CN220894029U - Light-duty motion aircraft glass inspection frock - Google Patents
Light-duty motion aircraft glass inspection frock Download PDFInfo
- Publication number
- CN220894029U CN220894029U CN202322229853.XU CN202322229853U CN220894029U CN 220894029 U CN220894029 U CN 220894029U CN 202322229853 U CN202322229853 U CN 202322229853U CN 220894029 U CN220894029 U CN 220894029U
- Authority
- CN
- China
- Prior art keywords
- fixedly arranged
- base
- frame
- rod
- test assembly
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000011521 glass Substances 0.000 title claims abstract description 38
- 238000007689 inspection Methods 0.000 title claims abstract description 13
- 230000033001 locomotion Effects 0.000 title abstract description 7
- 238000012360 testing method Methods 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 2
- 238000004088 simulation Methods 0.000 abstract description 4
- 238000001514 detection method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 206010011376 Crepitations Diseases 0.000 description 1
- 208000037656 Respiratory Sounds Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000004720 fertilization Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model relates to a light-duty movement aircraft glass inspection tool which comprises a base, wherein a linear slide rail is fixedly arranged at the top of the base, a test assembly is detachably arranged at the top of the linear slide rail, a placing frame is fixedly arranged at the top of the base, a fixing assembly is fixedly arranged in the placing frame, a mounting frame is fixedly arranged at the top of the base, a pressure test assembly is fixedly arranged in the mounting frame, a pressing plate is fixedly arranged at the bottom of the pressure test assembly, a limiting seat is arranged at the top of the base, a limiting rod is fixedly arranged at the top of the base, and a collar piece is movably arranged outside the limiting rod. This light-duty motion aircraft glass inspection frock places glass and fixes through fixed subassembly through the rack, and the linear slide rail drives test assembly and is close to glass, through the durability when pivoted test assembly simulation aircraft glass receives the impact.
Description
Technical Field
The utility model relates to the technical field of aircraft glass detection, in particular to a light-weight moving aircraft glass detection tool.
Background
The light aircraft is an aircraft with the maximum takeoff weight less than 5700 kg, and has 40 ten thousand frames worldwide, and the light aircraft has the characteristics of portability, safety, low use requirement, capability of taking off and landing on grasslands, easiness in operation, low price and the like, and is widely used for private flight, public service flight, commercial transportation, air tour, flight training, aviation clubs, geological exploration, aerial photography, emergency rescue, seeding and fertilization, forest and fishery patrol, fire extinguishment, prospecting and the like abroad.
Compared with a large-scale aircraft, the light-duty sport aircraft has lower structural strength, the corresponding safety is relatively lower when handling unexpected disasters, and the light-duty flight type is easily affected by bird strike or hail weather, so that strength detection is required to be carried out on cockpit glass of the light-duty aircraft, and the aim of improving the safety is fulfilled by improving the structural strength of the light-duty aircraft.
Disclosure of utility model
Aiming at the defects of the prior art, the utility model provides a light-duty movement aircraft glass inspection tool, which has the advantages of multiple simulation detection and the like, and solves the problem that multiple devices are needed in the process of testing aircraft glass.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a light-duty motion aircraft glass inspection frock, includes the base, the top fixed mounting of base has the linear slide rail, the top demountable installation of linear slide rail has test assembly, the top fixed mounting of base has the rack.
The pressure test device comprises a base, and is characterized in that a fixing assembly is fixedly arranged in the placement frame, a mounting frame is fixedly arranged at the top of the base, a pressure test assembly is fixedly arranged in the mounting frame, a pressing plate is fixedly arranged at the bottom of the pressure test assembly, and a limiting seat is arranged at the top of the base.
The top of base fixed mounting has the gag lever post, the outside movable mounting of gag lever post has the lantern ring spare.
Further, the test assembly comprises a motor frame, a servo motor, a transmission shaft rod and a test drill bit, the motor frame is arranged at the top of the linear sliding rail in a threaded mode, the servo motor is fixedly arranged in the motor frame, one end of the transmission shaft rod is coaxially connected with the servo motor, and the test drill bit is fixedly arranged at the other end of the transmission shaft rod.
