CN218258788U - High mach unmanned aerial vehicle titanium alloy wing surface inspection tool - Google Patents
High mach unmanned aerial vehicle titanium alloy wing surface inspection tool Download PDFInfo
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- CN218258788U CN218258788U CN202222972509.5U CN202222972509U CN218258788U CN 218258788 U CN218258788 U CN 218258788U CN 202222972509 U CN202222972509 U CN 202222972509U CN 218258788 U CN218258788 U CN 218258788U
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Abstract
The application relates to a high mach unmanned aerial vehicle titanium alloy airfoil inspection frock includes: the base, the first side ear and the second side ear; the base is in a rectangular block structure, and the first side lug and the second side lug are both in a plate structure; the first side lug and the second side lug are respectively fixed on two sides of the base in the length direction, and are arranged on the same side; the plate surfaces of the first side lugs and the second side lugs are both perpendicular to one side, facing the first side lugs, of the base, the plate surfaces of the first side lugs and the plate surfaces of the second side lugs are both arranged along the length direction of the base, and the plate surfaces on the two sides of the first side lugs are respectively flush with the plate surfaces on the two sides of the second side lugs; mounting holes are formed in the plate surface of the first side lug and the plate surface of the second side lug and are used for being fixed with the airfoil. Can inspect the accuracy of unmanned aerial vehicle airfoil, when the unmanned aerial vehicle airfoil can be installed on this application, the airfoil just can be accurate install on unmanned aerial vehicle.
Description
Technical Field
The application relates to the field of aviation equipment, especially relates to a high mach unmanned aerial vehicle titanium alloy airfoil inspection frock.
Background
Along with the attention of all countries in the world to the next generation weapon aircraft equipment, the manufacturing requirement to supersonic speed unmanned aerial vehicle spare part is higher and higher, and present supersonic speed unmanned aerial vehicle airfoil is mostly titanium alloy spare earlier, needs the base installation inspection frock of airfoil to guarantee the accurate installation of the base of airfoil, and how to design the base installation inspection frock of airfoil and guarantee the accurate installation of the base of airfoil is the problem that technical staff in the field awaits the solution urgently.
Disclosure of Invention
In view of this, this application provides a high mach unmanned aerial vehicle titanium alloy airfoil inspection frock, and it can inspect the accuracy of unmanned aerial vehicle airfoil, and when the unmanned aerial vehicle airfoil can be installed on this application, the airfoil just can be accurate install on unmanned aerial vehicle.
According to an aspect of the application, a high mach unmanned aerial vehicle titanium alloy airfoil inspection frock is provided, includes:
the base, the first side ear and the second side ear;
the base is of a rectangular block structure, and the first side lug and the second side lug are both of plate structures;
the first side lug and the second side lug are respectively fixed on two sides of the base in the length direction, and the first side lug and the second side lug are arranged on the same side;
the plate surfaces of the first side lugs and the second side lugs are perpendicular to one side, facing the first side lugs, of the base, the plate surfaces of the first side lugs and the plate surfaces of the second side lugs are arranged along the length direction of the base, and the plate surfaces on the two sides of the first side lugs are flush with the plate surfaces on the two sides of the second side lugs respectively;
the mounting holes are formed in the plate surface of the first side lug and the plate surface of the second side lug and used for being fixed with the airfoil.
In a possible implementation manner, a side of the first side ear, which is away from the second side ear, is flush with an end of the base, which is away from the second side ear in the length direction;
the second side ear back of the body away from one side of first side ear with the base deviates from one end parallel and level setting on the length direction of first side ear.
In one possible implementation, the first side ear is located at a middle position in a width direction of the base.
In a possible implementation manner, two side walls in the length direction of the base are both arc-shaped, and are recessed towards one side of a plane formed by the first side ear and the second side ear.
In a possible implementation manner, two mounting holes are formed in each of the first side ear and the second side ear;
the circle centers of the four mounting holes are located on the same straight line, and the connecting lines of the circle centers of the four mounting holes are parallel to a plane on one side, facing the first side ear, of the base.
In a possible implementation manner, a through hole is formed in the base, and the through hole penetrates through two side walls in the length direction of the base;
the perforation is arranged at the same side of the first side ear.
In one possible implementation, the first side lug and the second side lug are each in a rectangular plate-like structure;
the first side ear is back to two corners of the base and the second side ear is back to two corners of the base.
