CN217637358U - Adjustable aircraft boresight device - Google Patents
Adjustable aircraft boresight device Download PDFInfo
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- CN217637358U CN217637358U CN202221059513.6U CN202221059513U CN217637358U CN 217637358 U CN217637358 U CN 217637358U CN 202221059513 U CN202221059513 U CN 202221059513U CN 217637358 U CN217637358 U CN 217637358U
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- tube device
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- mirror
- upper clamp
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Abstract
The utility model provides an adjustable airplane boresight device, which also comprises an upper clamp body, a mirror tube device, an adjusting mechanism and a lower clamp body; the airplane boresight device is hinged by the lower end of the upper clamp body and the upper end of the lower clamp body through an adjusting mechanism; the adjusting mechanism is connected with three screws; the mirror tube device is hinged on the upper clamp body; the lens tube device is sleeved with a lens tube, and the lens tube can rotate; a second adjusting screw is arranged on the mirror tube device, and a second spring nail is arranged at the other end of the second adjusting screw; the upper clamp body is provided with an adjusting screw I for abutting against the lower end of the lens tube device, and the upper clamp body is provided with a spring nail I for abutting against the upper end of the lens tube device; the middle sections of the two sides of the lower clamp body are provided with supporting rods; two ends of the bottom of the lower clamp body are provided with support legs; holes are arranged on the supporting legs. The utility model discloses can miniature regulation mirror pipe on laser mirror or the adjustment of the optic angle of controlling from top to bottom, simple structure is fit for off-site work, portable.
Description
Technical Field
The utility model belongs to the aviation aircraft maintenance device field, concretely relates to adjustable aircraft school target device.
Background
The aircraft boresight device is used for calibrating an aircraft weapon system, a fire control system, a reconnaissance pod and the like, belongs to a relatively important guarantee device, is special equipment used for boresight operation of military aircraft, is used for calibrating photoelectric and mechanical axes of the aircraft weapon system and other related airborne equipment relative to a reference axis, and realizes the work of checking the coordination relationship of the space axes, measuring initial deviation, correcting auxiliary deviation and the like.
The airplane needs to be installed and adjusted in the boresight process, most of the existing airplane boresight devices are of a single and fixed structure, can only adapt to the boresight work of a very small number of airplanes, and when the front and back boresight angles and the left and right boresight angles are different, the calibration work of an airplane weapon system, a fire control system, a detection pod and the like is difficult to realize due to the uniqueness of the boresight devices.
SUMMERY OF THE UTILITY MODEL
In view of the above, an object of the present invention is to provide a device capable of adjusting the target calibration up and down.
The utility model discloses a realize through following technical scheme:
an adjustable aircraft boresight device comprises a level gauge (the prior art is adopted) arranged on an upper clamp body; the adjustable airplane boresight device further comprises an upper clamp body, a mirror tube device, an adjusting mechanism and a lower clamp body; the airplane boresight device is hinged by the lower end of the upper clamp body and the upper end of the lower clamp body through an adjusting mechanism; the lower clamp body is U-shaped; the adjusting mechanism is connected with three screws, and a pressure spring is arranged on the left screw and the right screw and used for adjusting the upper clamp body to keep the upper clamp body horizontal; the mirror tube device is hinged on the upper clamp body; the lens tube device is sleeved with a lens tube, and the lens tube can rotate; a second adjusting screw is arranged on the mirror tube device, and a second spring nail is arranged at the other end of the second adjusting screw and used for adjusting left and right angle deviation of the mirror tube; the upper clamp body is provided with an adjusting screw I for abutting against the lower end of the lens tube device, and the upper clamp body is provided with a spring nail I for abutting against the upper end of the lens tube device and used for adjusting the vertical angle deviation of the lens tube device; the middle sections of the two sides of the lower clamp body are provided with supporting rods; two ends of the bottom of the lower clamp body are provided with support legs; holes are arranged on the supporting legs.
Further, in order to facilitate the use of operators, a hole position is arranged at the upper part of the lower clamp body.
Furthermore, a retainer is connected between the support legs through nuts.
The utility model has the advantages that:
the utility model discloses can miniature regulation mirror pipe on laser mirror or the adjustment of the optical lens angle of controlling from top to bottom, simple structure is fit for off-site work, simple structure, operation convenient to use, portable.
Drawings
The present invention will be described in further detail with reference to the accompanying drawings.
Fig. 1 is a schematic structural view of an adjustable type airplane boresight device of the present invention.
Fig. 2 is a local cross-sectional view of an adjustable aircraft boresight device in the utility model.
Shown in the figure: 1-adjusting a screw I; 101-spring nail one; 2-installing a fixture body; 3-a mirror tube device; 31-a lens tube; 4-adjusting a second screw; 41-spring nail II; 5-a level meter; 6-an adjusting mechanism; 7-connecting the clamp body; 8-a support bar; 9-a leg; 10-a nut; 11-a cage.
Detailed Description
The following description is given for illustrative embodiments of the present invention, and other advantages and effects of the present invention will be apparent to those skilled in the art from the disclosure of the present invention.
It should be understood that the drawings of the present application are only used to match the contents disclosed in the specification, so as to be known and read by those skilled in the art, and not to limit the practical limitations of the present invention, so that the present application does not have any technical significance, and any modification of the structure, change of the ratio relationship, or adjustment of the size should still fall within the scope of the present application without affecting the function and the achievable purpose of the present application. Meanwhile, the terms such as "upper", "lower", "left", "right", "middle", and the like used in the present specification are for convenience of description, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof may be considered as the scope of the present invention without substantial changes in the technical content.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art. It is to be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
As shown in fig. 1 and 2, an adjustable type airplane boresight device includes: the device comprises a first adjusting screw 1, a first spring nail 101, an upper clamp body 2, a mirror tube device 3, a mirror tube 31, a second adjusting screw 4, a second spring nail 41, a level gauge 5, an adjusting mechanism 6, a lower clamp body 7, a support rod 8, a support leg 9, a nut 10 and a retainer 11.