Further, fixed subassembly is including screwed pipe, threaded rod, hand wheel and splint, and screwed pipe fixed mounting in the inside of rack, threaded rod screw thread install in the inside of screwed pipe, and the one end fixed mounting of threaded rod has the hand wheel, and the other end fixed mounting has splint.
Further, the lantern ring spare comprises lantern ring and connecting plate, and connecting plate fixed mounting in the top of pressfitting board, lantern ring fixed connection in the connecting plate, lantern ring movable mounting in the outside of gag lever post.
Further, the pressure test assembly comprises an electric push rod and a fixing frame, the fixing frame is fixedly arranged at the top of the mounting frame, the electric push rod is fixedly arranged in the fixing frame, and the bottom of the electric push rod is fixedly connected with the pressing plate.
Compared with the prior art, the technical scheme of the application has the following beneficial effects:
This light-duty motion aircraft glass inspection frock, place glass through the rack and fix through fixed subassembly, the linear slide rail drives test assembly and is close to glass, through the durability when pivoted test assembly simulation aircraft glass receives the impact to detect that glass crackles and broken relevant data appear, and spacing seat then can be used for placing glass cover, detects glass's structural strength through pressure test assembly, data presentation when receiving the pressure is covered to simulation aircraft glass.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
fig. 2 is a top view of the structure of the mounting bracket of the present utility model.
In the figure: 1 base, 2 linear slide rail, 3 test module, 4 racks, 5 fixed subassembly, 6 pressure test module, 7 pressboard, 8 spacing seats, 9 gag lever post, 10 mounting bracket, 11 lantern ring spare.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1 and 2, in a light-duty moving aircraft glass inspection tool in this embodiment, a placement frame 4 is fixedly installed on the top of a base 1.
In this embodiment, the shape of rack 4 is "L" style of calligraphy, and the outer wall of rack 4 is provided with square plate that quantity is two for carry out the bearing to glass's bottom when the test, carry out two-way centre gripping to glass at cooperation fixed subassembly 5 and ensure the stability of glass board when the test.
It should be noted that, the outer wall of the placement frame 4 is provided with a controller, and the test assembly 3, the linear slide rail 2 and the pressure test assembly 6 are all electrically connected with the controller, and the controller is used to operate the stopping and starting of the electrical connection device.
Referring to fig. 1 and 2, in order to uniformly stress the glass, a limit rod 9 is fixedly mounted on the top of the base 1 in this embodiment, and a collar piece 11 is movably mounted on the outside of the limit rod 9.
In this embodiment, the number of the limiting rods 9 and the number of the collar pieces 11 are two, and the two collar pieces 11 are respectively mounted on the left and right sides of the pressing plate 7, so as to ensure that the pressing plate 7 can stably move up and down to ensure uniform stress of the glass cover when driven by the pressing side assembly 6.
The working principle of the embodiment is as follows:
The glass plate is fixed through the placing frame 4 and the fixing component 5, the hardness, the strength and the durability of the glass can be tested through the testing component 3, and the pressing plate 7 can be driven to test the compression resistance of the glass through the pressure testing component 6 after the glass plate is placed on the limiting seat 8 for positioning, so that the data representation of the bearing capacity of the aircraft glass when the aircraft glass is impacted can be simulated.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. A light sport aircraft glass inspection tool comprising:
Base (1), the top fixed mounting of base (1) has linear slide rail (2), the top demountable installation of linear slide rail (2) has test assembly (3), the top fixed mounting of base (1) has rack (4):
The method is characterized in that: the pressure test device is characterized in that a fixing assembly (5) is fixedly arranged in the placement frame (4), a mounting frame (10) is fixedly arranged at the top of the base (1), a pressure test assembly (6) is fixedly arranged in the mounting frame (10), a pressing plate (7) is fixedly arranged at the bottom of the pressure test assembly (6), and a limiting seat (8) is arranged at the top of the base (1);
The top of the base (1) is fixedly provided with a limiting rod (9), and the outside of the limiting rod (9) is movably provided with a collar piece (11).
2. The light sport aircraft glass inspection tool of claim 1, wherein: the test assembly (3) comprises a motor frame, a servo motor, a transmission shaft rod and a test drill bit, the motor frame is arranged at the top of the linear sliding rail (2) in a threaded mode, the servo motor is fixedly arranged in the motor frame, one end of the transmission shaft rod is coaxially connected with the servo motor, and the test drill bit is fixedly arranged at the other end of the transmission shaft rod.
3. The light sport aircraft glass inspection tool of claim 1, wherein: the fixing assembly (5) comprises a threaded pipe, a threaded rod, a hand wheel and a clamping plate, the threaded pipe is fixedly arranged in the accommodating frame (4), the threaded rod is arranged in the threaded pipe in a threaded mode, the hand wheel is fixedly arranged at one end of the threaded rod, and the clamping plate is fixedly arranged at the other end of the threaded rod.
4. The light sport aircraft glass inspection tool of claim 1, wherein: the lantern ring piece (11) comprises lantern ring and connecting plate, and connecting plate fixed mounting is in the top of pressfitting board (7), and lantern ring fixed connection is in the connecting plate, and lantern ring movable mounting is in the outside of gag lever post (9).
5. The light sport aircraft glass inspection tool of claim 1, wherein: the pressure testing assembly (6) comprises an electric push rod and a fixing frame, the fixing frame is fixedly arranged at the top of the mounting frame (10), the electric push rod is fixedly arranged in the fixing frame, and the bottom of the electric push rod is fixedly connected with the pressing plate (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322229853.XU CN220894029U (en) | 2023-08-18 | 2023-08-18 | Light-duty motion aircraft glass inspection frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322229853.XU CN220894029U (en) | 2023-08-18 | 2023-08-18 | Light-duty motion aircraft glass inspection frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220894029U true CN220894029U (en) | 2024-05-03 |
Family
ID=90875766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322229853.XU Active CN220894029U (en) | 2023-08-18 | 2023-08-18 | Light-duty motion aircraft glass inspection frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220894029U (en) |
-
2023
- 2023-08-18 CN CN202322229853.XU patent/CN220894029U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205450295U (en) | Machine carries nuclear radiation ring border and detects and sampling device | |
| CN212391413U (en) | Electric power X ray digital imaging unmanned aerial vehicle detection device and system | |
| CN105181474A (en) | Aircraft antenna housing negative pressure aerodynamic load static strength testing device | |
| CN220894029U (en) | Light-duty motion aircraft glass inspection frock | |
| CN201885999U (en) | Automatic flaw detecting device for aluminum alloy cast bars | |
| CN214895139U (en) | Many unmanned aerial vehicle monitoring system | |
| CN216117914U (en) | High-precision combined type PCB test fixture | |
| CN111806675A (en) | Aerial monitoring formula unmanned aerial vehicle | |
| CN109738244B (en) | Focusing capture type high-altitude polycyclic aromatic hydrocarbon sampler | |
| CN111409858B (en) | Be used for wing to prevent and remove icing material testing arrangement | |
| CN204575625U (en) | aviation fire test system | |
| CN109738243A (en) | A kind of high-altitude sampler for the acquisition of black carbon | |
| CN220221156U (en) | Unmanned aerial vehicle mounting device for marine fan inspection | |
| CN214066913U (en) | Color inspection machine with protection film | |
| CN209100549U (en) | A kind of endergonic device | |
| CN220854505U (en) | Puncture-resistant test device for automobile glass film production | |
| CN111007217A (en) | Hydraulic engineering detection device and method based on big data | |
| CN219455442U (en) | Balance weight frame of airplane model | |
| CN108453650B (en) | Debugging tool for steering column assembly of aircraft | |
| CN219619385U (en) | Unmanned aerial vehicle arm detection device | |
| CN221348620U (en) | Monitoring equipment for monitoring raise dust by utilizing beta rays | |
| CN216411525U (en) | LED tester with high detection precision | |
| CN219179173U (en) | Sample loading device for ageing test of xenon lamp of automotive interior and exterior sample | |
| CN219800308U (en) | Guide rail device for simulating unmanned aerial vehicle aerial photography | |
| CN220568352U (en) | Charging gun air tightness test equipment |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |