CN209617538U - A kind of Small General Aircraft wing measuring tool - Google Patents
A kind of Small General Aircraft wing measuring tool Download PDFInfo
- Publication number
- CN209617538U CN209617538U CN201822077427.8U CN201822077427U CN209617538U CN 209617538 U CN209617538 U CN 209617538U CN 201822077427 U CN201822077427 U CN 201822077427U CN 209617538 U CN209617538 U CN 209617538U
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- China
- Prior art keywords
- set square
- ruler
- aircraft wing
- measuring tool
- small general
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- 238000005259 measurement Methods 0.000 claims abstract description 17
- 238000004441 surface measurement Methods 0.000 claims abstract description 8
- 238000010276 construction Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000002459 sustained Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances data:image/svg+xml;base64,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 data:image/svg+xml;base64,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 O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Abstract
The utility model provides a kind of Small General Aircraft wing measuring tool, it includes horizontal measuring instrument, aircraft wing upper surface measurement point and height measuring device, the height measuring device includes set square and the ruler on the set square is arranged in by shaft, the triangle plate shape is isosceles triangle, groove is set on the set square bottom edge, the equivalent width that the width and groove of the ruler open up, providing holes A on the upside of the set square, providing holes B on the upside of the ruler, the internal diameter of the hole A and the internal diameter of hole B are all larger than the outer diameter of shaft, the utility model has measurement accurate, the characteristics of convenient reading.
Description
Technical field
The utility model is specifically related to a kind of Small General Aircraft wing measuring tool, belongs to the manufacturing inspection of general-purpose aircraft
Field.
Background technique
During measuring Small General Aircraft, frequently with means be by level and straight steel ruler by airframe tune
After whole level, to the measurement point of wing lower surface, accurate data can be read directly, when the measurement point of measurement upper surface of the airfoil
When, since there are certain gradients for upper surface of the airfoil, when by straight steel ruler adjustment with fuselage construction horizontal plane, measurement is time-consuming
Arduously.
Utility model content
The purpose of the utility model is to overcome the defect of the prior art, provide that a kind of measurement is accurate, convenient reading it is small
Type general-purpose aircraft wing measuring tool.
To achieve the goals above, the technical solution that the utility model is taken is as follows:
A kind of Small General Aircraft wing measuring tool comprising horizontal measuring instrument, aircraft wing upper surface measurement point A with
And height measuring device, the height measuring device include set square and are arranged in by shaft straight on the set square
Ruler, the triangle plate shape are isosceles triangle, groove are arranged on the set square bottom edge, width and the groove of the ruler are opened
If equivalent width, providing holes A on the upside of the set square, the internal diameter of providing holes B, the hole A and hole B's is interior on the upside of the ruler
Diameter is all larger than the outer diameter of shaft.
Further, the horizontal measuring instrument model uses DS05.
Further, scale is arranged in the downside of the ruler.
Further, the shaft is fixedly connected with handle.
Compared with prior art, it is had the beneficial effect that acquired by the utility model:
The utility model carries out auxiliary adjustment level to fuselage construction horizontal plane by horizontal measuring instrument, utilizes height
Specified point and fuselage construction horizontal plane relative position difference in height on measuring device survey aircraft wing measure easy to use, meter
Number is accurate.
The set square of the height measuring device of the utility model is isosceles triangle, and after holding handle, set square is in weight
Under power effect, the inside sideline of the side line of ruler and the groove of set square downward vertically, is then aligned, at this time by bottom edge automatically
It can guarantee that ruler is in a vertical state, record aircraft wing upper surface measurement point and fuselage construction horizontal plane are read in measurement
Between difference in height, measurement data is accurate, and measure it is convenient.
Detailed description of the invention
It is attached that FIG. 1 is a schematic structural view of the utility model；
Attached drawing 2 is the structural schematic diagram of the utility model set square；
Attached drawing 3 is the structural schematic diagram of the utility model ruler；
Wherein, 1, horizontal measuring instrument, 2, aircraft wing upper surface measurement point, 3, hole B, 4, set square, 5, shaft, 6, straight
Ruler, 7, groove, 8, hole A.
Specific embodiment
Further details of narration is carried out to the utility model below in conjunction with attached drawing.