The aircraft target correcting device is formed by hinging an upper clamp body 2 and a lower clamp body 7 through an adjusting mechanism 6, the hinging parts of the adjusting mechanism 6 are fixedly connected through three side-by-side screws, and a pressure spring is arranged on the left screw and the right screw.
The upper clamp body 2 is provided with a level 5 of a conventional type on the market.
The lens tube device 3 is hinged to the inner side of the upper clamp body 2, and the lens tube 31 is sleeved on the lens tube device 3 and can rotate.
The adjusting screw I1 is in threaded connection with the upper clamp body 2, the screw head of the adjusting screw I penetrates through the upper clamp body 2 and abuts against the lower end of the lens tube device 3, the spring nail I101 is fixed on the upper clamp body 2, the head of the spring nail I penetrates through the upper clamp body 2 and abuts against the upper end of the lens tube device 3, and the structure is used for adjusting the up-and-down angle of the lens tube device 3.
The lens tube device 3 is connected with a second adjusting screw 4 through threads, the screw head of the second adjusting screw is abutted against the lens tube 31 and used for controlling the rotation of the lens tube 31, the second spring nail 41 is arranged opposite to the second adjusting screw 4, the head of the second spring nail is abutted against the other surface of the lens tube 31 where the screw head of the second adjusting screw 4 is located and used for controlling the lens tube 31 to rotate in the opposite direction, and the structure can be used for adjusting the left and right angles of the lens tube 31.
The lower clamp body 7 is U-shaped, the middle sections of two sides of the lower clamp body 7 are provided with support rods 8, two ends of the bottom of the lower clamp body 7 are provided with support legs 9, holes are formed in the support legs 9, and a retainer 11 is connected between the support legs 9 through screws 10.
The utility model discloses a theory of operation as follows:
firstly, taking down the retainer 11 and the nut 10, mounting the whole aircraft boresight device at the aircraft joint through hole positions at the support legs 9, screwing the nut 10, observing the T-shaped level 5 on the upper clamp body 2, transversely adjusting the T-shaped level 5 to be horizontal through the two support rods 8 and the nuts 10 at the support legs, and screwing the support rods 8 and the nuts 10;
secondly, rotating a middle nut of the adjusting mechanism 6 by using a tool, and longitudinally adjusting the level of the T-shaped level 5 by two pressure springs on screws on two sides of the adjusting mechanism 6;
and thirdly, rotating the adjusting screw I1 and the spring nail I101 to enable the laser mirror or the optical mirror on the mirror tube 31 to be capable of adjusting the angle up and down, rotating the adjusting screw II 4 and the spring nail II 41 to enable the laser mirror or the optical mirror on the mirror tube 31 to be capable of adjusting the angle left and right, and observing the division line of the target correcting mirror (optical mirror) and the cross mark on the target plate to measure and adjust the angle of the weapon axis deviation.
The protection scope of the present invention is not limited to the technical solution disclosed in the specific embodiment, and all the modifications, equivalent replacements, improvements, etc. made by the technical entity of the present invention to the above embodiments all fall into the protection scope of the present invention.
Claims (3)
1. An adjustable airplane boresight device comprises a level gauge (5) arranged on an upper clamp body (2); the method is characterized in that: comprises an upper clamp body (2), a tube device (3), an adjusting mechanism (6) and a lower clamp body (7); the airplane boresight device is hinged by an upper clamp body (2) and a lower clamp body (7) through an adjusting mechanism (6); the lower clamp body (7) is U-shaped; the adjusting mechanism (6) is connected by three screws, wherein the left screw and the right screw are provided with pressure springs; the mirror tube device (3) is hinged on the upper clamp body (2); the lens tube device (3) is sleeved with a lens tube (31), and the lens tube (31) can rotate; a second adjusting screw (4) is arranged on the mirror tube device (3), and a second spring nail (41) is arranged at the other end of the second adjusting screw (4) and is used for adjusting the left-right angle deviation of the mirror tube device (3); an adjusting screw I (1) is arranged on the upper clamp body (2) to abut against the lower end of the mirror tube device (3), and a spring nail I (101) is arranged on the upper clamp body (2) to abut against the upper end of the mirror tube device (3) and used for adjusting the vertical angle deviation of the mirror tube device (3); the middle sections of the two sides of the lower clamp body (7) are provided with supporting rods (8); two ends of the bottom of the lower clamp body (7) are provided with support legs (9); holes are arranged on the supporting legs (9).
2. The adjustable type airplane boresight device is characterized in that a hole position is formed in the upper portion of the lower clamp body (7).
3. The adjustable type airplane boresight device is characterized in that a retainer (11) is connected between the supporting legs (9) through a nut (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221059513.6U CN217637358U (en) | 2022-05-06 | 2022-05-06 | Adjustable aircraft boresight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221059513.6U CN217637358U (en) | 2022-05-06 | 2022-05-06 | Adjustable aircraft boresight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217637358U true CN217637358U (en) | 2022-10-21 |
Family
ID=83649703
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221059513.6U Active CN217637358U (en) | 2022-05-06 | 2022-05-06 | Adjustable aircraft boresight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217637358U (en) |
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2022
- 2022-05-06 CN CN202221059513.6U patent/CN217637358U/en active Active
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