3 are fixed through screws, the side pressing plate 5 is a metal sheet and has certain elasticity, the fixed block 3 is fixedly connected to the machine head 1, when the side pressing plate 5 is tightly attached to the fixed block 3, the side pressing plate 5 and the fixed block 3 are in interference fit through elastic resilience of the side pressing plate 5, and when force is applied to the gesture module assembly 2 in the front end direction of the machine head 1, the gesture module assembly 2 can be tightly attached to the inner side of the front end of the machine head 1, and the technical effect that the gesture module assembly 2 is good in sensitivity is achieved.
The side of support 4 is equipped with mounting panel 6, and the both sides of gesture module assembly 2 are equipped with otic placode 7, and otic placode 7 passes through screw fixed connection on mounting panel 6, realizes that gesture module assembly 2 can dismantle the connection on support 4, twists the screw in-process moreover, and the difficult structure of destroying gesture module assembly 2. The mounting plate 6 comprises a first fixing portion 8, an extending portion 9 and a second fixing portion 10, the extending portion 9 is arranged between the first fixing portion 8 and the second fixing portion 10, the first fixing portion 8, the extending portion 9 and the second fixing portion 10 are of an integrally formed structure, the first fixing portion 8 is fixed on the side face of the support 4, the first fixing portion 8 and the support 4 can be fixedly connected in a welding mode, and screws are arranged between the second fixing portion 10 and the ear plates 7. The connecting node between the mounting plate 6 and the gesture module assembly 2 can be separated from the bracket 4 by a certain distance, so that the whole gesture module assembly 2 is mounted, and screws can be conveniently screwed between the second fixing part 10 and the ear plate 7.
The top level of aircraft nose 1 is equipped with the apron 11 that is the L shape, and apron 11 and fixed block 3 pass through the fix with screw, and the apron 11 is located gesture module assembly 2's top, and apron 11 can play the fixed action with fixed block 3, can play the guard action to gesture module assembly 2 again.
The machine head 1 is provided with a flanging structure 12 for mounting the LED lamp, argon arc welding is adopted between the bottom of the fixing block 3 and the flanging structure 12, the fixing effect on the fixing block 3 is achieved, and the purpose that no crater exists outside a finished product can be achieved.
The utility model discloses still include gesture glass 13, gesture glass 13 and support 4 bond fixedly, and the inboard department of 1 front end of aircraft nose is located to gesture glass 13, plays the front end guard action to gesture module assembly 2, the gesture signal of 2 discernments of gesture module assembly of being convenient for moreover. The inboard of aircraft nose 1 front end is equipped with and is annular bellying 14, and the front end of gesture module assembly 2 and the regional corresponding setting that bellying 14 enclose, can set up transparent material such as glass in the region that bellying 14 enclose established, the gesture module assembly 2 of being convenient for discerns the gesture signal.
As shown in fig. 6 to 7, in order to implement the second embodiment of the present invention,
on the structure basis based on embodiment one, aircraft nose 1 is equipped with bottom sprag frame 15, and bottom sprag frame 15 supports in gesture module assembly 2's bottom department, can play the supporting role to gesture module assembly 2 after the installation, improves the installation fastness of gesture module assembly 2 on support 4.
The above is only a specific embodiment of the present invention, but the technical features of the present invention are not limited thereto. Any simple changes, equivalent substitutions or modifications made on the basis of the present invention to solve the same technical problems and achieve the same technical effects are all covered by the protection scope of the present invention.
Claims (10)
1. A gesture sensing easy-to-detach structure design device,
comprises a machine head and a gesture module assembly arranged on the machine head,
it is characterized by also comprising:
the fixed block is fixedly connected to the machine head;
the gesture module assembly is detachably connected to the bracket;
utilize the elasticity of support is kick-backed for the support with fixed block interference fit, the support with can dismantle the connection between the fixed block, gesture module assembly closely laminates on the front end inboard of aircraft nose.
2. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the support is provided with a side pressure plate, the side pressure plate is L-shaped, the side pressure plate is in interference fit with the fixed block, and the side pressure plate is fixed with the fixed block through screws.
3. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the side of support is equipped with the mounting panel, the both sides of gesture module assembly are equipped with the otic placode, the otic placode passes through screw fixed connection and is in on the mounting panel.
4. The gesture-sensing easy-to-detach structure design device according to claim 3, wherein: the mounting panel includes first fixed part, extension and second fixed part, the extension is located first fixed part with between the second fixed part, first fixed part the extension with the second fixed part is the integrated into one piece structure, first fixed part is fixed on the side of support, the second fixed part with be equipped with the screw between the otic placode.
5. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the top level of aircraft nose is equipped with the apron that is the L shape, the apron with the fixed block passes through the fix with screw, the apron is located gesture module assembly's top.
6. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the aircraft nose is equipped with the flange structure who is used for installing the LED lamp, the bottom of fixed block with adopt argon arc welding between the flange structure.
7. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the hand gesture glass is fixedly bonded with the support, and the hand gesture glass is arranged on the inner side of the front end of the machine head.
8. The gesture-sensing easy-to-detach structure design device according to claim 7, wherein: the inner side of the front end of the machine head is provided with an annular protruding portion, and the front end of the gesture module assembly and the area surrounded by the protruding portion are correspondingly arranged.
9. The gesture-sensing easy-to-detach structure design device according to claim 1, wherein: the aircraft nose is equipped with the bottom sprag frame, the bottom sprag frame supports and is in gesture module assembly's bottom department.
10. The gesture-sensing easy-to-detach structure design device according to claim 9, wherein: the bottom support frame comprises a base and a bottom support plate in an L shape, the bottom support plate is welded on the top surface of the base, the base is fixed on the machine head through screws, and the bottom support plate is supported at the bottom of the gesture module assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020997919.3U CN212112408U (en) | 2020-06-03 | 2020-06-03 | Gesture response readily removable structural design device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020997919.3U CN212112408U (en) | 2020-06-03 | 2020-06-03 | Gesture response readily removable structural design device |
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| Publication Number | Publication Date |
|---|---|
| CN212112408U true CN212112408U (en) | 2020-12-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020997919.3U Active CN212112408U (en) | 2020-06-03 | 2020-06-03 | Gesture response readily removable structural design device |
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|---|---|
| CN (1) | CN212112408U (en) |
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- 2020-06-03 CN CN202020997919.3U patent/CN212112408U/en active Active
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