CN217155208U - Detection mechanism for positioning civil air defense engineering support - Google Patents

Detection mechanism for positioning civil air defense engineering support Download PDF

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Publication number
CN217155208U
CN217155208U CN202221042582.6U CN202221042582U CN217155208U CN 217155208 U CN217155208 U CN 217155208U CN 202221042582 U CN202221042582 U CN 202221042582U CN 217155208 U CN217155208 U CN 217155208U
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CN
China
Prior art keywords
air defense
civil air
detection
positioning
detection mechanism
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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.)
Expired - Fee Related
Application number
CN202221042582.6U
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Chinese (zh)
Inventor
张伟
李季阳
邵建峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Central Research Institute of Building and Construction Co Ltd MCC Group
MCC Inspection and Certification Co Ltd
Original Assignee
Central Research Institute of Building and Construction Co Ltd MCC Group
MCC Inspection and Certification Co Ltd
Priority date (The priority date 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 date listed.)
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Application filed by Central Research Institute of Building and Construction Co Ltd MCC Group, MCC Inspection and Certification Co Ltd filed Critical Central Research Institute of Building and Construction Co Ltd MCC Group
Priority to CN202221042582.6U priority Critical patent/CN217155208U/en
Application granted granted Critical
Publication of CN217155208U publication Critical patent/CN217155208U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a detection device technical field specifically discloses a detection mechanism for civil air defense engineering support location, including the bottom plate, locate the mounting panel of bottom plate top and the detection case of rigid coupling at the bottom plate upper surface, the through-hole has all been opened to the both sides of detection case, and sliding connection has the dipperstick in the through-hole, and the one end rigid coupling that the dipperstick stretches out the detection case has the stopper, stopper and bottom plate sliding connection, the detection case internal rotation is connected with the carousel, and the upper rigid coupling has the screw rod on the carousel, and threaded connection has the gliding slider of dipperstick in can driving the detection case on the screw rod, the inner wall and the slider outer wall of detection case laminate mutually, still be equipped with drive screw rod pivoted drive assembly on the mounting panel, solved the complicated, the inconvenient problem of using of traditional civil air defense engineering detection mechanism structure.