As shown in Fig. 1, the utility model provides a kind of Small General Aircraft wing measuring tool comprising horizontal measurement
Instrument 1, aircraft wing upper surface measurement point 2 and height measuring device, the height measuring device include set square 4 and pass through
Shaft 5 is arranged in the ruler 6 on the set square 4, and 4 shape of set square is isosceles triangle, on 4 bottom edge of set square
Setting groove 7, the equivalent width that the width and groove 7 of the ruler 6 open up, the 4 upside providing holes A8 of set square are described straight
6 upside providing holes B3 of ruler, the internal diameter of the hole A8 and the internal diameter of hole B3 are all larger than the outer diameter of shaft 5, and the utility model passes through water
Flat measuring instrument 1 adjusts level to fuselage construction horizontal plane, utilizes the specified point on height measuring device survey aircraft wing
With fuselage construction horizontal plane relative position difference in height, measurement is easy to use, and it is accurate to count.
1 model of horizontal measuring instrument uses DS05, and scale is arranged in the downside of the ruler 6, and the shaft 5 and handle are solid
The set square 4 of fixed connection, height measuring device is isosceles triangle, after holding handle, set square 4 under the effect of gravity, bottom
The inside sideline of the side line of ruler 6 and the groove 7 of set square 4 downward vertically, is then aligned by side automatically, can guarantee at this time
Ruler 6 is in a vertical state, and the number between record aircraft wing upper surface measurement point 2 and fuselage construction horizontal plane is read in measurement
Value, measurement data is accurate, and measures conveniently.
The present apparatus is suitable for biplane, and there are the measurement point of 4 leveling fuselages in fuselage two sides, and the fuselage construction horizontal plane is
To be adjusted to the plane formed after sustained height with jack cooperation 4 measurement points of fine tuning under level meter and fuselage, the survey on wing
Amount point is all the relative position surveyed with the fuselage construction horizontal plane, i.e. height difference.
The course of work is as follows:
Fuselage construction horizontal plane is leveled by horizontal measuring instrument 1, holds handle, set square 4 is made in gravity
Under, the inside sideline of the side line of ruler 6 and the groove 7 of set square 4 downward vertically, is then aligned, at this time by bottom edge automatically
I.e. can guarantee ruler 6 it is in a vertical state, measurement read record aircraft wing upper surface measurement point 2 and fuselage construction horizontal plane it
Between numerical value h1, measurement data is accurate, and measure it is convenient.
Embodiment described above is only the preferred embodiment of the utility model, and the not feasible implementation of the utility model
Exhaustion.For persons skilled in the art, under the premise of without departing substantially from the utility model principle and spirit, it is made
Any obvious change out, should all be contemplated as falling within the claims of the utility model.
Claims (4)
1. a kind of Small General Aircraft wing measuring tool, which is characterized in that it includes horizontal measuring instrument (1), on aircraft wing
Surface measurement point (2) and height measuring device, the height measuring device include set square (4) and are set by shaft (5)
The ruler (6) on the set square (4) is set, set square (4) shape is isosceles triangle, set square (4) bottom edge
Upper setting groove (7), the equivalent width that width and groove (7) of the ruler (6) open up, set square (4) upside setting
Hole A(8), providing holes B(3 on the upside of the ruler (6)), the hole A(8) internal diameter and hole B(3) internal diameter be all larger than shaft (5)
Outer diameter.
2. a kind of Small General Aircraft wing measuring tool according to claim 1, which is characterized in that the horizontal measurement
Instrument (1) model uses DS05.
3. a kind of Small General Aircraft wing measuring tool according to claim 1, which is characterized in that the ruler (6)
Downside be arranged scale.
4. a kind of Small General Aircraft wing measuring tool according to claim 1, which is characterized in that the shaft (5)
It is fixedly connected with handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822077427.8U CN209617538U (en) | 2018-12-12 | 2018-12-12 | A kind of Small General Aircraft wing measuring tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822077427.8U CN209617538U (en) | 2018-12-12 | 2018-12-12 | A kind of Small General Aircraft wing measuring tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209617538U true CN209617538U (en) | 2019-11-12 |
Family
ID=68445518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822077427.8U Active CN209617538U (en) | 2018-12-12 | 2018-12-12 | A kind of Small General Aircraft wing measuring tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209617538U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607050A (en) * | 2020-12-24 | 2021-04-06 | 中航贵州飞机有限责任公司 | Rechargeable type luminous measuring scale for measuring level of airplane |
-
2018
- 2018-12-12 CN CN201822077427.8U patent/CN209617538U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607050A (en) * | 2020-12-24 | 2021-04-06 | 中航贵州飞机有限责任公司 | Rechargeable type luminous measuring scale for measuring level of airplane |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |