Aviation titanium alloy processing monitoring thermal imager support

Abstract

The utility model relates to an aviation titanium alloy processing monitoring thermal imager support which comprises an annular cavity matched with a thermal imager, the upper portion and the lower portion of the annular cavity are open, a bracket and a supporting block are arranged below the cavity, a supporting groove matched with a thermal imager handle is formed in the side portion of the cavity, and supporting beams are symmetrically arranged on the two sides of the supporting groove. And the end part of the joist is detachably connected with a holding arm. According to the utility model, the upper and lower parts of the annular cavity are open, a thermal imager is placed in the annular cavity during use, a handle of the thermal imager can be placed in the supporting groove, the bracket below the cavity can support the thermal imager, and the supporting block ensures that the thermal imager is not in direct contact with a machine tool, so that the thermal imager is protected; and the symmetrically arranged holding arms can enable an operator to hold the thermal imager with two hands, so that the operation is easier.

Description

Technical Field

[0001] This utility model relates to the field of aviation titanium alloy processing monitoring technology, and in particular to a support for an aviation titanium alloy processing monitoring thermal imager. Background Technology

[0002] A thermal imager for monitoring aerospace titanium alloy machining is a non-contact monitoring device used to detect the temperature distribution in the cutting area of ​​a machine tool in real time. Its core structure typically includes an infrared optical lens, a thermal imaging sensor, an image processing module, a display screen, and a data output interface. During the machining of aerospace titanium alloys, this device captures infrared radiation from the workpiece, cutting tool, or machining area to generate a thermal distribution image. This helps operators identify abnormal temperature rises, predict tool wear, and prevent workpiece thermal deformation, thereby ensuring machining accuracy and equipment safety.

[0003] However, in practical applications, existing thermal imagers for process monitoring have significant structural adaptability issues, mainly in terms of insufficient placement stability and inconvenience of handheld operation.

[0004] 1. Placement stability defects:

[0005] Most of these devices rely solely on simple flat bases or universal tripod interfaces for placement. In machining environments with frequent machine tool vibrations and limited space, such structures are prone to causing blurred monitoring images due to equipment swaying, and it is difficult to flexibly adjust the observation angle. Some devices even lack dedicated support designs, requiring additional worktable space and interfering with normal machining operations.

[0006] 2. Lack of ergonomics in handheld operation:

[0007] When temporary mobile devices are needed for multi-point monitoring, existing thermal imagers often have a regular rectangular design, lacking ergonomic curved surfaces or anti-slip structures in the grip area. Prolonged handheld use can lead to operator fatigue, and the device's center of gravity is poorly distributed (e.g., the screen and lens are unbalanced), resulting in poor stability during single-handed operation, easy screen obstruction, or accidental button presses, thus affecting monitoring efficiency.

[0008] The aforementioned problems make it difficult to quickly and stably deploy or flexibly operate the equipment in the dynamic and complex environment of aerospace titanium alloy processing, which reduces the accuracy of monitoring data and increases the labor intensity of operators. Therefore, there is an urgent need for a thermal imager structural design that combines stable placement with comfortable grip to meet the special requirements of aerospace titanium alloy processing sites. Utility Model Content

[0009] To overcome the above shortcomings, this utility model provides a support bracket for a thermal imager for monitoring the processing of aerospace titanium alloys, which aims to improve the problems of mismatch between general structure and special requirements of machine tool scenarios, low grip comfort, and reduced operating efficiency.

[0010] To achieve the above objectives, the present invention adopts the following technical solution: a support for an aerospace titanium alloy processing monitoring thermal imager, comprising an open annular cavity adapted to the thermal imager, a bracket and a support block below the cavity, a groove adapted to the handle of the thermal imager on the side of the cavity, support beams symmetrically arranged on both sides of the groove, and a handle arm detachably connected to the end of the support beam.

[0011] Preferably, the lower end of the support block is provided with an adjustable lifting mechanism.

[0012] As a further preferred embodiment, the adjustable lifting mechanism is a lifting screw.

[0013] Preferably, a magnet is provided at the bottom of the support block.

