CN201971164U - Eye position adjusting device for airplane - Google Patents
Eye position adjusting device for airplane Download PDFInfo
- Publication number
- CN201971164U CN201971164U CN 201120109767 CN201120109767U CN201971164U CN 201971164 U CN201971164 U CN 201971164U CN 201120109767 CN201120109767 CN 201120109767 CN 201120109767 U CN201120109767 U CN 201120109767U CN 201971164 U CN201971164 U CN 201971164U
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- eye position
- type frame
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- site
- airplane
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Abstract
The utility model provides an eye position adjusting device for an airplane, which is convenient for a pilot to determine the deviation between an eye position point of the driver and an eye position point designed in a control cabin. The eye position adjusting device adopts the technical scheme that the eye position adjusting device for the airplane comprises a support plate, a circular-arc scale plate and a T-shaped frame, wherein the T-shaped frame consists of a support rod and a crossed cross-shaped rod, the circular-arc scale plate and the T-shaped frame are installed on the support plate, and the T-shaped frame is positioned at a cross point of the horizontal extension line of the eye position point designed in the control cabin and the symmetrical surface of the airplane. The eye position adjusting device is applicable to airplanes with non-section pilot seat adjustment, and simultaneously is convenient for the section pilot seat adjustment, so that the pilot can adjust the self eye position point more accurately. Compared with the existing eye position adjusting device for the airplane, the device is suitable for the airplane with non-section pilot seat adjustment, and is convenient for the section pilot seat adjustment, so that the pilot can adjust the self eye position point more accurately.
Description
Technical field
The utility model relates to a kind of aircraft eye position setting device.
Background technology
For existing eye position setting device, because the driver's seat regulated quantity is limited, therefore when the chaufeur of different builds is adjusted seat, having some chaufeurs can't be with reference sphere and alignment with the ball furnishing one straight line of its eyes sight line with setting device front and back, eye position, as shown in Figure 1, for this kind situation, existing setting device can't provide the deviation size in design eye site of eye site and the driving compartment of different chaufeurs.
Summary of the invention
Can't provide the deficiency of deviation size in the design eye site of the eye position of different chaufeurs and driving compartment at existing aircraft eye position setting device, the utility model provides a kind of aircraft eye position setting device that makes things convenient for the deviation size in the design eye site that chaufeur determines its site and driving compartment.The technical scheme that the utility model is taked is: a kind of aircraft eye position setting device, comprise supporting plate, the circular arc scaleplate, T type frame, T type frame is made up of a strut bar and the cross rod that intersects, circular arc scaleplate and T type frame are installed on the supporting plate, and T type chord position is in the horizontal extended line in design eye site and the aircraft plane of symmetry intersection point place of driving compartment.
Further, for better implement the utility model, be carved with scale on the above-mentioned circular arc scaleplate, scale center, T type frame and driver and copilot design eye site are in same straight line.
Further, for better implement the utility model, above-mentioned T type frame is to the distance and ratio corresponding driver's seat horizontal unit regulated quantity and the minimum scale ratio of T type frame to the distance in design eye site of circular arc scaleplate.
By design, make aircraft eye position setting device can finish the job task that it is born, satisfied the installation requirement of task device.Compare with existing aircraft eye position setting device, this device is applicable to that not having joint regulates the driver's seat aircraft, is convenient to have joint to regulate the more accurate eye site that must regulate oneself of driver's seat chaufeur simultaneously.
Description of drawings
Fig. 1 is existing aircraft eye position setting device front view and birds-eye view, wherein 1: alignment with the ball, 2: reference sphere, 3: supporting plate;
Fig. 2 is the utility model front view and birds-eye view, wherein 1: scale, 2: circular arc scaleplate, 3: supporting plate, 4:T type frame;
Fig. 3 for hypothesis chaufeur eye site partially before the time situation, wherein 5: a site of chaufeur, 6: design-calculated eye site, 7: the position of T type frame on scale that chaufeur is seen.
The specific embodiment
Describe the utility model in detail below in conjunction with Figure of description, please refer to Figure of description 2, a kind of aircraft eye position setting device, comprise supporting plate 3, circular arc scaleplate 1, T type frame 4, T type frame 4 is made up of a strut bar and the cross rod that intersects, circular arc scaleplate 1 is installed on the supporting plate 3 with T type frame 4, and T type frame 4 is positioned at the horizontal extended line in design eye site and the aircraft plane of symmetry intersection point place of driving compartment.
