CN212030558U - Flight automatic control sensitivity testing arrangement - Google Patents

Abstract

The utility model discloses a flight automatic control sensitivity testing arrangement, including the detector, the detector outer wall runs through there is first pivot, the outer wall connection of first pivot has the protective cover, first pivot is rotated with the protective cover and is connected, the protective cover back is provided with the second pivot, second pivot outer wall connection has first fixture block, the second pivot is rotated with first fixture block and is connected, first fixture block outer wall is provided with the second fixture block, first fixture block is connected with second fixture block lock, the inside kelly that has run through of second fixture block, the second fixture block is connected with the kelly lock, first recess has been seted up to the kelly outer wall, kelly and first recess sliding connection, first recess outer wall is provided with the effect board. The utility model discloses a slide the inside of detecting appearance with the apron under the effect of movable groove, untie the fixed band and remove the fixed to inside charging wire, take out the charging wire and use.

Description

Flight automatic control sensitivity testing arrangement

Technical Field

The utility model relates to a sensitivity test field, concretely relates to flight automatic control sensitivity testing arrangement.

Background

Sensitivity refers to the degree of change in response of a method to a change in unit concentration or unit quantity of a substance to be measured, and can be described by the ratio of the response or other indicator of the instrument to the corresponding concentration or quantity of the substance to be measured, the rate of displacement of the sensitivity indicator relative to the change to be measured, and the sensitivity as a marker for measuring physical instruments.

However, the existing sensitivity testing device on the market has the problems that the cover plate is usually in a random opening and closing state in the using process, the position of the cover plate cannot be stably fixed, the cover plate can be accidentally closed in the midway of sensitivity information receiving, and when the sensitivity testing device is compared with the recorded data, the data cannot be clamped inside the cover plate for comparison and checking.

Therefore, it is necessary to develop an automatic flight control sensitivity testing device to solve the above problems.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a flight automatic control sensitivity testing arrangement, use the lead screw to connect fixedly with the detector action board, open the protective cover under the effect of first pivot, rotate first fixture block under the effect of second pivot, fill in first fixture block to the inside of action board, slide second fixture block under the effect of first recess, when sliding and fastening with first fixture block mutually, place the dead lever in the inside of second fixture block and carry out the position fixing of first fixture block and second fixture block, thereby the position angle of fixed protective cover, grasp second magnet, make second magnet and first magnet laminate, slide second magnet to the four corners department of protective cover, thereby drive first magnet to slide under the effect of second recess, thereby slide to the four corners department of the inside of protective cover, place the preceding sensitivity record table that needs to fix in the outer wall of protective cover, use second magnet and first magnet to fix the laminating in the four corners department of paper, it is more when the data, can place the data in the bottom of silica gel pad, rotate the fixed plate under the effect of third pivot, make the inside activity clamp of fixed plate slide in the inside of third recess, place the screw in the inside of fixed plate and protective cover and be connected fixedly to the record of sensitivity before can contrast when receiving sensitivity looks over compares, with the above-mentioned weak point in the solution technique.

In order to achieve the above object, the present invention provides the following technical solutions: a flight automatic control sensitivity testing device comprises a detector, wherein a first rotating shaft penetrates through the outer wall of the detector, a protective cover is connected to the outer wall of the first rotating shaft, the first rotating shaft is rotatably connected with the protective cover, a second rotating shaft is arranged at the back of the protective cover, a first clamping block is connected to the outer wall of the second rotating shaft, the second rotating shaft is rotatably connected with the first clamping block, a second clamping block is arranged on the outer wall of the first clamping block, the first clamping block is connected with the second clamping block in a buckling mode, a clamping rod penetrates through the inner portion of the second clamping block, the second clamping block is connected with the clamping rod in a buckling mode, a first groove is formed in the outer wall of the clamping rod, the clamping rod is connected with the first groove in a sliding mode, an action plate is arranged on the outer wall of the first groove, a lead screw is arranged at the joint of the action plate and the detector, the lead, second recess internally mounted has first magnet, second recess and first magnet sliding connection, the laminating of first magnet outer wall has the second magnet, second magnet outer wall is provided with the third pivot, third pivot outer wall connection has the fixed plate, the third pivot rotates with the fixed plate to be connected, the third recess has been seted up to the fixed plate inner wall, third recess internal connection has the activity to press from both sides, third recess and activity press from both sides sliding connection.

