CN208984445U - A kind of aircraft parts machining pressure and resistance to compression force checking device - Google Patents
A kind of aircraft parts machining pressure and resistance to compression force checking device Download PDFInfo
- Publication number
- CN208984445U CN208984445U CN201821517560.4U CN201821517560U CN208984445U CN 208984445 U CN208984445 U CN 208984445U CN 201821517560 U CN201821517560 U CN 201821517560U CN 208984445 U CN208984445 U CN 208984445U
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- Prior art keywords
- resistance
- pedestal
- compression force
- rewinding box
- parts machining
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Abstract
The utility model discloses a kind of aircraft parts machining pressure and resistance to compression force checking devices, including body, the lower surface of the body is hinged with movable plate, and the front surface of body is provided with air inlet, the side surface of the body offers sliding slot, and the side surface of body corresponds to sliding slot and is internally embedded and is equipped with cleaning plant, by devising two rewinding boxes in the utility model in the utility model, different types of components can be stored, it causes confusion after avoiding detection with the components not detected, facilitates people and it is arranged；Alarm is devised, people can be reminded, hand is avoided and causes injury when cylinder pushes, provide good protective effect；Electric telescopic rod, working plate and positioning mechanism are devised, staff is facilitated and fast clamp is carried out to components, avoids detection article from being subjected to displacement when by different pressures and cause measured value inaccurate, and work efficiency is high, measuring accuracy is high.
Description
Technical field
The utility model relates to compressive resistance detection field, specifically a kind of aircraft parts machining pressure and compressive resistance
Detection device.
Background technique
Aircraft is the instrument to fly in endoatmosphere or exoatmosphere space (space), and aircraft is divided into 3 classes: aviation
Device, spacecraft, rocket and guided missile, the referred to as aircraft, such as balloon, dirigible, aircraft of flight in endoatmosphere, they lean on air
Quiet buoyancy or air relative motion generate air force go up to the air flight, space flight be known as spacecraft, such as man-made land
Ball satellite, manned spaceship, space probe, space shuttle etc., they obtained under the promotion of carrier rocket necessary speed into
Enter space, the track movement similar with celestial body is then done by inertia, wherein the components of aircraft need during production
Compressive resistance detection is carried out to it.
But present aircraft components, since the device is smaller, do not detect during carrying out compressive resistance detection
Components and detection after components be easy to cause confusion, staff can be impacted, the cylinder in the device exists
During pushing, staff can surprisingly be touched, and hand is caused to weigh wounded, have certain risk, and cannot be to components
It is automatically popped up, is not easy to staff and it is quickly fixed, reduce working efficiency.Therefore, those skilled in the art
Member provides a kind of aircraft parts machining and presses and resistance to compression force checking device, mentioned above in the background art to solve
Problem.
Utility model content
The purpose of this utility model is to provide a kind of aircraft parts machining pressure and resistance to compression force checking device, with
Solve the problems mentioned above in the background art.
To achieve the above object, the utility model provides the following technical solutions:
A kind of aircraft parts machining pressure and resistance to compression force checking device, including pedestal, groove, the first rewinding box,
Partition, the second rewinding box, stand, workbench, RF transmitter, infrared receiver, transverse slat, control switch, alarm, gas
Cylinder, pressure sensor, the first fixed plate, sliding slot, sliding block, working plate, positioning mechanism, the second fixed plate, screw rod, pushes away lower platen
Plate and electric telescopic rod, the side of the pedestal open up fluted, and the side respective slot internal slide of pedestal is equipped with
One rewinding box, first rewinding box are internally provided with partition, and the other side of the pedestal is slidably fitted with the second rewinding box,
The upper surface fixation of the pedestal is connected to two stands, and the upper surface of pedestal is connected with workbench between two stands,
The upper surface of the pedestal is provided with RF transmitter and infrared receiver at workbench front position, described infrared
The side of line transmitter is provided with infrared receiver, transverse slat is connected with above the stand, and the side of stand is provided with
Control switch, the upper surface of the transverse slat is provided with alarm, and the lower surface of transverse slat is connected with cylinder, and the cylinder stretches
End is connected with lower platen, and the lower surface insertion of the lower platen is provided with pressure sensor.
The upper surface of the workbench is connected with the first fixed plate, and work as a further solution of the present invention,
The upper surface for making platform offers sliding slot at the first fixed plate front position, and the inside of the sliding slot is equipped with sliding block, described
The upper surface of sliding block is connected with working plate, and the rear surface of the working plate is connected with electric telescopic rod, and the upper surface of working plate
It is connected with positioning mechanism.
The positioning mechanism includes the second fixed plate, screw rod and push plate as a further solution of the present invention,
The inside of the positioning mechanism is equipped with the second fixed plate, and the side of second fixed plate, which is run through, is equipped with screw rod, the spiral shell
One end of bar is connected with push plate by bearing, and second fixed plate is connect with screw rod by screw thread with rotating manner, described fixed
There are two the quantity of position mechanism is arranged altogether.
First fixed plate and working plate are connected by electric telescopic rod as a further solution of the present invention,
It connects, the working plate is connect with workbench by sliding slot and sliding block in sliding manner.
The internal structure of second rewinding box and the first rewinding box is interior as a further solution of the present invention,
Portion's structure is identical, and the side surface of the second rewinding box and the first rewinding box is connected with pull rod.
The lower surface of the RF transmitter is connected with fixed block as a further solution of the present invention, institute
The lower surface for stating infrared receiver is connected with fixed block.
Compared with prior art, the utility model has the beneficial effects that
1., can be to different types of components by devising the first rewinding box and the second rewinding box in the utility model
It is stored, the components for avoiding the components after detecting and not detecting cause confusion, and facilitate staff and carry out to it
It arranges；
2., can be to work by devising RF transmitter, infrared receiver and alarm in the utility model
Personnel remind, and avoid hand and cause injury when cylinder pushes, provide good protective effect；
3. facilitating staff couple by devising electric telescopic rod, working plate and positioning mechanism in the utility model
Components carry out fast clamp, and detection article is avoided to be subjected to displacement when by different pressures and cause measured value is inaccurate to ask
Topic, and work efficiency is high, measuring accuracy is high.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of a kind of aircraft parts machining pressure and resistance to compression force checking device；
Fig. 2 is the structural representation of positioning mechanism in a kind of aircraft parts machining pressure and resistance to compression force checking device
Figure；
Fig. 3 is the enlarged structure schematic diagram of part A in Fig. 1.
In figure: 1, pedestal；2, groove；3, the first rewinding box；4, partition；5, the second rewinding box；6, stand；7, workbench；
8, RF transmitter；9, infrared receiver；10, transverse slat；11, control switch；12, alarm；13, cylinder；14, it pushes
Plate；15, pressure sensor；16, the first fixed plate；17, sliding slot；18, sliding block；19, working plate；20, positioning mechanism；201, second
Fixed plate；202, screw rod；203, push plate；21, electric telescopic rod.
Specific embodiment
Please refer to Fig. 1~3, in the utility model embodiment, a kind of aircraft parts machining pressure and compressive resistance inspection
Survey device, including pedestal 1, groove 2, the first rewinding box 3, partition 4, the second rewinding box 5, stand 6, workbench 7, infrared ray transmitting
Device 8, infrared receiver 9, transverse slat 10, control switch 11, alarm 12, cylinder 13, lower platen 14, pressure sensor 15,
One fixed plate 16, sliding slot 17, sliding block 18, working plate 19, positioning mechanism 20, the second fixed plate 201, screw rod 202,203 and of push plate
Electric telescopic rod 21, the side of pedestal 1 opens up fluted 2, and 2 internal slide of side respective slot of pedestal 1 is equipped with first
Rewinding box 3, the first rewinding box 3 are internally provided with partition 4, and the other side of pedestal 1 is slidably fitted with the second rewinding box 5, and second
The internal structure of rewinding box 5 is identical as the internal structure of the first rewinding box 3, and the side table of the second rewinding box 5 and the first rewinding box 3
Face is connected with pull rod, by devising the first rewinding box 3 and the second rewinding box 5, can carry out to different types of components
Storage, the components for avoiding the components after detecting and not detecting cause confusion, facilitate staff and arrange to it.
The upper surface fixation of pedestal 1 is connected to two stands 6, and the upper surface of pedestal 1 is connected between two stands 6
The upper surface of workbench 7, pedestal 1 is provided with RF transmitter 8 and infrared receiver 9 at 7 front position of workbench,
The side of RF transmitter 8 is provided with infrared receiver 9, and the lower surface of RF transmitter 8 is connected with fixed block, infrared
The lower surface of line receiver 9 is connected with fixed block, and the top of stand 6 is connected with transverse slat 10, and the side of stand 6 is provided with control
Switch 11, the upper surface of transverse slat 10 is provided with alarm 12, and the lower surface of transverse slat 10 is connected with cylinder 13, and cylinder 13 stretches
End is connected with lower platen 14, and the lower surface insertion of lower platen 14 is provided with pressure sensor 15, by devising infrared ray transmitting
Device 8, infrared receiver 9 and alarm 12, can remind staff, avoid hand and make when cylinder 13 pushes
At injury, good protective effect is provided.
The upper surface of workbench 7 is connected with the first fixed plate 16, and the upper surface of workbench 7 is before the first fixed plate 16
The orientation place of setting offers sliding slot 17, and the inside of sliding slot 17 is equipped with sliding block 18, and the upper surface of sliding block 18 is connected with working plate 19, work
The rear surface for making plate 19 is connected with electric telescopic rod 21, and the upper surface of working plate 19 is connected with positioning mechanism 20, and first is fixed
Plate 16 is connect with working plate 19 by electric telescopic rod 21, and working plate 19 and workbench 7 pass through sliding slot 17 and sliding block 18 to slide
Mode connects, and positioning mechanism 20 includes the second fixed plate 201, screw rod 202 and push plate 203, and the inside of positioning mechanism 20 is installed
There is the second fixed plate 201, through screw rod 202 is equipped with, one end of screw rod 202 is solid by bearing for the side of the second fixed plate 201
It is connected to push plate 203, the second fixed plate 201 is connect with screw rod 202 by screw thread with rotating manner, and the quantity of positioning mechanism 20 is set altogether
There are two setting, by devising electric telescopic rod 21, working plate 19 and positioning mechanism 20, facilitate staff to components into
Row fast clamp avoids detecting the problem that article is subjected to displacement when by different pressures and causes measured value inaccurate, and work
Make high-efficient, measuring accuracy height.
The working principle of the utility model is: firstly, being controlled by the ST10R167 type microcontroller in control switch 11
The electric telescopic rod 21 of CDJ2B10-10 type processed works, and electric telescopic rod 21 pushes the work forward forward plate 19, the cunning under working plate 19
Block 18 slides in sliding slot 17, it is pushed outwardly from the following position directly of lower platen 14, components are placed on by user
On working plate 19, screw rod 202 is inwardly screwed, driving push plate 203, inwardly movement clamps components, can adapt in difference
The components of size improve the practicality, and electric telescopic rod 21 is shunk, and the components on working plate 19 are brought back to lower platen
At 14 following position directly, different size of pressure value is provided by control switch 11, cylinder 13 moves downward, and drives lower platen
14 move downward, and the pressure sensor 15 on lower platen 14 first touches components, can directly know pressure value, working efficiency
Height, measuring accuracy is high, avoids detecting the problem that article is subjected to displacement when by different pressures and causes measured value inaccurate；
Then, user pulls open the first rewinding box 3 and the second rewinding box 5 to both sides, and the first rewinding box 3 skids off in groove 2, and inside is set
Three pieces of partitions 4 are set, the components not detected can be placed in the first rewinding box 3 by user, the components that will test
It is placed in the second rewinding box 5, such design can carry out storage arrangement, the person of being convenient to use to different components；Most
Afterwards, when cylinder 13 pushes, once the hand of staff unintentionally encounters between RF transmitter 8 and infrared receiver 9
When at position, when infrared receiver 9 can't accept the signal of the transmitting of RF transmitter 8, then data-signal is passed into control
ST10R167 type microcontroller in system switch 11 works to control alarm 12, and alarm 12 sounds an alarm sound and carries out to people
It reminds, it is injured in the process of work to can be avoided personnel.
It is above-described, the only preferable specific embodiment of the utility model, but the protection scope of the utility model is simultaneously
It is not limited to this, anyone skilled in the art within the technical scope disclosed by the utility model, according to this reality
It is subject to equivalent substitution or change with novel technical solution and its utility model design, should all covers the protection in the utility model
Within the scope of.
Claims (6)
1. a kind of aircraft parts machining pressure and resistance to compression force checking device, including pedestal (1), which is characterized in that described
The side of pedestal (1) opens up fluted (2), and side respective slot (2) internal slide of pedestal (1) is equipped with the first rewinding box
(3), first rewinding box (3) is internally provided with partition (4), and the other side of the pedestal (1) is slidably fitted with the second receipts
The upper surface fixation of magazine (5), the pedestal (1) is connected to two stands (6), and the upper surface of pedestal (1) is close to two stands
(6) it is connected between workbench (7), the upper surface of the pedestal (1) is provided with infrared ray at workbench (7) front position
The side of transmitter (8) and infrared receiver (9), the RF transmitter (8) is provided with infrared receiver (9), institute
It states and is connected with above stand (6) transverse slat (10), and the side of stand (6) is provided with control switch (11), the transverse slat (10)
Upper surface be provided with alarm (12), and the lower surface of transverse slat (10) is connected with cylinder (13), the cylinder (13) it is flexible
End is connected with lower platen (14), and the lower surface insertion of the lower platen (14) is provided with pressure sensor (15).
2. a kind of aircraft parts machining pressure according to claim 1 and resistance to compression force checking device, feature exist
In the upper surface of the workbench (7) is connected with the first fixed plate (16), and the upper surface of workbench (7) is fixed close to first
It is offered sliding slot (17) at plate (16) front position, the inside of the sliding slot (17) is equipped with sliding block (18), the sliding block (18)
Upper surface be connected with working plate (19), the rear surface of the working plate (19) is connected with electric telescopic rod (21), and working plate
(19) upper surface is connected with positioning mechanism (20).
3. a kind of aircraft parts machining pressure according to claim 2 and resistance to compression force checking device, feature exist
In the positioning mechanism (20) includes the second fixed plate (201), screw rod (202) and push plate (203), the positioning mechanism
(20) inside is equipped with the second fixed plate (201), and the side of second fixed plate (201), which is run through, is equipped with screw rod (202),
One end of the screw rod (202) is connected with push plate (203) by bearing, and second fixed plate (201) passes through with screw rod (202)
Screw thread is connected with rotating manner, there are two the quantity of the positioning mechanism (20) is arranged altogether.
4. a kind of aircraft parts machining pressure according to claim 2 and resistance to compression force checking device, feature exist
In first fixed plate (16) is connect with working plate (19) by electric telescopic rod (21), the working plate (19) and work
Platform (7) is connected in sliding manner by sliding slot (17) and sliding block (18).
5. a kind of aircraft parts machining pressure according to claim 1 and resistance to compression force checking device, feature exist
In, the internal structure of second rewinding box (5) is identical as the internal structure of the first rewinding box (3), and the second rewinding box (5) and
The side surface of first rewinding box (3) is connected with pull rod.
6. a kind of aircraft parts machining pressure according to claim 1 and resistance to compression force checking device, feature exist
In the lower surface of the RF transmitter (8) is connected with fixed block, and the lower surface of the infrared receiver (9) is connected with
Fixed block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821517560.4U CN208984445U (en) | 2018-09-18 | 2018-09-18 | A kind of aircraft parts machining pressure and resistance to compression force checking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821517560.4U CN208984445U (en) | 2018-09-18 | 2018-09-18 | A kind of aircraft parts machining pressure and resistance to compression force checking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208984445U true CN208984445U (en) | 2019-06-14 |
Family
ID=66784407
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821517560.4U Expired - Fee Related CN208984445U (en) | 2018-09-18 | 2018-09-18 | A kind of aircraft parts machining pressure and resistance to compression force checking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208984445U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110686814A (en) * | 2019-10-17 | 2020-01-14 | 徐州烁鼎机械制造有限公司 | Engineering machine tool dismantles and examines pressure equipment |
| CN111413209A (en) * | 2020-04-23 | 2020-07-14 | 中国地质科学院水文地质环境地质研究所 | A pressure-bearing detection device for civil mechanics is experimental |
| CN112198054A (en) * | 2020-10-12 | 2021-01-08 | 广东恒成科技股份有限公司 | Pressure resistance detection and application device of large casting simulation body |
| CN115343038A (en) * | 2022-10-13 | 2022-11-15 | 南通市东盛铸锻有限公司 | Metal parts resistance to deformation ability test equipment |
-
2018
- 2018-09-18 CN CN201821517560.4U patent/CN208984445U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110686814A (en) * | 2019-10-17 | 2020-01-14 | 徐州烁鼎机械制造有限公司 | Engineering machine tool dismantles and examines pressure equipment |
| CN111413209A (en) * | 2020-04-23 | 2020-07-14 | 中国地质科学院水文地质环境地质研究所 | A pressure-bearing detection device for civil mechanics is experimental |
| CN112198054A (en) * | 2020-10-12 | 2021-01-08 | 广东恒成科技股份有限公司 | Pressure resistance detection and application device of large casting simulation body |
| CN115343038A (en) * | 2022-10-13 | 2022-11-15 | 南通市东盛铸锻有限公司 | Metal parts resistance to deformation ability test equipment |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190614 Termination date: 20210918 |
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| CF01 | Termination of patent right due to non-payment of annual fee |