CN211347743U

CN211347743U - Rudder blade coating structural performance detection device

Info

Publication number: CN211347743U
Application number: CN201922431096.8U
Authority: CN
Inventors: 常代展; 王雷
Original assignee: Jiangsu Haitai New Material Technology Co ltd
Current assignee: Jiangsu Haitai New Material Technology Co ltd
Priority date: 2019-12-30
Filing date: 2019-12-30
Publication date: 2020-08-25
Anticipated expiration: 2029-12-30

Abstract

The utility model discloses a rudder blade coating structural performance detection device, which comprises a machine body and a controller, wherein the controller is connected with a first automatic telescopic rod, a second automatic telescopic rod, a third automatic telescopic rod, an infrared sensor, a laser sensor and a heater through signal lines, the bottom end of the machine body is provided with a base, the base is provided with the controller, two corresponding workbenches are fixed on the base and are respectively a first workbench and a second workbench, the first workbench and the second workbench are respectively provided with the infrared sensor, the first workbench is provided with the heater, the second workbench is provided with the laser sensor, the top end inside the machine body is provided with the third automatic telescopic rod, the third automatic telescopic rod is connected with a pressure host, a pressing plate is arranged below the pressure host, the utility model has simple structure and novel design, the anti-compression performance of the rudder sheet can be detected under the high-temperature condition of the coating structure of the rudder sheet.

Description

Rudder blade coating structural performance detection device

Technical Field

The utility model relates to a rudder blade coating structural performance detects technical field, specifically is a rudder blade coating structural performance detection device.

Background

The rudder sheet is mainly used for being used outside large-scale equipment such as airplanes and missiles, the coating structure on the surface of the rudder sheet directly influences the use of the equipment, so the height precision is required, when the missiles are contacted with air in the flying process, a large amount of heat is generated, and meanwhile, pressure is generated, if the coating structure performance of the rudder sheet is low, the flying direction of the missiles can be directly influenced, the precision of the missile is influenced, and therefore the rudder sheet is required to be detected before being installed on the missiles.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a rudder piece coating structural performance detection device to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a rudder piece coating structure performance detection device, includes organism and controller, its characterized in that: the controller is connected with a first automatic telescopic rod, a second automatic telescopic rod, a third automatic telescopic rod, infrared sensors, laser sensors and a heater through signal lines, a base is arranged at the bottom end of the machine body, the controller is installed on the base, two corresponding work tables are fixed on the base and are respectively a first work table and a second work table, the first work table and the second work table are on the same horizontal line, the infrared sensors are respectively installed on the first work table and the second work table, the two infrared sensors are on the same horizontal line, signals are mutually transmitted between the two infrared sensors by infrared rays, the heater is arranged on the first work table, the laser sensors are arranged on the second work table, the third automatic telescopic rod is installed at the top end inside the machine body, and the pressure host is connected on the third automatic telescopic rod, and a pressure plate is arranged below the pressure host machine, and the pressure plate and the pressure host machine transmit pressure values through an analog signal line.

Preferably, the heater is installed on a first movable plate, the first movable plate is fixed on a first workbench through a first supporting rod, the first movable plate drives the first movable plate to move through a first automatic telescopic rod, the first movable plate and the first automatic telescopic rod are connected through a first connecting block, and the first automatic telescopic rod is fixed on the base through a bolt.

Preferably, the laser sensor is installed on a second movable plate, the second movable plate is fixed on a second workbench through a second supporting rod, the second movable plate drives the second movable plate to move through a second automatic telescopic rod, the second movable plate and the second automatic telescopic rod are connected through a second connecting block, and the second automatic telescopic rod is fixed on the base through a bolt.

Preferably, the heater is a flange heater.

Preferably, the laser sensor is model number ZLTA 05.

Preferably, the model of the infrared sensor is APM-12D23-20-DF 8.

Compared with the prior art, the beneficial effects of the utility model are that:

(1) the utility model discloses simple structure modern design, the coating structure that can detect the rudder piece under the high temperature condition, the compressive property of rudder piece.

(2) The utility model discloses special laser inductor can detect the coating structure on rudder piece surface, detects whether its surface levels and has the bubble.

(3) The utility model discloses a with full-automatic detection device, when the surface coating performance and the compressive property that detect the rudder piece have a problem, infrared inductor can sense the back and can report to the police, need not the manual work and is looking at always, has saved manpower and materials.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1, the present invention provides a technical solution: the utility model provides a rudder piece coating structure performance detection device, includes organism 1 and controller 2, its characterized in that: the controller 2 is connected with a first automatic telescopic rod 3, a second automatic telescopic rod 4, a third automatic telescopic rod 5, an infrared inductor 6, a laser inductor 7 and a heater 8 through signal lines, a base 9 is arranged at the bottom end of the machine body 1, the controller 2 is installed on the base 9, two corresponding workbenches are fixed on the base 9 and respectively comprise a first workbench 10 and a second workbench 11, the first workbench 10 and the second workbench 11 are on the same horizontal line, the infrared inductors 6 are respectively installed on the first workbench 10 and the second workbench 11, the two infrared inductors 6 are on the same horizontal line, signals are transmitted between the two infrared inductors 6 by infrared rays, the heater 8 is arranged on the first workbench 10, the laser inductor 7 is arranged on the second workbench 11, the third automatic telescopic rod 5 is installed at the top end inside the machine body 15, the third automatic telescopic rod 5 is connected with a pressure host machine 16, a pressure plate 17 is arranged below the pressure host machine 16, the pressure plate 17 and the pressure host machine 16 transmit a pressure value through an analog signal line, and when the pressure value reaches a fixed value, if a rudder sheet is still intact, the pressure plate can automatically retract through the third telescopic rod; if the rudder sheet is deformed and damaged, the deformed rudder sheet touches infrared rays, and the infrared rays transmit signals to the infrared sensor to give an alarm.

The utility model discloses in, heater 8 is installed 18 on first fly leaf, first fly leaf 18 is fixed on first workstation 10 through first branch 19, first fly leaf 18 drives its removal function through first automatic telescopic link 3, link to each other through first connecting block 21 between first fly leaf 18 and the first automatic telescopic link 3, first automatic telescopic link 3 passes through the bolt fastening on the base, adopts such mounting means, can drive heater 8 and make a round trip to function, can heat it comprehensively.

The utility model discloses in, laser sensor 7 is installed on second fly leaf 22, second fly leaf 22 is fixed on second workstation 11 through second branch 23, second fly leaf 22 drives its removal function through second automatic telescopic link 4, link to each other through second connecting block 25 between second fly leaf 22 and the second automatic telescopic link 4, second automatic telescopic link 4 passes through the bolt fastening on the base, adopts such mounting means, can drive laser sensor 7 and make a round trip to function, can detect more dead angles, has improved the precision that detects greatly.

The utility model discloses in, what heater 8 adopted is flange formula heater, has characteristics such as small, heating power is big, can heat various medium in various occasions.

The utility model discloses in, laser sensor 7's model is ZLTA05, has small, can detect rudder piece surface coating, detects whether it levels smoothly.

The utility model discloses in, infrared inductor 6's model is APM-12D23-20-DF8, begins to warp when the rudder piece and damages to certain degree, then can touch infrared ray, infrared ray gives infrared inductor with signal transmission, reports to the police simultaneously.

The working principle is as follows: the rudder piece that will need to detect is put into on the inside workstation of organism, open the switch board, the laser sensor swings under the effect of the automatic telescopic link of second, come to detect the rudder piece, whether detect its surface smooth and flat, rudder piece surface detection back, first automatic telescopic link drives heater round trip movement and heats the rudder piece surface, detect its high temperature resistance, the last clamp plate pressurizes the rudder piece after the heating under the effect of the automatic telescopic link of third, detect its compressive property, if the rudder piece warp or damage, can report to the police after the infrared inductor detects.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a rudder piece coating structure performance detection device, includes organism (1) and controller (2), its characterized in that: the controller (2) is connected with a first automatic telescopic rod (3), a second automatic telescopic rod (4), a third automatic telescopic rod (5), an infrared inductor (6), a laser inductor (7) and a heater (8) through signal lines, a base (9) is arranged at the bottom end of the machine body (1), the controller (2) is installed on the base (9), two corresponding workbenches are fixed on the base (9) and respectively comprise a first workbench (10) and a second workbench (11), the first workbench (10) and the second workbench (11) are on the same horizontal line, the first workbench (10) and the second workbench (11) are respectively provided with the infrared inductor (6), the two infrared inductors (6) are on the same horizontal line, signals are mutually transmitted by infrared rays between the two infrared inductors (6), the heater (8) is arranged on the first workbench (10), be equipped with laser inductor (7) on second workstation (11), third automatic telescopic link (5) are installed on the inside top of organism (1), be connected pressure host computer (16) on third automatic telescopic link (5), pressure host computer (16) below is installed clamp plate (17), the pressure value is transmitted through the analog signal line in clamp plate (17) and pressure host computer (16).

2. The rudder blade coating structure performance detection device according to claim 1, characterized in that: the heater (8) is installed on a first movable plate (18), the first movable plate (18) is fixed on a first workbench (10) through a first support rod (19), the first movable plate (18) drives the first movable plate to move through a first automatic telescopic rod (3), the first movable plate (18) is connected with the first automatic telescopic rod (3) through a first connecting block (21), and the first automatic telescopic rod (3) is fixed on the base through a bolt.

3. The rudder blade coating structure performance detection device according to claim 1, characterized in that: laser-induced ware (7) are installed on second fly leaf (22), second fly leaf (22) are fixed on second workstation (11) through second branch (23), second fly leaf (22) drive its removal operation through second automatic telescopic link (4), link to each other through second connecting block (25) between second fly leaf (22) and second automatic telescopic link (4), second automatic telescopic link (4) are through the bolt fastening on the base.

4. The rudder blade coating structure performance detection device according to claim 1, characterized in that: the heater (8) adopts a flange type heater.

5. The rudder blade coating structure performance detection device according to claim 1, characterized in that: the laser sensor (7) is in the model number ZLTA 05.

6. The rudder blade coating structure performance detection device according to claim 1, characterized in that: the model of the infrared sensor (6) is APM-12D23-20-DF 8.