Preferably, the number of the first iron absorption stones is four, and the four first iron absorption stones are symmetrically arranged around the central axis of the second groove.

Preferably, the second magnet quantity is provided with four, four the second magnet sets up about protective cover axis symmetry, first magnet and second magnet phase-match.

Preferably, the outer wall of the movable clamp is provided with a silica gel pad, and the silica gel pad is matched with the movable clamp.

Preferably, be connected with the screw between fixed plate and the protective cover, the fixed plate is connected with the protective cover lock.

Preferably, the inner wall of the detector is provided with a movable groove, a cover plate is arranged in the movable groove, and the movable groove is connected with the cover plate in a sliding mode.

In the technical scheme, the utility model provides a technological effect and advantage:

1. the action plate and the detector are connected and fixed through the lead screw, the protective cover is opened under the action of the first rotating shaft, the first fixture block is rotated under the action of the second rotating shaft, the first fixture block is plugged into the action plate, the second fixture block slides under the action of the first groove, and when the second fixture block slides to be buckled and fixed with the first fixture block, the fixed rod is placed in the second fixture block to fix the positions of the first fixture block and the second fixture block, so that the position angle of the protective cover is fixed.

2. Through sliding the inside of detector with the apron under the effect of activity groove, untie the fixed band and remove the fixed to inside charging wire, take out the charging wire and use, compare with prior art, this device can arrange in order and accomodate and fix the charging line that need use in the testing process, avoids the problem that the charging line lost.

Drawings

In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments described in the present invention, and other drawings can be obtained by those skilled in the art according to these drawings.

Fig. 1 is a schematic front view of a cross-sectional structure of the present invention;

fig. 2 is a schematic front view of the structure of the present invention;

fig. 3 is a schematic side view of the cross-sectional structure of the present invention;

fig. 4 is an enlarged schematic structural view of a point a in fig. 1 according to the present invention;

fig. 5 is a schematic diagram of a side view profile structure of the detector of the present invention.

Description of reference numerals:

the detection device comprises a detector 1, a first rotating shaft 2, a protective cover 3, a second rotating shaft 4, a first clamping block 5, a second clamping block 6, a clamping rod 7, a first groove 8, an action plate 9, a lead screw 10, a second groove 11, a first magnet 12, a second magnet 13, a third rotating shaft 14, a fixing plate 15, a third groove 16, a movable clamp 17, a movable groove 18 and a cover plate 19.

Detailed Description

In order to make the technical solution of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings.

The utility model provides a flight automatic control sensitivity testing device as shown in figures 1-5, which comprises a detector 1, wherein a first rotating shaft 2 penetrates through the outer wall of the detector 1, the outer wall of the first rotating shaft 2 is connected with a protective cover 3, the first rotating shaft 2 is rotationally connected with the protective cover 3, the back of the protective cover 3 is provided with a second rotating shaft 4, the outer wall of the second rotating shaft 4 is connected with a first clamping block 5, the second rotating shaft 4 is rotationally connected with the first clamping block 5, the outer wall of the first clamping block 5 is provided with a second clamping block 6, the first clamping block 5 is connected with the second clamping block 6 in a buckling way, a clamping rod 7 penetrates through the inner part of the second clamping block 6, the second clamping block 6 is connected with a clamping rod 7 in a buckling way, the outer wall of the clamping rod 7 is provided with a first groove 8, the clamping rod 7 is connected with the first groove 8 in a sliding way, the outer wall of the first groove 8, the utility model discloses a detector, including effect board 9, lead screw 10 and effect board 9 threaded connection, second recess 11 has been seted up to protective cover 3 inner wall, second recess 11 internally mounted has first magnet 12, second recess 11 and first magnet 12 sliding connection, the laminating of first magnet 12 outer wall has second magnet 13, second magnet 13 outer wall is provided with third pivot 14, the 14 outer wall connections of third pivot have fixed plate 15, third pivot 14 rotates with fixed plate 15 to be connected, third recess 16 has been seted up to fixed plate 15 inner wall, third recess 16 internal connection has movable clamp 17, third recess 16 and movable clamp 17 sliding connection.

Further, in the above technical solution, the number of the first iron absorption stones 12 is four, and the four first iron absorption stones 12 are symmetrically arranged about the central axis of the second groove 11, which effectively illustrates that the second iron absorption stone 13 drives the first iron absorption stone 12 to slide under the action of the second groove 11, so as to slide to four corners inside the protecting cover 3.