[0014] The beneficial effects of this utility model are:

[0015] This utility model features a support bracket for a thermal imager used in the processing of aerospace titanium alloys. The bracket has an open annular cavity at the top and bottom. When in use, the thermal imager is placed in the annular cavity, and the handle of the thermal imager can be placed in the slot. The bracket at the bottom of the cavity can support the thermal imager, and the support block ensures that the thermal imager does not directly contact the machine tool, thus protecting the thermal imager. The symmetrically arranged grips allow the operator to hold the thermal imager with both hands, making operation easier.

[0016] The height of the support block of the thermal imager bracket for monitoring aerospace titanium alloy processing is flexibly adjustable, which can flexibly adjust the contact state between the thermal imager bracket and the machine tool to ensure good contact; the iron is provided so that the thermal imager bracket can be attracted to the machine tool, improving the stability of the thermal imager for monitoring aerospace titanium alloy processing. Attached Figure Description

[0017] Figure 1 This is a perspective view of the present utility model;

[0018] Figure 2 This is a top view of the present invention;

[0019] Figure 3 This is the front view of the present invention;

[0020] Figure 4 This is the left view of the present invention.

[0021] In the diagram: 1. Cavity; 2. Slot; 3. Support beam; 4. Handle arm; 5. Bracket; 6. Support block; 7. Triangular or other polygonal structure. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model. Example

[0023] Reference Figures 1-4 This utility model provides a support bracket for an aerospace titanium alloy processing monitoring thermal imager, including an open annular cavity 1 adapted to the aerospace titanium alloy processing monitoring thermal imager. Below the annular cavity 1 are evenly distributed brackets 5 and support blocks 6. The side of the annular cavity 1 is provided with an arc-shaped groove 2 adapted to the handle of the thermal imager. Support beams 3 are symmetrically arranged on both sides of the arc-shaped groove 2, and grip arms 4 are detachably connected to the ends of the support beams 3. The grip arms 4 are parallel to the handle of the thermal imager. The ends of the support beams 3 are triangular or other polygonal structures 7, and the ends of the grip arms have corresponding triangular or other polygonal holes. The support beams 3 and grip arms 4 are detachably connected through the triangular or other polygonal structures 7 and the holes. They are installed in use and removed when not in use. Magnets are provided on the support blocks 6. When the aerospace titanium alloy processing monitoring thermal imager bracket and the thermal imager are placed on a machine tool, the magnets can attract the machine tool table, thereby improving the stability of the imager. Example

[0024] Reference Figures 1-4 This utility model provides a support bracket for an aerospace titanium alloy processing monitoring thermal imager, including an open annular cavity 1 adapted to the thermal imager. Below the annular cavity 1 are evenly distributed brackets 5 and support blocks 6. An arc-shaped groove 2 adapted to the handle of the thermal imager is provided on the side of the annular cavity 1. Support beams 3 are symmetrically arranged on both sides of the arc-shaped groove 2, and a grip arm 4 is detachably connected to the end of each support beam 3. The grip arm 4 is parallel to the handle of the thermal imager. The end of the support beam 3 is a triangular or other polygonal structure 7, and the end of the grip arm has a corresponding triangular or other polygonal hole. The support beam 3 and the grip arm 4 are detachably connected through the triangular or other polygonal structure 7 and the hole. It is installed when in use and removed when not in use. A magnet is installed at the bottom of the support block 6. When the aviation titanium alloy processing monitoring thermal imager bracket and thermal imager are placed on the machine tool, the magnet can attract the machine tool table, thereby improving the stability of the imager; or an adjustable screw is installed at the bottom of the support block 6 to achieve flexible adjustment of the height of the support block 6, and then a magnet is installed on the screw.

[0025] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A support for a thermal imager for monitoring the processing of aerospace titanium alloys, comprising an open annular cavity adapted to the thermal imager, characterized in that: The cavity has a bracket and a support block at the bottom, and a slot adapted to the handle of the thermal imager is provided on the side of the cavity. Support beams are symmetrically arranged on both sides of the slot, and a grip arm is detachably connected to the end of the support beam.

2. The aerospace titanium alloy processing monitoring thermal imager bracket according to claim 1, characterized in that: The lower end of the support block is equipped with an adjustable lifting mechanism.

3. The aerospace titanium alloy processing monitoring thermal imager bracket according to claim 2, characterized in that: The adjustable lifting mechanism is a lifting screw.

4. The aerospace titanium alloy processing monitoring thermal imager bracket according to claim 1, characterized in that: A magnet is provided at the bottom of the support block.

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