CN208606924U - Torque test device - Google Patents
Torque test device Download PDFInfo
- Publication number
- CN208606924U CN208606924U CN201821302801.3U CN201821302801U CN208606924U CN 208606924 U CN208606924 U CN 208606924U CN 201821302801 U CN201821302801 U CN 201821302801U CN 208606924 U CN208606924 U CN 208606924U
- Authority
- CN
- China
- Prior art keywords
- pedestal
- rudder piece
- dial plate
- angle dial
- fixed
- 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.)
- Expired - Fee Related
Links
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- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The utility model discloses a kind of torque test devices, including pedestal, it is equipped on the right side of the upper surface of the pedestal and turns round bar fixing device, turning round bar fixing device includes turning round a fixed pedestal, turn round item, turn round a connecting shaft and angle indicator, the left side for turning round bar fixing device is equipped with angle dial plate mechanism, angle dial plate mechanism includes that angle dial plate is fixedly mounted with pedestal, angle dial plate cover board and angle dial plate, the left end for turning round a connecting shaft passes through angle dial plate and connects rudder piece connector, the rudder piece connector includes rudder piece cover plate of connector, rudder piece connector base, rudder piece clamps connecting rod axle bumper, rudder piece clamp clip, breaker strip and rudder piece clamp connecting rod.The torque test device can carry out the torsional test of rudder piece by the test mounting base for the different bores that change the outfit to A type bore, Type B bore and c-type bore aircraft steering engine；By replacing the torsion item of different torques, it is able to satisfy the torsional test of a variety of rudder pieces.
Description
Technical field
The utility model belongs to aircraft steering engine rudder piece torsional test technical field, and in particular to a kind of torsional test dress
It sets.
Background technique
When carrying out torsional test for the aircraft steering engine rudder piece of different bores in the past, it can all be made according to test block corresponding
Torque test device, torque test devices various types of in this way do not require nothing more than more parking spaces, and service efficiency
It is low.
Utility model content
The purpose of this utility model is to provide a kind of torque test devices, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the utility model provides the following technical solutions: a kind of torque test device, including pedestal,
It is equipped on the right side of the upper surface of the pedestal and turns round bar fixing device, torsion bar fixing device includes turning round a fixed pedestal, turning round item, turn round item company
Spindle and angle indicator, the right end turned round a fixed pedestal and be fixed on pedestal, a fixed pedestal of turning round connect torsion item
A connecting shaft is turned round in one end, the other end connection for turning round item, and angle indicator is connected to the upper surface for turning round a connecting shaft, turns round bar fixing device
Left side be equipped with angle dial plate mechanism, angle dial plate mechanism includes that angle dial plate is fixedly mounted with pedestal, angle dial plate cover board and angle table
Disk, the angle dial plate are fixedly mounted with the upper surface that pedestal is fixed on pedestal, and the side that angle dial plate is fixedly mounted with pedestal is equipped with angle dial plate
And fixed by angle dial plate cover board, the left end for turning round a connecting shaft passes through angle dial plate and connects rudder piece connector, the rudder piece
Connector includes rudder piece cover plate of connector, rudder piece connector base, rudder piece clamping connecting rod axle bumper, rudder piece clamp clip, buffering adhesive
Piece and rudder piece clamp connecting rod, the rudder piece connector base and rudder piece cover plate of connector and lock connection torsion item connection by screw
The left end of axis, the rudder piece clamp the two sides that rudder piece connector base is arranged in connecting rod axle bumper, and rudder piece clamp clip passes through rudder piece
Connecting rod is clamped to be fixed between rudder piece clamping connecting rod axle bumper.
Preferably, the medial surface of the rudder piece clamp clip is equipped with breaker strip.
Preferably, small aircraft installation pedestal, the small aircraft installation are equipped on the left of the upper surface of the pedestal
Small aircraft shell is fixed on pedestal, the side wall of the small aircraft shell is equipped with test steering wheel rudder piece, Miniature Vehicle
Device installation pedestal is fixed on the base by pedestal hole location, and pedestal hole location includes A type bore aircraft installation pedestal hole location, Type B
Bore aircraft installation pedestal hole location and c-type bore aircraft installation pedestal hole location, and respectively correspond installation A type bore aircraft
Installation pedestal, Type B bore aircraft installation pedestal and c-type bore aircraft installation pedestal.