Further, in above-mentioned technical scheme, second magnet 13 quantity is provided with four, four second magnet 13 sets up about the axis symmetry in the protective cover 3, first magnet 12 and second magnet 13 phase-match, and second magnet 13 has effectively been explained to this structure, makes second magnet 13 and the laminating of first magnet 12, slides second magnet 13 to the four corners department of protective cover 3, uses second magnet 13 and first magnet 12 to carry out fixed laminating to the four corners department of paper.

Further, the activity is pressed from both sides 17 outer wall and is provided with the silica gel pad, the silica gel pad presss from both sides 17 phase-matchs with the activity, and this structure has effectively explained that the inside activity of fixed plate 15 presss from both sides 17 and slides in the inside of third recess 16 to make the silica gel pad fix the data, avoid the landing.

Further, in the above technical solution, a screw is connected between the fixing plate 15 and the protective cover 3, the fixing plate 15 is connected with the protective cover 3 in a buckling manner, and the structure effectively illustrates that the fixing plate 15 is rotated under the action of the third rotating shaft 14, and the screw is placed inside the fixing plate 15 and the protective cover 3 to be connected and fixed.

The implementation mode is specifically as follows: when the device is in actual use, the action plate 9 and the detector 1 are connected and fixed by the screw rod 10, the protective cover 3 is opened under the action of the first rotating shaft 2, the first fixture block 5 is rotated under the action of the second rotating shaft 4, the first fixture block 5 is plugged into the action plate 9, the second fixture block 6 slides under the action of the first groove 8, when the second fixture block slides to be buckled and fixed with the first fixture block 5, the clamping rod 7 is placed in the second fixture block 6 to fix the positions of the first fixture block 5 and the second fixture block 6, so as to fix the position angle of the protective cover 3, the second magnet 13 is grasped, the second magnet 13 is attached to the first magnet 12, the second magnet 13 slides to the four corners of the protective cover 3, so as to drive the first magnet 12 to slide under the action of the second groove 11, so as to slide to the four corners of the protective cover 3, and place the previous sensitivity recording meter to be fixed on the outer wall of the protective cover 3, use second magnet 13 and first magnet 12 to fix the laminating in the four corners department of paper, it is more as the data, can place the data in the bottom of silica gel pad, rotate fixed plate 15 under the effect of third pivot 14, make the inside activity of fixed plate 15 press from both sides 17 and slide in the inside of third recess 16, place the screw in fixed plate 15 and protective cover 3's inside and be connected fixedly, thereby can contrast the record of looking over preceding sensitivity in the time of receiving sensitivity and contrast, compare with prior art, this device has solved and has stablized fixedly to protective cover 3's position in the use, can accidentally close midway in carrying out sensitivity information reception, when contrasting with the data of writing up before, can't contrast the problem of looking over at protective cover 3 inside with the data centre gripping.

As shown in fig. 1-5: the inner wall of the detector 1 is provided with a movable groove 18, a cover plate 19 is arranged in the movable groove 18, the movable groove 18 is connected with the cover plate 19 in a sliding mode, the structure effectively shows that the cover plate 19 slides out of the detector 1 under the action of the movable groove 18, fixing of an internal charging wire is released by unfastening a fixing belt, and the charging wire is taken out for use.

The implementation mode is specifically as follows: this device is when in actual use, when detector 1 detects and receives, when needing to carry out the power connection, can slide apron 19 out of the inside of detector 1 under the effect of activity groove 18, unties the fixed band and removes the fixed to inside charging wire, takes out the charging wire and uses, compares with prior art, and this device can arrange in order and accomodate and fix the charging line that need use in the testing process, avoids the problem that the charging line lost.

This practical theory of operation:

referring to the attached drawings 1-4 of the specification, when the device is used, an action plate 9 and a detector 1 are connected and fixed by a screw rod 10, a protective cover 3 is opened under the action of a first rotating shaft 2, a first fixture block 5 is rotated under the action of a second rotating shaft 4, the first fixture block 5 is plugged into the action plate 9, a second fixture block 6 slides under the action of a first groove 8, when the second fixture block slides to be buckled and fixed with the first fixture block 5, a clamping rod 7 is placed in the second fixture block 6 to fix the positions of the first fixture block 5 and the second fixture block 6, so that the position angle of the protective cover 3 is fixed, a second magnet 13 is held, the second magnet 13 is attached to the first magnet 12, the second magnet 13 slides to the four corners of the protective cover 3, so that the first magnet 12 slides under the action of the second groove 11 to slide to the four corners of the inner part of the protective cover 3, placing a previous sensitivity recording table to be fixed on the outer wall of a protective cover 3, fixedly attaching the four corners of paper by using a second magnet 13 and a first magnet 12, placing data at the bottom of a silica gel pad when more data exist, rotating a fixing plate 15 under the action of a third rotating shaft 14 to enable a movable clamp 17 inside the fixing plate 15 to slide inside a third groove 16, placing screws inside the fixing plate 15 and the protective cover 3 to be connected and fixed, and comparing and checking previous sensitivity records while receiving sensitivity;

referring to fig. 1-5 of the specification, when the device is used, when the detector 1 detects and receives and power connection is needed, the cover plate 19 can slide out of the detector 1 under the action of the movable groove 18, the fixing belt is unfastened to release the fixing of the internal charging wire, and the charging wire is taken out for use.

While certain exemplary embodiments of the present invention have been described above by way of illustration only, it will be apparent to those of ordinary skill in the art that the described embodiments may be modified in various different ways without departing from the spirit and scope of the present invention. Accordingly, the drawings and description are illustrative in nature and should not be construed as limiting the scope of the invention.

Claims (6)

1. The utility model provides a flight automatic control sensitivity testing arrangement, includes detector (1), its characterized in that: the outer wall of the detector (1) penetrates through a first rotating shaft (2), the outer wall of the first rotating shaft (2) is connected with a protective cover (3), the first rotating shaft (2) is rotatably connected with the protective cover (3), the back of the protective cover (3) is provided with a second rotating shaft (4), the outer wall of the second rotating shaft (4) is connected with a first clamping block (5), the second rotating shaft (4) is rotatably connected with the first clamping block (5), the outer wall of the first clamping block (5) is provided with a second clamping block (6), the first clamping block (5) is connected with the second clamping block (6) in a buckling manner, a clamping rod (7) penetrates through the inside of the second clamping block (6), the second clamping block (6) is connected with the clamping rod (7) in a buckling manner, the outer wall of the clamping rod (7) is provided with a first groove (8), the clamping rod (7) is connected with the first groove (8) in a sliding manner, the outer wall of the first groove (8) is provided with an, a screw rod (10) is arranged at the joint of the action plate (9) and the detector (1), the screw rod (10) is in threaded connection with the acting plate (9), a second groove (11) is formed in the inner wall of the protective cover (3), a first iron absorption stone (12) is arranged in the second groove (11), the second groove (11) is connected with the first iron absorption stone (12) in a sliding way, a second magnet (13) is attached to the outer wall of the first magnet (12), a third rotating shaft (14) is arranged on the outer wall of the second magnet (13), the outer wall of the third rotating shaft (14) is connected with a fixed plate (15), the third rotating shaft (14) is rotatably connected with the fixed plate (15), third recess (16) have been seted up to fixed plate (15) inner wall, third recess (16) internal connection has movable clamp (17), third recess (16) and movable clamp (17) sliding connection.

2. The automatic control sensitivity test device for the flight according to claim 1, characterized in that: the number of the first iron absorbing stones (12) is four, and the four first iron absorbing stones (12) are symmetrically arranged around the central axis of the second groove (11).

3. The automatic control sensitivity test device for the flight according to claim 1, characterized in that: second magnet (13) quantity is provided with four, four second magnet (13) set up about protective cover (3) axis symmetry, first magnet (12) and second magnet (13) phase-match.

4. The automatic control sensitivity test device for the flight according to claim 1, characterized in that: the outer wall of the movable clamp (17) is provided with a silica gel pad, and the silica gel pad is matched with the movable clamp (17).

5. The automatic control sensitivity test device for the flight according to claim 1, characterized in that: be connected with the screw between fixed plate (15) and protective cover (3), fixed plate (15) are connected with protective cover (3) lock.

6. The automatic control sensitivity test device for the flight according to claim 1, characterized in that: a movable groove (18) is formed in the inner wall of the detector (1), a cover plate (19) is arranged inside the movable groove (18), and the movable groove (18) is connected with the cover plate (19) in a sliding mode.

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