In one possible implementation, the first side ear, the second side ear and the base are integrally formed.
In a possible implementation manner, the joints of the first side lug, the second side lug and the base are all round corners.
The high mach unmanned aerial vehicle titanium alloy airfoil inspection frock of this application embodiment is provided with base, first side ear and second side ear, and wherein, first side ear and second side ear set up to platelike structure, and first side ear and second side ear all fix equal vertical fixation on the length direction's of base one side lateral wall, and first side ear and second side ear interval set up. And with the both sides face parallel and level of first side ear and second side ear, constituted the overall structure of this application embodiment high mach unmanned aerial vehicle titanium alloy airfoil inspection frock from this to seted up the mounting hole on first side ear and second side ear, be used for fixing the airfoil on first side ear and second side ear through the bolt. The high mach unmanned aerial vehicle titanium alloy airfoil inspection frock of this application embodiment is to the unmanned aerial vehicle titanium alloy airfoil manufacturing back, to the inspection of the precision degree of the base of airfoil, whether the inspection airfoil base can be accurate install on unmanned aerial vehicle's organism promptly. When carrying out the inspection of the precision of high mach unmanned aerial vehicle titanium alloy airfoil, align the pilot hole on the airfoil with the mounting hole on first side ear, the second side ear, if can pass through bolt fastening, and when the airfoil was towards one side and the base butt of base this moment, accord with the accuracy requirement of unmanned aerial vehicle airfoil promptly. To sum up, this application embodiment can inspect the accuracy of unmanned aerial vehicle airfoil, and when the unmanned aerial vehicle airfoil can be installed on this application embodiment, the airfoil just can be accurate install on unmanned aerial vehicle.
Other features and aspects of the present application will become apparent from the following detailed description of exemplary embodiments, which proceeds with reference to the accompanying drawings.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate exemplary embodiments, features, and aspects of the application and, together with the description, serve to explain the principles of the application.
FIG. 1 shows a front view of a high Mach unmanned aerial vehicle titanium alloy airfoil inspection tool of an embodiment of the application;
FIG. 2 shows a left side view of a titanium alloy airfoil inspection tool for a high Mach unmanned aerial vehicle according to an embodiment of the application;
FIG. 3 shows a top view of a high Mach unmanned aerial vehicle titanium alloy airfoil inspection tool of an embodiment of the application.
Detailed Description
Various exemplary embodiments, features and aspects of the present application will be described in detail below with reference to the accompanying drawings. In the drawings, like reference numbers indicate functionally identical or similar elements. While the various aspects of the embodiments are presented in drawings, the drawings are not necessarily drawn to scale unless specifically indicated.
It will be understood that, the terms "central," "longitudinal," "lateral," "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in an orientation or positional relationship indicated in the drawings to facilitate the description of the present invention or to facilitate the description thereof, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be considered as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "plurality" means two or more unless specifically limited otherwise.
The word "exemplary" is used exclusively herein to mean "serving as an example, embodiment, or illustration. Any embodiment described herein as "exemplary" is not necessarily to be construed as preferred or advantageous over other embodiments.
Furthermore, in the following detailed description, numerous specific details are set forth in order to provide a better understanding of the present application. It will be understood by those skilled in the art that the present application may be practiced without some of these specific details. In some instances, methods, means, elements and circuits that are well known to those skilled in the art have not been described in detail so as not to obscure the present application.
Fig. 1 shows a front view of a titanium alloy airfoil inspection tool for a high mach unmanned aerial vehicle according to an embodiment of the present application. Fig. 2 shows a left side view of the high mach unmanned aerial vehicle titanium alloy airfoil inspection tool of the embodiment of the application. FIG. 3 shows a top view of the titanium alloy airfoil inspection tool for a high Mach unmanned aerial vehicle according to an embodiment of the application. As shown in fig. 1 to 3, the titanium alloy airfoil inspection tool for the high mach unmanned aerial vehicle comprises: the base 100 is in a rectangular block structure, and the first side ear 200 and the second side ear 300 are both in a plate structure. The first side ear 200 and the second side ear 300 are respectively fixed on both sides of the base 100 in the length direction, and the first side ear 200 and the second side ear 300 are arranged on the same side. The face of first side ear 200 and the face of second side ear 300 all set up with base 100 perpendicularly towards one side of first side ear 200, and the face of first side ear 200 and the face of second side ear 300 all set up along base 100's length direction, and the both sides face of first side ear 200 sets up with the both sides face parallel and level of second side ear 300 respectively. Mounting holes 400 are formed in the plate surface of the first side lug 200 and the plate surface of the second side lug 300 and used for being fixed with the airfoil.
The high mach unmanned aerial vehicle titanium alloy airfoil inspection frock of this application embodiment is provided with base 100, first side ear 200 and second side ear 300, and wherein, first side ear 200 and second side ear 300 set up to platelike structure, and first side ear 200 and second side ear 300 are all fixed equal vertical fixation on the lateral wall of one side on the length direction of base 100, and first side ear 200 and second side ear 300 interval set up. And the two side plate surfaces of the first side lug 200 and the second side lug 300 are flush, so that the whole structure of the titanium alloy airfoil inspection tool for the high mach unmanned aerial vehicle in the embodiment of the application is formed, and the first side lug 200 and the second side lug 300 are provided with mounting holes 400 for fixing the airfoil on the first side lug 200 and the second side lug 300 through bolts. The high mach unmanned aerial vehicle titanium alloy airfoil inspection frock of this application embodiment is to the unmanned aerial vehicle titanium alloy airfoil manufacturing back, to the inspection of the precision degree of the base 100 of airfoil, whether the installation that inspects airfoil base 100 promptly can be accurate is on unmanned aerial vehicle's organism. When carrying out the inspection of the precision of high mach unmanned aerial vehicle titanium alloy airfoil, align pilot hole on the airfoil with mounting hole 400 on first side ear 200, the second side ear 300, if can pass through bolt fastening, and when the airfoil was towards one side of base 100 and base 100 butt this moment, accord with the accuracy requirement of unmanned aerial vehicle airfoil promptly. To sum up, this application embodiment can inspect the accuracy of unmanned aerial vehicle airfoil, and when the unmanned aerial vehicle airfoil can be installed on this application embodiment, the airfoil just can be accurate install on unmanned aerial vehicle.
In a possible implementation manner, a side of the first side ear 200 facing away from the second side ear 300 is disposed flush with an end of the base 100 facing away from the second side ear 300 in the length direction, and a side of the second side ear 300 facing away from the first side ear 200 is disposed flush with an end of the base 100 facing away from the first side ear 200 in the length direction.
Here, it should be noted that in one possible implementation, a side of first side ear 200 facing away from second side ear 300 is a first side wall of first side ear 200, and a side of second side ear 300 facing away from first side ear 200 is a first side wall of second side ear 300. The two ends of the base 100 in the length direction are a first end face and a second end face, wherein the first side wall of the first side lug 200 is flush with the first end face, and the first side wall of the second side lug 300 is flush with the second end face.
In one possible implementation, the first side ear 200 is located at a middle position in the width direction of the base 100.
Here, it should be noted that, in one possible implementation, the first side ears 200 are disposed on the chassis 100 with the center line of the forehead in the width direction of the chassis 100 as an axis symmetry.
In one possible implementation manner, both side walls in the length direction of the base 100 are arc-shaped and are concave towards one side of the plane formed by the first side ear 200 and the second side ear 300.
Here, it should be noted that, in one possible implementation, a line connecting centers of the arc-shaped sidewalls of the two sides of the base 100 is disposed to coincide with a center line in a height direction of the base 100.
In a possible implementation manner, two mounting holes 400 are formed in each of the first side ear 200 and the second side ear 300, the centers of circles of the four mounting holes 400 are located on the same straight line, and a connection line of the centers of circles of the four mounting holes 400 is parallel to a plane of one side of the base 100 facing the first side ear 200.
Here, it should be noted that, in one possible implementation, the two mounting holes 400 of the first side ear 200 are respectively disposed adjacent to the first side wall and the third side wall of the first side ear 200, wherein the third side wall of the first side ear 200 is a side wall facing the second side ear 300. The two mounting holes 400 of the second side ear 300 are respectively disposed adjacent to the first side wall and the third side wall of the second side ear 300, wherein the third side wall of the second side ear 300 is the side wall facing the first side ear 200.
Furthermore, in a possible implementation manner, the base 100 is provided with a through hole 500, the through hole 500 is disposed through two side walls of the base 100 in the length direction, and the through hole 500 is disposed on the same side as the first side ear 200. Thereby, the fixing of the base 100 is facilitated.
Here, it should be noted that in one possible implementation, the perforation 500 may be provided in two, two perforations 500 corresponding to the first side ear 200 and the second side ear 300, respectively.
Further, in a possible implementation manner, the first side ear 200 and the second side ear 300 are both rectangular plate-shaped structures, and both corners of the first side ear 200 facing away from the base 100 and both corners of the second side ear 300 facing away from the base 100 are rounded. Therefore, the structure of the embodiment of the application is further optimized.
In one possible implementation, the first side ear 200, the second side ear 300 and the base 100 are integrally formed. Thus, fabrication of embodiments of the present application is facilitated.
In one possible implementation, the joints between the first side ear 200 and the second side ear 300 and the base 100 are rounded. Therefore, the structure of the embodiment of the application is further optimized.
Having described embodiments of the present application, the foregoing description is intended to be exemplary, not exhaustive, and not limited to the disclosed embodiments. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein is chosen in order to best explain the principles of the embodiments, the practical application, or improvements made to the technology in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein.
Claims (9)
1. The utility model provides a high mach unmanned aerial vehicle titanium alloy airfoil inspection frock which characterized in that includes:
the base, the first side ear and the second side ear;
the base is of a rectangular block structure, and the first side lug and the second side lug are both of plate structures;
the first side lug and the second side lug are respectively fixed on two sides of the base in the length direction, and the first side lug and the second side lug are arranged on the same side;
the plate surfaces of the first side lugs and the second side lugs are perpendicular to one side, facing the first side lugs, of the base, the plate surfaces of the first side lugs and the plate surfaces of the second side lugs are arranged along the length direction of the base, and the plate surfaces on the two sides of the first side lugs are flush with the plate surfaces on the two sides of the second side lugs respectively;
mounting holes are formed in the plate surface of the first side lug and the plate surface of the second side lug and are used for being fixed with the airfoil.
2. The high mach unmanned titanium alloy airfoil inspection tool of claim 1, wherein a side of the first side tab facing away from the second side tab is flush with a lengthwise end of the base facing away from the second side tab;
the second side ear back of the body away from one side of first side ear with the base deviates from one end parallel and level setting on the length direction of first side ear.
3. The high mach unmanned titanium alloy airfoil inspection tool of claim 1, wherein the first side lug is located at a middle position in a width direction of the base.
4. The high mach unmanned aerial vehicle titanium alloy airfoil inspection tool of claim 1, wherein the side walls on both sides of the base in the length direction are both arc-shaped and are recessed towards one side of a plane formed by the first side lug and the second side lug.
5. The high mach unmanned aerial vehicle titanium alloy airfoil inspection tool of claim 1, wherein two mounting holes are formed in the first side lug and the second side lug;
the circle centers of the four mounting holes are located on the same straight line, and the connecting lines of the circle centers of the four mounting holes are parallel to a plane on one side, facing the first side ear, of the base.
6. The high mach unmanned aerial vehicle titanium alloy airfoil inspection tool of claim 5, wherein the base is provided with through holes, and the through holes penetrate through side walls on two sides of the base in the length direction;
the perforation and the first side ear are arranged at the same side.
7. The high mach unmanned titanium alloy airfoil inspection tool of any one of claims 1 to 6, wherein the first and second side ears each have a rectangular plate-like structure;
the first side ear is back to two corners of the base and the second side ear is back to two corners of the base.
8. The high mach unmanned titanium alloy airfoil inspection tool of any one of claims 1 to 6, wherein the first and second side ears and the base are integrally formed.
9. The high mach unmanned titanium alloy airfoil inspection tool of any one of claims 1 to 6, wherein the joints of the first and second side ears and the base are rounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222972509.5U CN218258788U (en) | 2022-11-08 | 2022-11-08 | High mach unmanned aerial vehicle titanium alloy wing surface inspection tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222972509.5U CN218258788U (en) | 2022-11-08 | 2022-11-08 | High mach unmanned aerial vehicle titanium alloy wing surface inspection tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218258788U true CN218258788U (en) | 2023-01-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222972509.5U Active CN218258788U (en) | 2022-11-08 | 2022-11-08 | High mach unmanned aerial vehicle titanium alloy wing surface inspection tool |
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| CN (1) | CN218258788U (en) |
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- 2022-11-08 CN CN202222972509.5U patent/CN218258788U/en active Active
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