CN109060576A - A kind of wear-resistant detection device of aircraft brake wheel - Google Patents
A kind of wear-resistant detection device of aircraft brake wheel Download PDFInfo
- Publication number
- CN109060576A CN109060576A CN201811032975.7A CN201811032975A CN109060576A CN 109060576 A CN109060576 A CN 109060576A CN 201811032975 A CN201811032975 A CN 201811032975A CN 109060576 A CN109060576 A CN 109060576A
- Authority
- CN
- China
- Prior art keywords
- wear
- seat
- brake wheel
- detection device
- aircraft brake
- 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.)
- Withdrawn
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/56—Investigating resistance to wear or abrasion
Abstract
The present invention provides a kind of wear-resistant detection device of aircraft brake wheel, including curved support seat, adjusts bolt, placement plate, horizontal ruler, pressing plate, laser displacement sensor, sliding seat and locking knob；The output shaft of the communtation deceleration device penetrates into the centre of connecting plate upwards, and it is clamped by rectangular fixture block and connecting plate, the adjusting bolt is upward through in the stepped hole in placement plate, the top center of the placement plate is inlaid with guiding axis, and guiding axis is equipped with the pressing plate that can slide up and down, on the inner wall of the frame and inner opposite end is mounted on the support column of vertical direction, and two groups of lateral support columns are additionally provided on the top inner side face of frame.Can the detection position to laser displacement sensor be adjusted, so that the different location up and down to brake machine wheel periphery detects, the degree of wear of inner rings different on brake machine wheel top end face position can be detected, save the time of detection.
Description
Technical field
The invention belongs to brake machine wheel detection technique fields, more specifically, in particular to a kind of aircraft brake wheel
Wear-resistant detection device.
Background technique
Brake, the mechanical brake device also known as retarder that can exactly slow down, brake machine wheel is just in aeronautical technology
It is the device that can make aircraft, when brake machine wheel abrasion is more serious, is easy to cause more serious accident.
Based on above-mentioned, the inventors discovered that, in the abrasion detection of brake machine wheel, usually use hand-held device or use
Single detection device detects the abrasion of brake machine wheel, and detection faces are narrow, often waste the biggish time.
Then, in view of this, being studied improvement for existing structure and missing, a kind of aircraft brake wheel is provided
Wear-resistant detection device, to achieve the purpose that with more more practical value.
Summary of the invention
In order to solve the above technical problem, the present invention provides a kind of wear-resistant detection devices of aircraft brake wheel, with solution
Certainly the problems mentioned above in the background art.
The purpose and effect of the wear-resistant detection device of aircraft brake wheel of the present invention, are reached by technological means in detail below
At:
A kind of wear-resistant detection device of aircraft brake wheel, including frame, control cabinet, curved support seat, ball base, connection
Plate, communtation deceleration device, rectangular fixture block adjust bolt, placement plate, guiding axis, stepped hole, horizontal ruler, pressing plate, clump weight placement
Slot, support column, detent sliding slot, laser displacement sensor, sliding seat and locking knob；The curved support seat fixation is embedded in frame
The inside of frame, and array ball base is inlaid on the top end face of curved support seat, the communtation deceleration device is arranged in curved support
The inside of seat, and the output shaft of communtation deceleration device penetrates into the centre of connecting plate upwards, and by rectangular fixture block with connect board
It connects, four groups of adjusting bolts is welded in the connecting plate apical lateral, and adjust bolt and be upward through the stepped hole in placement plate
Interior, the top center of the placement plate is inlaid with guiding axis, and guiding axis is equipped with the pressing plate that can slide up and down, on the pressing plate
Three equipped with ring-shaped assemble pouring weight placing groove, and on the inner wall of the frame and inner opposite end is mounted on the branch of vertical direction
Dagger, and two groups of lateral support columns are additionally provided on the top inner side face of frame, close to curved support seat on the sliding seat
One end is inlaid with laser displacement sensor, and is connected between laser displacement sensor and control cabinet by conducting wire.
Further, the bottom face of the connecting plate is attached on the ball of ball base.
Further, nut is equipped on the inside of the stepped hole and on the adjusting bolt of stepped hole bottom side.
Further, the Basolateral of the placement plate is uniformly connected with three groups of horizontal rulers.
Further, the sliding seat sliding is on the detent sliding slot of support column, and the both ends of sliding seat are equipped with locking rotating
Button.
Further, the distance between two groups of support columns in the frame top inner side are greater than the diameter of pressing plate.
Compared with prior art, the invention has the following beneficial effects:
The setting of horizontal ruler in the present invention is adjusted the level of placement plate using the nut adjusted on bolt, and utilizes
Horizontal ruler is grasped, and the Level tune of placement plate can be made more accurate.
By be arranged sliding seat, can the detection position to laser displacement sensor be adjusted, outside to brake machine wheel
The different location up and down in week is detected, while can also be carried out to the degree of wear of different inner rings position on brake machine wheel top end face
Detection, saves the time of detection, can also will be utilized respectively two groups of laser displacement sensors and detect identical position, reduces detection and misses
The generation of difference.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is another side structural schematic diagram of the invention.
Fig. 3 is enlarged structure schematic diagram at A of the invention.
Fig. 4 is left side structural schematic diagram of the invention.
In figure, the corresponding relationship of component names and accompanying drawing number are as follows:
Frame -1, control cabinet -101, curved support seat -2, ball base -201, connecting plate -3, communtation deceleration device -301, square card
Block -302 adjusts bolt -303, and placement plate -4, guiding axis -401, stepped hole -402, horizontal ruler -403, pressing plate -5, clump weight is put
Set slot -501, support column -6, detent sliding slot -601, laser displacement sensor -7, sliding seat -701, locking knob -701.
Specific embodiment
Embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples.Following embodiment is used for
Illustrate the present invention, but cannot be used to limit the scope of the invention.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more；Term " on ",
The orientation or positional relationship of the instructions such as "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and should not be understood as instruction or
Imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connected " " connects
Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected；It can be machine
Tool connection, is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment:
As shown in attached drawing 1 to attached drawing 4:
The present invention provides a kind of wear-resistant detection device of aircraft brake wheel, including frame 1, control cabinet 101, curved support seat
2, ball base 201, connecting plate 3, communtation deceleration device 301, rectangular fixture block 302, adjusting bolt 303, placement plate 4, guiding axis 401,
Stepped hole 402, horizontal ruler 403, pressing plate 5, clump weight placing groove 501, support column 6, detent sliding slot 601, laser displacement sensor
7, sliding seat 701 and locking knob 701；The fixed inside for being embedded in frame 1 of the curved support seat 2, and curved support seat 2
Array ball base 201 is inlaid on top end face, the inside of curved support seat 2 is arranged in the communtation deceleration device 301, and commutation subtracts
The output shaft of fast device 301 penetrates into the centre of connecting plate 3 upwards, and is clamped by rectangular fixture block 302 with connecting plate 3, the company
It is welded with four groups of adjusting bolts 303 in 3 apical lateral of fishplate bar, and adjusts bolt 303 and is upward through the stepped hole in placement plate 4
In 402, the top center of the placement plate 4 is inlaid with guiding axis 401, and guiding axis 401 is equipped with the pressing plate that can slide up and down
5, what the pressing plate 5 was equipped with ring-shaped three assembles pouring weight placing groove 501, and on the inner wall of the frame 1 and inner opposite end is equal
The support column 6 of vertical direction is installed, and is additionally provided with two groups of lateral support columns 6, the sliding on the top inner side face of frame 1
One end on seat 701 close to curved support seat 2 is inlaid with laser displacement sensor 7, and laser displacement sensor 7 and control cabinet
It is connected between 101 by conducting wire, laser displacement sensor 7 selects PL-02.
Wherein, the bottom face of the connecting plate 3 is attached on the ball of ball base 201, can be supported to connecting plate 3, together
When be also convenient for the rotation of connecting plate 3.
Wherein, it is equipped with nut on the adjusting bolt 303 of 402 inside of stepped hole and 402 bottom side of stepped hole, it can benefit
It is finely adjusted with level of the nut to placement plate.
Wherein, the Basolateral of the placement plate 4 is uniformly connected with three groups of horizontal rulers 403, available during the adjustment
Three groups of horizontal rulers 403 precisely adjust the level of placement plate.