Description

Detection mechanism for positioning civil air defense engineering support
Technical Field
The application relates to the technical field of detection devices, and particularly discloses a detection mechanism for positioning a civil air defense engineering support.
Background
The civil air defense door is a protective door used for closing an access, the support is a supporting part used for supporting the weight of a container or equipment and fixing the container or the equipment at a certain position, vibration and earthquake load during operation are born, for example, outdoor tower is born wind load, and for civil air defense engineering, the support plays an important role in supporting and protecting the support, so that the support is very important for positioning and detecting the support, and the existing positioning device for the support is very difficult to operate, can only be used by special personnel and is very inconvenient to use. Therefore, the inventor provides a detection mechanism for positioning a civil air defense engineering support so as to solve the above problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problem that traditional civil air defense engineering detection mechanism structure is complicated, inconvenient to use.
In order to achieve the purpose, the utility model discloses a basic scheme provides a detection mechanism for civil air defense engineering support location, including the bottom plate, locate the mounting panel of bottom plate top and the detection case of rigid coupling at the bottom plate upper surface, the through-hole has all been opened to the both sides of detection case, and sliding connection has the dipperstick in the through-hole, and the one end rigid coupling that the dipperstick stretches out the detection case has the stopper, stopper and bottom plate sliding connection, the detection case internal rotation is connected with the carousel, and the upper rigid coupling has the screw rod on the carousel, and threaded connection has the gliding slider of dipperstick in can driving the detection case on the screw rod, still be equipped with drive screw rod pivoted drive assembly on the mounting panel.
The principle and effect of this basic scheme lie in:
1. compared with the prior art, the utility model discloses a set up screw rod, slider and drive assembly, rotate as power drive screw rod through drive assembly, the screw rod rotates and drives the slider and remove, slides in the detection case through the slider and extrudees the dipperstick, releases the dipperstick, carries out the reading to the dipperstick and is convenient for compare, realizes the location measurement, compact structure facilitates the use.
2. Compared with the prior art, the utility model discloses set up the carousel, play the effect of being convenient for to the screw rod installation through setting up the carousel, protect the detection case bottom simultaneously, avoid the detection case impaired when the screw rod rotates.
Furthermore, the one end rigid coupling that the dipperstick stretched into the detection case has the contact piece, the contact piece is the triangle-shaped structure. The contact block with the triangular structure is convenient to slide relative to the sliding block when in contact with the sliding block, so that the situation of blocking is avoided.
Furthermore, the slider is an inverted trapezoidal structure, and the left and right inclined surfaces of the slider are respectively contacted with the inclined surfaces of the contact block.
Furthermore, a guide rod is fixedly connected in the detection box, and the top end of the guide rod is fixedly connected with the lower surface of the mounting plate. The guide rod is arranged to limit the sliding block, so that the sliding block is prevented from rotating along with the screw rod.
Further, the driving component is a motor. A driving motor is arranged as a power source.
Furthermore, a through hole is formed in the mounting plate, the motor is fixedly connected to the upper surface of the mounting plate, and an output shaft of the motor penetrates through the through hole to be fixedly connected with the screw rod. The output shaft of the motor penetrates through the through hole to be connected, and the mounting plate plays a role in connection and support.
Furthermore, the mounting blocks are symmetrically and fixedly connected to the upper surface of the mounting plate, and mounting holes convenient to mount are formed in the mounting blocks. The installation of the installation block is facilitated by arranging the installation hole.
Furthermore, the mounting plate upper surface symmetry is opened has the spacing groove that prevents that the stopper from droing. The measuring scale is prevented from sliding down by arranging the limiting groove.
Further, a position sensor is arranged on the bottom surface in the detection box. The position sensor is arranged to limit the sliding block.
Furthermore, the bottom plate is provided with a plurality of mounting holes. The installation of the bottom plate is convenient.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 shows a schematic structural diagram of a detection mechanism for positioning a civil air defense engineering support according to an embodiment of the application;
fig. 2 shows a partial schematic view of a detection mechanism for positioning a civil air defense engineering support, which is proposed by an embodiment of the application.
Detailed Description
To further illustrate the technical means and effects of the present invention adopted to achieve the objects of the present invention, the following detailed description of the embodiments, structures, features and effects according to the present invention will be made with reference to the accompanying drawings and preferred embodiments.
Reference numerals in the drawings of the specification include: bottom plate 1, mounting panel 2, detection case 3, stopper 4, dipperstick 5, slider 6, guide arm 7, installation piece 8, spacing groove 9, carousel 10, position sensor 11, contact block 12.
A detection mechanism for civil air defense construction support positioning, the embodiment is shown in fig. 1 and fig. 2: including bottom plate 1, locate mounting panel 2 and the detection case 3 of fixed connection at 1 upper surface of bottom plate 1 top of bottom plate, the through-hole has all been opened to the both sides of detection case 3, sliding connection has dipperstick 5 in the through-hole, dipperstick 5 stretches into the one end fixedly connected with contact block 12 of detection case 3, contact block 12 is the triangle-shaped structure, dipperstick 5 stretches out the one end fixedly connected with stopper 4 of detection case 3, 2 upper surface symmetries of mounting panel are opened there is the spacing groove 9 that prevents stopper 4 and drop, stopper 4's bottom card is gone into spacing inslot 9 and 1 sliding connection of bottom plate, the length of spacing groove 9 is confirmed according to the length of dipperstick 5, avoid dipperstick 5 landing through setting up spacing groove 9. 3 internal rotations of detection case are connected with carousel 10, carousel 10 top fixedly connected with screw rod, threaded connection has the gliding slider 6 of dipperstick 5 in can driving detection case 3 on the screw rod, slider 6 is the trapezoidal structure that falls, the inclined plane is respectively with the inclined plane looks adaptation of contact piece 12 about slider 6, the inner chamber and the 6 shape structure looks adaptations of slider of detection case 3, still be equipped with driving screw pivoted drive assembly on the mounting panel 2, drive assembly is the motor, the motor adopts BLDCL36 type brushless motor, it has the through hole to open on the mounting panel 2, motor fixed connection is on mounting panel 2 upper surface, the output shaft of motor passes through hole and screw rod fixed connection. The upper surface symmetry fixedly connected with installation piece 8 of mounting panel 2, fixedly connected with guide arm 7 in the detection case 3, the top of guide arm 7 and the lower fixed surface of mounting panel 2 are connected, avoid slider 6 to take place to follow the screw rod and rotate at the removal process through setting up guide arm 7, and the bottom is equipped with position sensor 11 in the detection case 3, and position sensor 11 electricity is connected with controller and power, and the controller is connected with power and motor electricity respectively.
In the implementation process of the utility model, the bottom plate 1 and the mounting plate 2 are installed through bolts, the limiting block 4 is stirred by hands to drive the measuring scale 5 to slide in the detection box 3, after the measuring scale 5 completely extends into the detection box 3, the motor is started through the control of the controller, the motor is a forward and reverse motor, the forward rotation of the motor drives the forward rotation of the screw rod, the forward rotation of the screw rod drives the slider 6 to slide downwards, the slider 6 slowly enters the detection box 3 in the downward sliding process, the internal thread of the slider 6 is checked in the moving process of the slider 6, the degree of fit of the thread between the screw rod and the slider is checked, after the slider 6 enters the detection direction, the left and right inclined planes of the slider 6 are respectively contacted with the inclined planes of the contact blocks 12, the slider 6 pushes the contact blocks 12 to respectively move towards opposite directions in the downward moving process, the measuring scale 5 moves towards the outside the detection box 3, when the slider 6 moves down to contact with the position sensor 11, the position sensor 11 transmits a signal to the controller, the controller controls the motor to stop rotating, and the reading can be read by the measuring scale 5 at the moment for comparing with the measured data size to realize positioning measurement.
Compared with the prior art, the utility model discloses a set up screw rod, slider 6 and drive assembly, rotate as power drive screw rod through drive assembly, the screw rod rotates and drives slider 6 and remove, extrudees dipperstick 5 through slider 6 slip-in detection case 3, pushes away dipperstick 5, carries out the reading to dipperstick 5 and is convenient for carry out the comparison, realizes the location measurement, facilitates the use, compact structure, practicality are strong, have solved the inconvenient problem of using of traditional civil air defense engineering detection mechanism.
The above description is only a preferred embodiment of the present invention, and the present invention is not limited to the above description, and although the present invention has been disclosed by the preferred embodiment, it is not limited to the present invention, and any person skilled in the art can make modifications or changes equivalent to the equivalent embodiments by utilizing the above disclosed technical contents without departing from the technical scope of the present invention, but all the modifications, changes and changes of the technical spirit of the present invention made to the above embodiments are also within the scope of the technical solution of the present invention.

