CN205808389U - A kind of aircraft flat rudder face angle measurement unit - Google Patents
A kind of aircraft flat rudder face angle measurement unit Download PDFInfo
- Publication number
- CN205808389U CN205808389U CN201620658839.9U CN201620658839U CN205808389U CN 205808389 U CN205808389 U CN 205808389U CN 201620658839 U CN201620658839 U CN 201620658839U CN 205808389 U CN205808389 U CN 205808389U
- Authority
- CN
- China
- Prior art keywords
- sucker
- compasses cutter
- compasses
- cutter
- bandage
- 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- Withdrawn - After Issue
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- Force Measurement Appropriate To Specific Purposes (AREA)
Abstract
The utility model discloses a kind of aircraft flat rudder face angle measurement unit, including arch block, compasses cutter sucker, connect sheet, thin flat head rivet, straight-flanked ring, bandage, plastics day word button, cushion block, lateral angles sensor, vertical angular transducer and wire, lateral angles sensor levels is fixed on the inside of compasses cutter sucker, the inside of compasses cutter sucker is additionally provided with the fixed plate that vertical direction is installed, vertical angular transducer is vertically installed in fixed plate, connect sheet to be fixed on the upper surface of compasses cutter sucker, straight-flanked ring one end is arranged on connection sheet by thin flat head rivet, one end of bandage is sleeved on the other end of straight-flanked ring, plastics day, word button was arranged on bandage, cushion block is arranged on the inside of compasses cutter sucker.This utility model has the advantages such as reasonable in design, space availability ratio are high, easy to use, light weight, and size is little, it is simple to deposits, transport and uses, easy to loading and unloading, efficiently solves the problem that fixing difficulty installed by sensor, it is achieved that the measurement of angle.
Description
Technical field
This utility model relates to aeronautical product technical field of angle detection, and a kind of aircraft flat rudder face angle is surveyed
Amount device.
Background technology
At present, flying to join timing signal carrying out aircraft, internal field and outfield still use angle to the measurement of deflection angle of airplane control surface degree
Degree chi frock clamp, and visually measure after each rudder face is clamped.Owing to frock size is big, heavy, aircraft front flap,
The position that rear wing flap, the secondary flap, tailplane, vertical fin etc. need to be measured is more, and therefore installation difficulty result in rudder face angular surveying all
The most inconvenient.A kind of device that can conveniently carry out angular surveying of urgent needs.
Summary of the invention
In order to solve above-mentioned technical problem, this utility model provides a kind of aircraft flat rudder face angle measurement unit.
This utility model solves its technical problem and realizes by the following technical solutions:
A kind of aircraft flat rudder face angle measurement unit, including arch block, compasses cutter sucker, screw two, nut one, connects
Sheet, thin flat head rivet, straight-flanked ring, bandage, plastics day word are buckled, cushion block, lateral angles sensor, vertical angular transducer and lead
Line, described lateral angles sensor levels is fixed on the inside of compasses cutter sucker, and the inside of compasses cutter sucker is additionally provided with vertical side
To the fixed plate installed, described vertical angular transducer is vertically installed in fixed plate, connects sheet by screw two, nut one
Coordinating to be fixed on the upper surface of compasses cutter sucker, one end of straight-flanked ring is arranged on connection sheet by thin flat head rivet, ties up
One end of band is sleeved on the other end of straight-flanked ring, described plastics day word button be arranged on bandage, cushion block is arranged on compasses cutter and inhales
The inside of dish, arch block is arranged on the right side central of compasses cutter sucker, and wire passes with lateral angles sensor, vertical angle respectively
Sensor is drawn after being connected at arch block.This utility model lateral angles sensor, vertical angular transducer are sensor with data readout
Double-shaft tilt angle sensor, its measurement of dip angle scope is :-30 °～30 °, precision may be up to 0.01 °.Meet each rudder face of aircraft inclined
Gyration maximum magnitude-28 °～the requirement of 25 °, it is achieved that to horizontal tail or the angular surveying of vertical fin.
Described lateral angles sensor is fixed on the inside of compasses cutter sucker, screw by the cooperation of screw one, nut two
Circuit board copper pillar it is cased with on one.
The beneficial effects of the utility model are:
This utility model has the advantages such as reasonable in design, space availability ratio be high, easy to use, light weight, and size is little,
It is easy to deposit, transport and use.Meanwhile, easy to loading and unloading, efficiently solve the problem that fixing difficulty installed by sensor, it is achieved that angle
The measurement of degree.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is front view of the present utility model；
Fig. 2 is the plan structure schematic diagram that this utility model is connected with external receptor；
Fig. 3 is the I partial enlarged drawing of Fig. 1；
Fig. 4 is II partial enlarged drawing of Fig. 2.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and beneficial effect clearer, below in conjunction with accompanying drawing, to this
The preferred embodiment of utility model is described in detail, and is described further this utility model, to facilitate technical staff to manage
Solve.
As shown in Figures 1 to 4, a kind of aircraft flat rudder face angle measurement unit, including arch block 1, compasses cutter sucker 4, spiral shell
Follow closely 25, nut 1, connect sheet 7, thin flat head rivet 8, straight-flanked ring 9, bandage 10, plastics day word buckle 11, cushion block 12, lateral angles
Sensor 2, vertical angular transducer 15 and wire, described lateral angles sensor 2 is horizontally fixed on the interior of compasses cutter sucker 4
Portion, the inside of compasses cutter sucker 4 is additionally provided with the fixed plate 16 that vertical direction is installed, and described vertical angular transducer 15 is vertically-mounted
In fixed plate 16, connect sheet 7 by screw 25, the coordinating to be fixed on the upper surface of compasses cutter sucker 4 of nut 1, square
One end of shape ring 9 is arranged on connection sheet 7 by thin flat head rivet 8, and one end of bandage 10 is sleeved on the other end of straight-flanked ring 9
On, described plastics day word button 11 be arranged on bandage 10, cushion block 12 is arranged on the inside of compasses cutter sucker 4, and arch block 1 is arranged on
The right side central of compasses cutter sucker 4, wire be connected with lateral angles sensor 2, vertical angular transducer 15 respectively after from arch
Draw at block 1.This utility model lateral angles sensor 2, vertical angular transducer 15 sense for sensor with data readout double-shaft tilt angle
Device, its measurement of dip angle scope is :-30 °～30 °, precision may be up to 0.01 °.Meet aircraft each control surface deflection angle maximum model
Enclose-28 °～the requirement of 25 °, it is achieved that to horizontal tail or the angular surveying of vertical fin.
Described lateral angles sensor 2 is fixed on the inside of compasses cutter sucker 4 by the cooperation of screw 1, nut 2 13,
Circuit board copper pillar 14 it is cased with on screw 1.
The upper end of compasses cutter sucker 4 is provided with sucker and plays group handle 17, during use, when compasses cutter sucker 4 is placed on workpiece table
During face, operator can stir sucker and play group handle 17, make compasses cutter sucker 4 absorption tightly on the surface of the workpiece, and then
Lateral angles sensor 2, vertical angular transducer 15 is utilized to export in external receptor by the signal of detection by wire,
Achieve the measurement to angle.
Finally illustrating, preferred embodiment above is only in order to illustrate the technical solution of the utility model and unrestricted, to the greatest extent
This utility model is described in detail by pipe by above preferred embodiment, but those skilled in the art should manage
Solve, in the form and details it can be made various change, without departing from this utility model claims institute
The scope limited.
Claims (2)
1. an aircraft flat rudder face angle measurement unit, including arch block (1), compasses cutter sucker (4), connects sheet (7), flat head
(11), cushion block (12), lateral angles sensor (2), vertical angle buckled in rivet (8), straight-flanked ring (9), bandage (10), plastics day word
Sensor (15) and wire, it is characterised in that: described lateral angles sensor (2) is horizontally fixed on the interior of compasses cutter sucker (4)
Portion, the inside of compasses cutter sucker (4) is additionally provided with the fixed plate (16) that vertical direction is installed, and described vertical angular transducer (15) is erected
Directly being arranged in fixed plate (16), connect sheet (7) and be fixed on the upper surface of compasses cutter sucker (4), one end of straight-flanked ring (9) leads to
Crossing thin flat head rivet (8) to be arranged in connection sheet (7), one end of bandage (10) is sleeved on the other end of straight-flanked ring (9), described
Being arranged on plastics day word button (11) on bandage (10), cushion block (12) is arranged on the inside of compasses cutter sucker (4), and arch block (1) is pacified
Be contained in the right side central of compasses cutter sucker (4), wire respectively with lateral angles sensor (2), vertical angular transducer (15) phase
Draw from arch block (1) after Lian.
A kind of aircraft flat rudder face angle measurement unit the most according to claim 1, it is characterised in that: described lateral angles passes
Sensor (2) is fixed on the inside of compasses cutter sucker (4), the upper set of screw one (3) by the cooperation of screw one (3), nut two (13)
There is circuit board copper pillar (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658839.9U CN205808389U (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft flat rudder face angle measurement unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658839.9U CN205808389U (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft flat rudder face angle measurement unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205808389U true CN205808389U (en) | 2016-12-14 |
Family
ID=57512261
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620658839.9U Withdrawn - After Issue CN205808389U (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft flat rudder face angle measurement unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205808389U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106017395A (en) * | 2016-06-28 | 2016-10-12 | 国营芜湖机械厂 | Aircraft horizontal rudder surface angle measuring device |
-
2016
- 2016-06-28 CN CN201620658839.9U patent/CN205808389U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106017395A (en) * | 2016-06-28 | 2016-10-12 | 国营芜湖机械厂 | Aircraft horizontal rudder surface angle measuring device |
| CN106017395B (en) * | 2016-06-28 | 2019-04-19 | 国营芜湖机械厂 | A kind of flat rudder face angle measurement unit of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161214 Effective date of abandoning: 20190419 |
|
| AV01 | Patent right actively abandoned |