Wherein, the sliding of sliding seat 701 is on the detent sliding slot 601 of support column 6, and the both ends of sliding seat 701 are equipped with
Locking knob 701 is fixed using position of the locking knob 701 to sliding seat 701.
Wherein, the distance between two groups of support columns 6 in 1 top inner side of frame are greater than the diameter of pressing plate 5, avoid propping up
Two groups of 7 signals of laser displacement sensor being slidably installed on dagger 6 are issued on pressing plate 5, cause detection error.
The specifically used mode and effect of the present embodiment:
In the present invention, first with the horizontal ruler 403 of 4 bottom side of placement plate, and by adjusting the nut on bolt 303 to placement plate
Level be adjusted, the brake machine wheel that detects will be needed to pass through guiding axis 401 and be placed in placement plate 4, pressure is then utilized
Plate 5 is pressed in the top of brake machine wheel, and to push down brake machine wheel in clump weight placing groove 501, then clump weight is put into
The position of sliding seat 701 is adjusted, and is lockked using the locking knob 701 at 701 both ends of sliding seat, starting motor passes through commutation
Retarder 301 drives connecting plate 3 and placement plate 4 slowly to rotate, and utilizes the laser displacement sensor 7 on four groups of sliding seats 701
In the distance results feedback to control cabinet 101 that detects, and will test to the periphery of brake machine wheel and upper surface respectively,
The different location up and down of brake machine wheel periphery is detected, while can also be to different inner rings position on brake machine wheel top end face
The degree of wear is detected.
The embodiment of the present invention is given for the purpose of illustration and description, and is not exhaustively or by this to send out
It is bright to be limited to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Choosing
Selecting and describe embodiment is and to make those skilled in the art to more preferably illustrate the principle of the present invention and practical application
It will be appreciated that the present invention is to design various embodiments suitable for specific applications with various modifications.
Claims (6)
1. a kind of wear-resistant detection device of aircraft brake wheel, it is characterised in that: the wear-resistant detection of the aircraft brake wheel
Device includes frame (1), control cabinet (101), curved support seat (2), ball base (201), connecting plate (3), communtation deceleration device
(301), rectangular fixture block (302) is adjusted bolt (303), placement plate (4), guiding axis (401), stepped hole (402), horizontal ruler
(403), pressing plate (5), clump weight placing groove (501), support column (6), detent sliding slot (601), laser displacement sensor (7) are sliding
Dynamic seat (701) and locking knob (701)；The fixed inside for being embedded in frame (1) of the curved support seat (2), and curved support
It is inlaid with array ball base (201) on the top end face of seat (2), the communtation deceleration device (301) is arranged in curved support seat (2)
Inside, and the output shaft of communtation deceleration device (301) penetrates into the centre of connecting plate (3) upwards, and by rectangular fixture block (302) with
Connecting plate (3) is clamped, and four groups of adjusting bolts (303) is welded in connecting plate (3) apical lateral, and adjust bolt (303)
It being upward through the stepped hole (402) on placement plate (4) Nei, the top center of the placement plate (4) is inlaid with guiding axis (401),
And guiding axis (401) is equipped with and can slide up and down pressing plate (5), what the pressing plate (5) was equipped with ring-shaped three assembles pouring weight and puts
It sets slot (501), on the inner wall of the frame (1) and inner opposite end is mounted on the support column (6) of vertical direction, and frame
(1) two groups of lateral support columns (6) are additionally provided on top inner side face, on the sliding seat (701) close curved support seat (2)
One end be inlaid with laser displacement sensor (7), and pass through conducting wire between laser displacement sensor (7) and control cabinet (101)
It is connected.
2. the wear-resistant detection device of aircraft brake wheel as described in claim 1, it is characterised in that: the connecting plate (3)
Bottom face is attached on the ball of ball base (201).
3. the wear-resistant detection device of aircraft brake wheel as described in claim 1, it is characterised in that: the stepped hole (402)
Nut is equipped on the adjusting bolt (303) of inside and stepped hole (402) bottom side.
4. the wear-resistant detection device of aircraft brake wheel as described in claim 1, it is characterised in that: the placement plate (4)
Basolateral is uniformly connected with three groups of horizontal rulers (403).
5. the wear-resistant detection device of aircraft brake wheel as described in claim 1, it is characterised in that: the sliding seat (701)
Sliding is on the detent sliding slot (601) of support column (6), and the both ends of sliding seat (701) are equipped with locking knob (701).
6. the wear-resistant detection device of aircraft brake wheel as described in claim 1, it is characterised in that: frame (1) top
The distance between two groups of support columns (6) on inside are greater than the diameter of pressing plate (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811032975.7A CN109060576A (en) | 2018-09-05 | 2018-09-05 | A kind of wear-resistant detection device of aircraft brake wheel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811032975.7A CN109060576A (en) | 2018-09-05 | 2018-09-05 | A kind of wear-resistant detection device of aircraft brake wheel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109060576A true CN109060576A (en) | 2018-12-21 |
Family
ID=64758541
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811032975.7A Withdrawn CN109060576A (en) | 2018-09-05 | 2018-09-05 | A kind of wear-resistant detection device of aircraft brake wheel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109060576A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110864989A (en) * | 2019-11-19 | 2020-03-06 | 上海市特种设备监督检验技术研究院 | Test platform and method for detecting wear resistance of parts in pipeline |
| CN116839651A (en) * | 2023-08-30 | 2023-10-03 | 沈阳国仪检测技术有限公司 | System for be used for testing pipeline detector spare part |
-
2018
- 2018-09-05 CN CN201811032975.7A patent/CN109060576A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110864989A (en) * | 2019-11-19 | 2020-03-06 | 上海市特种设备监督检验技术研究院 | Test platform and method for detecting wear resistance of parts in pipeline |
| CN110864989B (en) * | 2019-11-19 | 2021-01-12 | 上海市特种设备监督检验技术研究院 | Test platform and method for detecting wear resistance of parts in pipeline |
| CN116839651A (en) * | 2023-08-30 | 2023-10-03 | 沈阳国仪检测技术有限公司 | System for be used for testing pipeline detector spare part |
| CN116839651B (en) * | 2023-08-30 | 2023-11-17 | 沈阳国仪检测技术有限公司 | System for be used for testing pipeline detector spare part |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100462671C (en) | Laser outer diameter detecting instrument | |
| CN202486072U (en) | Sapphire crystal X-ray automatic orientation material bonding machine | |
| CN109060576A (en) | A kind of wear-resistant detection device of aircraft brake wheel | |
| CN103394441B (en) | Clearance between roll regulation system and control flow | |
| CN206248700U (en) | A kind of adjustable probe automatic detection device | |
| CN204730808U (en) | Adjustable caliper cylinder frock | |
| CN205685296U (en) | The device of centering is installed for equipment | |
| CN204788326U (en) | Depth of parallelism check out test set | |
| CN205718770U (en) | Bearing outer ring height dimension test measuring device | |
| CN105115470A (en) | Tool of quickly detecting unevenness of steel plate | |
| CN209512819U (en) | A kind of high-acruracy survey mechanism for measuring for verticality | |
| CN101865644A (en) | Multifunctional detector | |
| CN201615737U (en) | Multifunctional detector | |
| CN103743319A (en) | Manual detection device of automobile brake disc | |
| CN110986743A (en) | Automobile gear coaxiality detection device and system | |
| KR101453543B1 (en) | Vertical turning lathe having function of displaying center of turn table | |
| CN212903028U (en) | Beat detector of quick inspection concentricity | |
| CN109489613A (en) | A kind of high-acruracy survey mechanism for measuring for verticality | |
| CN213591134U (en) | Double-tip armature rotor roundness detection mechanism | |
| CN203298709U (en) | A connecting frame coaxiality detection apparatus | |
| CN207007136U (en) | A kind of sheet metal part thickness test equipment | |
| CN105066827A (en) | General spline M value detector | |
| CN208968408U (en) | A kind of hole location special gauge | |
| CN203236297U (en) | Sensing ring tracking device for rotary machine tool | |
| CN218034834U (en) | Long-distance guide rail precision detection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181221 |