Claims (10)

1. The utility model provides a detection mechanism for civil air defense engineering support location which characterized in that: including the bottom plate, locate the mounting panel and the detection case of rigid coupling on the bottom plate upper surface of bottom plate top, the through-hole has all been opened to the both sides of detection case, and sliding connection has the dipperstick in the through-hole, and the one end rigid coupling that the dipperstick stretches out the detection case has the stopper, stopper and bottom plate sliding connection, the detection case internal rotation is connected with the carousel, and the upper rigid coupling has the screw rod on the carousel, and threaded connection has the gliding slider of dipperstick in can driving the detection case on the screw rod, the inner wall and the slider outer wall of detection case laminate mutually, still be equipped with drive screw rod pivoted drive assembly on the mounting panel.
2. The detection mechanism for the positioning of the civil air defense engineering support according to claim 1, characterized in that one end of the measuring ruler extending into the detection box is fixedly connected with a contact block, and the contact block is of a triangular structure.
3. The detection mechanism for the positioning of the civil air defense engineering support according to claim 2, characterized in that the sliding block is of an inverted trapezoidal structure, and the left and right inclined surfaces of the sliding block are respectively contacted with the inclined surfaces of the contact blocks.
4. The detection mechanism for the positioning of the civil air defense engineering support according to claim 1, characterized in that a guide rod is fixedly connected in the detection box, and the top end of the guide rod is fixedly connected with the lower surface of the mounting plate.
5. A detection mechanism for the positioning of civil air defense construction supports according to claim 1, characterised in that the drive assembly is an electric motor.
6. The detection mechanism for the positioning of the civil air defense engineering support according to claim 5, characterized in that the mounting plate is provided with a through hole, the motor is fixedly connected on the upper surface of the mounting plate, and an output shaft of the motor passes through the through hole and is fixedly connected with the screw rod.
7. The detection mechanism for the positioning of the civil air defense engineering support according to claim 1, characterized in that the mounting blocks are symmetrically and fixedly connected to the upper surface of the mounting plate, and the mounting blocks are provided with mounting holes for facilitating mounting.
8. The detection mechanism for the positioning of the civil air defense engineering support according to claim 1, characterized in that the upper surface of the mounting plate is symmetrically provided with limit grooves for preventing the limit blocks from falling off.
9. The detection mechanism for the positioning of the civil air defense engineering support according to claim 4, characterized in that the inner bottom surface of the detection box is provided with a position sensor.
10. A detection mechanism for the positioning of a civil air defense construction support according to any of claims 1 to 9, characterized in that the base plate is provided with a plurality of mounting holes.
CN202221042582.6U 2022-04-29 2022-04-29 Detection mechanism for positioning civil air defense engineering support Expired - Fee Related CN217155208U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221042582.6U CN217155208U (en) 2022-04-29 2022-04-29 Detection mechanism for positioning civil air defense engineering support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221042582.6U CN217155208U (en) 2022-04-29 2022-04-29 Detection mechanism for positioning civil air defense engineering support

Publications (1)

Publication Number Publication Date
CN217155208U true CN217155208U (en) 2022-08-09

Family

ID=82663111

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221042582.6U Expired - Fee Related CN217155208U (en) 2022-04-29 2022-04-29 Detection mechanism for positioning civil air defense engineering support

Country Status (1)

Country Link
CN (1) CN217155208U (en)

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20220809

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