Be carved with scale on the circular arc scaleplate 1, scale center, T type frame and driver and copilot design eye site are in same straight line.T type frame 4 is to the distance and ratio corresponding driver's seat horizontal unit regulated quantity and the minimum scale ratio of T type frame 4 to the distance in design eye site of circular arc scaleplate 1.
In installation process, at first determine the position of T type frame 4, T type frame 4 needs on the horizontal extended line in design eye site and aircraft plane of symmetry intersection point of driving compartment, and guarantee that it is within the field range of chaufeur, consider the driving compartment space structure simultaneously, make T type frame 4 and driving compartment structure keep suitable distance, so that the installation of circular arc scaleplate 1.T type frame 4 and circular arc scaleplate 1 are fixed on the supporting plate 3.Be carved with scale on the circular arc scaleplate 1, scale center-point, T type frame 4 and chaufeur design eye site in-line, the minimum scale of scale is decided according to resolution of eye, and T type frame 4 is to the distance and ratio corresponding driver's seat horizontal unit regulated quantity and the minimum scale ratio of T type frame 4 to the distance in design eye site of circular arc scaleplate 1.
In using the utility model process, when driver's observation when T type frame 4 is in the scale center, a site of chaufeur overlaps with the design eye site of driving compartment.If driver's observation arrives T type frame 4 not when the scale center, the eye site that chaufeur is described does not overlap with design eye site, shown in Figure of description 3: the eye site 5 of supposing chaufeur is more forward than the position in design-calculated eye site 6, then the scale center-point is not just dropped in the position of T type frame on scale seen of chaufeur, but has dropped on a little on 7.T type frame was projected in scale on the circular arc scaleplate and promptly put 7 and just represented the deviation size in eye site 5 with the design eye site 6 of driving compartment of chaufeur with the distance of scale center-point this moment, so that chaufeur is adjusted a site faster.
Compare with existing aircraft eye position setting device, the utility model is applicable to the aircraft that the driver's seat adjustment amount is limited, be convenient to chaufeur and regulate the eye site of oneself more accurately, and deviation clear and design eye site.
Claims (3)
1. aircraft eye position setting device, comprise supporting plate, the circular arc scaleplate, it is characterized in that: also comprise T type frame, T type frame is made up of a strut bar and the cross rod that intersects, circular arc scaleplate and T type frame are installed on the supporting plate, and T type chord position is in driving compartment design eye horizontal extended line in site and aircraft plane of symmetry intersection point place.
2. aircraft eye according to claim 1 position setting device is characterized in that: be carved with scale on the circular arc scaleplate, scale center, T type frame and driver and copilot design eye site are in same straight line.
3. aircraft eye according to claim 2 position setting device is characterized in that: T type frame is to the distance and ratio corresponding driver's seat horizontal unit regulated quantity and the minimum scale ratio of T type frame to the distance in design eye site of circular arc scaleplate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120109767 CN201971164U (en) | 2011-04-15 | 2011-04-15 | Eye position adjusting device for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120109767 CN201971164U (en) | 2011-04-15 | 2011-04-15 | Eye position adjusting device for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201971164U true CN201971164U (en) | 2011-09-14 |
Family
ID=44576268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120109767 Expired - Fee Related CN201971164U (en) | 2011-04-15 | 2011-04-15 | Eye position adjusting device for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201971164U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104044750A (en) * | 2014-06-12 | 2014-09-17 | 中国商用飞机有限责任公司 | Auxiliary positioning device for designing eye position of cockpit |
| CN111301689A (en) * | 2020-02-12 | 2020-06-19 | 中国商用飞机有限责任公司 | System and method for intelligently adjusting eye position of pilot |
-
2011
- 2011-04-15 CN CN 201120109767 patent/CN201971164U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104044750A (en) * | 2014-06-12 | 2014-09-17 | 中国商用飞机有限责任公司 | Auxiliary positioning device for designing eye position of cockpit |
| CN104044750B (en) * | 2014-06-12 | 2016-01-27 | 中国商用飞机有限责任公司 | Auxiliary positioning device for designing eye position of cockpit |
| CN111301689A (en) * | 2020-02-12 | 2020-06-19 | 中国商用飞机有限责任公司 | System and method for intelligently adjusting eye position of pilot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110914 Termination date: 20170415 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |