CN217918464U - External environment framing equipment for airplane - Google Patents

Abstract

The utility model discloses an external environment viewing device is used to aircraft, including viewing device and mount, viewing device sets up the bottom with the mount, viewing device's top fixedly connected with limit slide, the bottom of mount is equipped with spacing spout, the outer wall and the limit slide inner wall sliding connection of spacing spout, viewing device's one end fixedly connected with mounting bracket. Through setting up protection frame and ejector pad, will promote the protection frame and insert the sliding tray inner wall, make the small opening coincide with the spread groove each other, drive the clearance hair pad and clean the clearance to the lens this moment, thereby later promote spacing slider and insert spacing spout inner wall and promote the ejector pad card under the effect of first spring and go into the draw-in groove inner wall and go on installing fixed while mount to the view finding equipment and fix at the sliding tray inner wall to the protection frame, when the lens of the convenient view finding equipment carries out effective protection, make things convenient for the dismouting of view finding equipment, effective lifting means's operability and practicality.

Description

External environment framing equipment for airplane

Technical Field

The utility model relates to an aircraft viewfinder equipment technical field specifically is an aircraft is with external environment viewfinder equipment.

Background

The main function of the viewfinder is to view the shot scenery when shooting by digital cameras and digital video cameras, namely to view the scenery, and in order to shoot more high-altitude overhead-view pictures, the viewfinder is installed on the airplane, thereby carrying out all-directional overhead-view framing on the ground.

But the aircraft that uses at present uses external environment equipment of finding a view, often directly hang and use in the aircraft outside, because external environment is complicated, has a large amount of dust impurities, can long-term adhesion outside the lens, causes the corruption, and the protectiveness is poor, leads to finding a view the effect poor, and the dismouting and the electric connection of the equipment of finding a view simultaneously waste time and energy inefficiency, and the practicality is poor.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an external environment viewing equipment for aircraft to solve the external environment viewing equipment for aircraft of the present use that proposes in the above-mentioned background art, often directly hang and lean on and use in the aircraft outside, because the external environment is complicated, there are a large amount of dust impurities, can adhere for a long time in the lens outside, cause the corruption, the protectiveness is poor, lead to finding a view the effect poor, the while viewing equipment dismouting waste time and energy inefficiency, the poor problem of practicality.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an external environment viewing device for aircraft, includes viewing device and mount, viewing device sets up the bottom with the mount, viewing device's top fixedly connected with limit slide, the bottom of mount is equipped with limit slide, limit slide's outer wall and limit slide inner wall sliding connection, viewing device's one end fixedly connected with mounting bracket, the top of mount is equipped with first mounting groove, the inner wall fixedly connected with fixed establishment of first mounting groove, fixed establishment's inboard is equipped with the spout, the first spring of inner wall fixedly connected with of spout, the inner wall sliding connection of spout has the ejector pad, one side of ejector pad and the one end fixed connection of first spring, viewing device's top is equipped with the sliding tray, the inner wall bottom sliding connection of sliding tray has the protection frame, one side of protection frame is equipped with the small opening, one side fixedly connected with of protection frame clears up the hair pad, the bottom fixedly connected with second spring of protection frame.

Preferably, the inside of mounting bracket is equipped with the spread groove, spread groove and the mutual through connection of sliding tray, the inboard fixedly connected with lens of mounting bracket.

Preferably, one side of the limiting slide block is provided with a clamping groove, and the inner wall of the clamping groove is matched with the outer wall of the push block.

Preferably, the top end of the fixing frame is fixedly connected with two connecting seats.

Preferably, the top of mount is equipped with the second mounting groove, the inner wall fixedly connected with electric connection block of second mounting groove, the top of viewing equipment is equipped with the third mounting groove, the inner wall fixedly connected with electric connection seat of third mounting groove.

Preferably, the inside fixedly connected with of electrical connection block goes up the connecting block, go up the first electrical connection line of top fixedly connected with of connecting block, the bottom of going up the connecting block is equipped with the electrical connection groove.

Preferably, the inboard of electric connection seat is equipped with the spacing groove, the inner wall sliding connection of spacing groove has the electric connection head, the inner wall fixedly connected with third spring of spacing groove, the bottom fixedly connected with second connecting wire of electric connection head, the second connecting wire passes through electric connection with the equipment of looking a view, first electric connection wire passes through electric connection with the aircraft.

Compared with the prior art, the beneficial effects of the utility model are that:

1. through the arrangement of the protective frame and the push block, the protective frame is pushed to be inserted into the inner wall of the sliding groove, so that the leaking groove and the connecting groove are superposed with each other, the cleaning matting is driven to clean the lens at the moment, then the limit slide block is pushed to be inserted into the inner wall of the limit sliding groove, the push block is pushed to be clamped into the inner wall of the clamping groove under the action of the first spring, the view finding equipment is installed and fixed by the fixing frame, the protective frame is fixed on the inner wall of the sliding groove, the lens of the view finding equipment is conveniently and effectively protected, the view finding equipment is convenient to disassemble and assemble, and the operability and practicability of the equipment are effectively improved;

2. through setting up electrical connection block and electrical connection seat, when with view finding equipment and mount fixed connection, electrical connection head card income electrical connection groove inner wall under the effect of third spring this moment to make view finding equipment carry out electric connection through electrical connection block and aircraft, thereby supply power to view finding equipment, thereby conveniently carry out the outage operation of supplying power to view finding equipment, the convenience that lifting means used.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

fig. 2 is a schematic diagram of the explosion structure of the present invention;

FIG. 3 is a schematic structural view of the viewfinder apparatus of the present invention;

FIG. 4 is a schematic view of the protective frame of the present invention;

fig. 5 is a schematic view of the electrical connection seat of the present invention.

In the figure: 1. a viewing device; 2. a fixed mount; 3. a mounting frame; 4. a first mounting groove; 5. a fixing mechanism; 6. a chute; 7. a push block; 8. a first spring; 9. a limiting chute; 10. a sliding groove; 11. a protective frame; 12. a second spring; 13. cleaning the hair pad; 14. a leak groove; 15. connecting grooves; 16. a lens; 17. a second mounting groove; 18. an electrical connection block; 19. a connecting seat; 20. a third mounting groove; 21. an electrical connection seat; 22. a limiting slide block; 23. a card slot; 24. an upper connecting block; 25. electrically connecting the grooves; 26. a first electrical connection line; 27. a limiting groove; 28. a third spring; 29. an electrical connector; 30. and a second connecting line.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-5, the present invention provides a technical solution: the utility model provides an external environment equipment of finding a view for aircraft, including finding a view equipment 1 and mount 2, finding a view equipment 1 sets up the bottom with mount 2, the top fixedly connected with limit slide block 22 of finding a view equipment 1, the bottom of mount 2 is equipped with limit chute 9, limit chute 9's outer wall and limit slide block 22 inner wall sliding connection, the one end fixedly connected with mounting bracket 3 of finding a view equipment 1, the top of mount 2 is equipped with first mounting groove 4, the inner wall fixedly connected with fixed establishment 5 of first mounting groove 4, the inboard of fixed establishment 5 is equipped with spout 6, the first spring 8 of inner wall fixedly connected with of spout 6, the inner wall sliding connection of spout 6 has ejector pad 7, one side of ejector pad 7 and first spring 8's one end fixed connection, the top of finding a view equipment 1 is equipped with sliding tray 10, the inner wall bottom sliding connection of sliding tray 10 has protection frame 11, one side of protection frame 11 is equipped with leak groove 14, one side fixedly connected with clearance cushion 13 of protection frame 11, the bottom fixedly connected with second spring 12 of protection frame 11, when using, after taking out view equipment 1, promote the sliding tray 11 to insert sliding groove 10, make things convenient for inner wall and clean up the inner wall 16 the inner wall of the effective clearance cushion of the inner wall of pushing away of the inner wall of the installation of the push away of the inner wall of the effective clearance of the push away of the slide block 16, thereby the effective clearance of the inner wall of the push-down slide block 16 push away of the slide block that the installation slide block 16 push away of the installation after the installation of the slide block 16 push away the installation of the slide block carries out the installation of the slide groove 16, the installation of the slide block 16, the installation, the push away the installation of the slide groove 16.

The inboard of mounting bracket 3 is equipped with spread groove 15, and spread groove 15 and sliding tray 10 are through connection each other, and the inboard fixedly connected with lens 16 of mounting bracket 3, one side of limit slide 22 are equipped with draw-in groove 23, the inner wall of draw-in groove 23 and the outer wall phase-match of ejector pad 7, the top fixedly connected with connecting seat 19 of mounting bracket 2, and the quantity of connecting seat 19 sets up to two.

The top of mount 2 is equipped with second mounting groove 17, the inner wall fixedly connected with electrical connection block 18 of second mounting groove 17, the top of finder equipment 1 is equipped with third mounting groove 20, the inner wall fixedly connected with electrical connection seat 21 of third mounting groove 20, connecting block 24 on the inside fixedly connected with of electrical connection block 18, the first electrical connection line 26 of top fixedly connected with of going up connecting block 24, the bottom of going up connecting block 24 is equipped with electrical connection groove 25, the inboard of electrical connection seat 21 is equipped with spacing groove 27, the inner wall sliding connection of spacing groove 27 has electrical connector 29, the inner wall fixedly connected with third spring 28 of spacing groove 27, the bottom fixedly connected with second connecting line 30 of electrical connector 29, second connecting line 30 passes through electrical connection with finder equipment 1, first electrical connection line 26 passes through electrical connection with the aircraft, in the use, when finder equipment 1 and mount 2 fixed connection, electrical connector 29 blocks into electrical connection groove 25 inner wall under the effect of third spring 28 this moment, thereby make finder equipment 1 carry out electrical connection with the aircraft through electrical connection, thereby supply power to equipment 1, thereby supply the outage operation to convenience.

The working principle is as follows: when using, to promote protection frame 11 and insert sliding tray 10 inner wall, make small opening 14 and spread groove 15 coincide each other, drive clearance hair pad 13 and clean the clearance to lens 16 this moment, later promote spacing slider 22 to insert spacing spout 9 inner wall and promote ejector pad 7 card under the effect of first spring 8 and go into draw-in groove 23 inner wall thereby fix the installation of viewing equipment 1 and fix simultaneously mount 2 fixes at sliding tray 10 inner wall to protection frame 11, when conveniently carrying out effective protection to viewing equipment 1's lens 16, make things convenient for viewing equipment 1's dismouting, when with viewing equipment 1 and mount 2 fixed connection, electric connector 29 card goes into spread groove 25 inner wall under the effect of third spring 28 this moment, thereby make viewing equipment 1 carry out electric connection through electric connection piece 18 and aircraft, thereby supply power to viewing equipment 1, thereby make things convenient for carrying out the power supply outage operation to viewing equipment 1, just so accomplish the use of whole structure.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides an aircraft is with outside environment framing equipment, includes framing equipment (1) and mount (2), its characterized in that: the utility model discloses a novel electronic viewfinder, including frame (1), frame (11), the bottom of viewing equipment (1) setting and mount (2), the top fixedly connected with limit slide (22) of viewing equipment (1), the bottom of mount (2) is equipped with limit chute (9), the outer wall and limit slide (22) inner wall sliding connection of limit chute (9), the one end fixedly connected with mounting bracket (3) of viewing equipment (1), the top of mount (2) is equipped with first mounting groove (4), the inner wall fixedly connected with fixed establishment (5) of first mounting groove (4), the inboard of fixed establishment (5) is equipped with spout (6), the first spring of inner wall fixedly connected with (8) of spout (6), the inner wall sliding connection of spout (6) has ejector pad (7), the one side of ejector pad (7) and the one end fixed connection of first spring (8), the top of viewing equipment (1) is equipped with sliding tray (10), the inner wall bottom sliding connection of sliding tray (10) has protection frame (11), one side of protection frame (11) is equipped with hourglass groove (14), one side of protection frame (11) is fixed up and is cleared up the hair and is connected with second spring (12).

2. An external environment viewing device for an aircraft according to claim 1, wherein: the inboard of mounting bracket (3) is equipped with spread groove (15), spread groove (15) and sliding tray (10) link up each other and are connected, the inboard fixedly connected with lens (16) of mounting bracket (3).

3. An external environment viewing device for an aircraft according to claim 2, wherein: one side of the limiting slide block (22) is provided with a clamping groove (23), and the inner wall of the clamping groove (23) is matched with the outer wall of the push block (7).

4. An external environment viewing device for an aircraft according to claim 3, wherein: the top end of the fixing frame (2) is fixedly connected with two connecting seats (19), and the number of the connecting seats (19) is two.

5. An external environment viewing device for an aircraft according to claim 4, wherein: the top of mount (2) is equipped with second mounting groove (17), the inner wall fixedly connected with electric connection piece (18) of second mounting groove (17), the top of finding a view equipment (1) is equipped with third mounting groove (20), the inner wall fixedly connected with electric connection seat (21) of third mounting groove (20).

6. An external environment viewing device for an aircraft according to claim 5, wherein: connecting block (24) on the inside fixedly connected with of electrical property connecting block (18), go up first electrical connection line of top fixedly connected with (26) of connecting block (24), the bottom of going up connecting block (24) is equipped with electrical connection groove (25).

7. An external environment viewing device for an aircraft according to claim 6, wherein: the inboard of electric connection seat (21) is equipped with spacing groove (27), the inner wall sliding connection of spacing groove (27) has electric connection head (29), the inner wall fixedly connected with third spring (28) of spacing groove (27), the bottom fixedly connected with second connecting wire (30) of electric connection head (29), second connecting wire (30) and the equipment of looking a view (1) pass through electric connection, first electric connection wire (26) and aircraft pass through electric connection.

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