The technical effect and advantage of the utility model: the torque test device is installed by the test for the different bores that change the outfit
Seat can carry out the torsional test of rudder piece to A type bore, Type B bore and c-type bore aircraft steering engine；By replacing different torques
Torsion item, be able to satisfy the torsional test of a variety of rudder pieces.
Detailed description of the invention
Fig. 1 is the configuration schematic diagram of the utility model；
Fig. 2 is the combining structure schematic diagram of the utility model；
Fig. 3 is the schematic diagram of base structure of the utility model；
Fig. 4 is that the installation pedestal of the utility model uses schematic diagram.
In figure: 1 pedestal, 21 are turned round a fixed pedestal, 22 torsion items, 23 torsion connecting shafts, 24 angle indicators, 31 angle dial plates and are consolidated
Pedestal, 32 angle dial plate cover boards, 33 angle dial plates, 41 rudder piece cover plate of connector, 42 rudder piece connector bases, 43 rudder pieces are filled to clamp
Connecting rod axle bumper, 44 rudder piece clamp clips, 45 breaker strips, 46 rudder pieces clamp 7 small aircraft installation pedestal of connecting rod, 71 A types
Bore aircraft installation pedestal, 72 Type B bore aircraft installation pedestals, 73 c-type bore aircraft installation pedestals, 81 A type mouths
Diameter aircraft installation pedestal hole location, 82 Type B bore aircraft installation pedestal hole locations, 83 c-type bore aircraft installation pedestal holes
Position.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The utility model provides a kind of torque test device as shown in Figs 1-4, including pedestal 1, the pedestal 1 it is upper
It is equipped on the right side of end face and turns round bar fixing device, turning round bar fixing device includes turning round a fixed pedestal 21, turning round item 22, turn round 23 and of a connecting shaft
Item 22 is turned round in angle indicator 24, the right end turned round a fixed pedestal 21 and be fixed on pedestal 1, torsion fixed pedestal 21 connection
One end, turn round item 22 the other end connection turn round a connecting shaft 23, angle indicator 24 be connected to turn round a connecting shaft 23 upper surface, turn round
The left side of bar fixing device is equipped with angle dial plate mechanism, and angle dial plate mechanism includes that angle dial plate is fixedly mounted with pedestal 31, angle dial plate
Cover board 32 and angle dial plate 33, the angle dial plate are fixedly mounted with the upper surface that pedestal 31 is fixed on pedestal 1, and angle dial plate is fixedly mounted with pedestal
31 side is equipped with angle dial plate 33 and is fixed by angle dial plate cover board 32, and the left end for turning round a connecting shaft 23 passes through angle dial plate
33 and rudder piece connector is connected, the rudder piece connector includes rudder piece cover plate of connector 41, rudder piece connector base 42, rudder piece folder
It is close to extension bar axle bumper 43, rudder piece clamp clip 44, breaker strip 45 and rudder piece and clamps connecting rod 46, the rudder piece connector base 42
The left end that a connecting shaft 23 is turned round in connection is locked by screw with rudder piece cover plate of connector 41, the rudder piece clamps connecting rod axle bumper 43
The two sides of rudder piece connector base 42 are set, and rudder piece clamp clip 44 is clamped connecting rod 46 and be fixed on rudder piece and clamped by rudder piece to be connected
Between extension bar axle bumper 43.
Specifically, the medial surface of the rudder piece clamp clip 44 is equipped with breaker strip 45.
Specifically, small aircraft installation pedestal 7 is equipped on the left of the upper surface of the pedestal 1, the small aircraft peace
Small aircraft shell 6 is fixed on dress pedestal 7, the side wall of the small aircraft shell 6 is equipped with test steering wheel rudder piece 5, small
Type aircraft installation pedestal 7 is fixed on pedestal 1 by pedestal hole location, and pedestal hole location includes A type bore aircraft installation pedestal
Hole location 81, Type B bore aircraft installation pedestal hole location 82 and c-type bore aircraft installation pedestal hole location 83, and respectively correspond peace
Fill A type bore aircraft installation pedestal 71, Type B bore aircraft installation pedestal 72 and c-type bore aircraft installation pedestal 73.
It is mounted on test device pedestal 1 with screw by a fixed pedestal 21 is turned round, then is installed with screw by item 22 is turned round first
On turning round a fixed pedestal 21, the insertion of 22 other end of item will be turned round and turned round in the slot of a connecting shaft 23, angle indicator 24 is put and uses spiral shell
Nail is fixed；
Angle dial plate is fixedly mounted with pedestal 31 to be installed on test device pedestal 1, angle dial plate 33 is then placed into angle
Dial plate is fixedly mounted on pedestal 31, is compressed with angle dial plate cover board 32；
Rudder piece cover plate of connector 41 and rudder piece connector base 42 are connected to screw and turned round in a connecting shaft 23；
Breaker strip 45 is glued on rudder piece clamp clip 44, clamps connecting rod 46 for two panels rudder piece clamp clip with rudder piece
44 connect together, and rudder piece, which clamps 46 two sides of connecting rod, positive/negative thread, and rotation rudder piece, which clamps connecting rod 46, can be such that rudder piece presss from both sides
The tight tightening of piece 44 is unclamped；43 one end of connecting rod axle bumper connection rudder piece is clamped with rudder piece and clamps connecting rod 46, and other end is fixed
In rudder piece connector base 42.
Finally, it should be noted that the above descriptions are merely preferred embodiments of the present invention, it is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic
It is equivalently replaced, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (3)
1. a kind of torque test device, including pedestal (1), it is characterised in that: be equipped on the right side of the upper surface of the pedestal (1) and turn round item
Fixed device, turning round bar fixing device includes turning round a fixed pedestal (21), turning round item (22), turn round a connecting shaft (23) and angle indicator
(24), item is turned round in the right end turned round a fixed pedestal (21) and be fixed on pedestal (1), torsion fixed pedestal (21) connection
(22) connecting shaft (23) are turned round in one end, the other end connection for turning round item (22), and angle indicator (24), which is connected to, turns round a connecting shaft
(23) upper surface, the left side for turning round bar fixing device are equipped with angle dial plate mechanism, and angle dial plate mechanism includes that angle dial plate is fixedly mounted with
Pedestal (31), angle dial plate cover board (32) and angle dial plate (33), the angle dial plate are fixedly mounted with pedestal (31) and are fixed on pedestal (1)
Upper surface, the side that angle dial plate is fixedly mounted with pedestal (31) is equipped with angle dial plate (33) and solid by angle dial plate cover board (32)
Fixed, the left end for turning round a connecting shaft (23) passes through angle dial plate (33) and connects rudder piece connector, and the rudder piece connector includes rudder
Piece cover plate of connector (41), rudder piece connector base (42), rudder piece clamp connecting rod axle bumper (43), rudder piece clamp clip (44), delay
It rushes film (45) and rudder piece clamps connecting rod (46), the rudder piece connector base (42) and rudder piece cover plate of connector (41) pass through
The left end of connecting shaft (23) is turned round in screw locking connection, and the rudder piece clamps connecting rod axle bumper (43) and is arranged at rudder piece connector bottom
The two sides of seat (42), rudder piece clamp clip (44) clamp connecting rod (46) by rudder piece and are fixed on rudder piece clamping connecting rod axle bumper (43)
Between.
2. a kind of torque test device according to claim 1, it is characterised in that: the inside of the rudder piece clamp clip (44)
Face is equipped with breaker strip (45).
3. a kind of torque test device according to claim 1, it is characterised in that: on the left of the upper surface of the pedestal (1)
Equipped with small aircraft installation pedestal (7), small aircraft shell (6) are fixed on the small aircraft installation pedestal (7),
The side wall of the small aircraft shell (6) is equipped with test steering wheel rudder piece (5), and small aircraft installation pedestal (7) passes through pedestal
Hole location is fixed on pedestal (1), and pedestal hole location includes A type bore aircraft installation pedestal hole location (81), Type B bore aircraft peace
Pedestal hole location (82) and c-type bore aircraft installation pedestal hole location (83) are filled, and respectively corresponds installation A type bore aircraft installation
Pedestal (71), Type B bore aircraft installation pedestal (72) and c-type bore aircraft installation pedestal (73).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821302801.3U CN208606924U (en) | 2018-08-14 | 2018-08-14 | Torque test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821302801.3U CN208606924U (en) | 2018-08-14 | 2018-08-14 | Torque test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208606924U true CN208606924U (en) | 2019-03-15 |
Family
ID=65680881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821302801.3U Expired - Fee Related CN208606924U (en) | 2018-08-14 | 2018-08-14 | Torque test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208606924U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110723312A (en) * | 2019-10-25 | 2020-01-24 | 北京机电工程研究所 | Steering engine loading device |
-
2018
- 2018-08-14 CN CN201821302801.3U patent/CN208606924U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110723312A (en) * | 2019-10-25 | 2020-01-24 | 北京机电工程研究所 | Steering engine loading device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190315 Termination date: 20200814 |