Fuel selector support of small aircraft

Abstract

The utility model relates to the technical field of aircraft parts, in particular to a small aircraft fuel selector support which comprises a selector support body, and a left bottom plate and a right bottom plate which are mutually symmetrical are fixedly installed at the bottom of the selector support body. The side faces, close to each other, of the two bottom plates are each fixedly provided with a front guide rod and a rear guide rod which are symmetrical to each other, a fixed base is arranged below the bottom plates, a rubber pad groove is formed in the fixed base, a buffering damping pad is arranged in the rubber pad groove, and an upper padding plate is arranged above the buffering damping pad. Side shock pads are fixedly installed on the left side face and the right side face of the upper base plate, the bottom plate and the side shock pads are fixedly installed on the buffer shock pads, the left side face and the right side face of the upper base plate are each provided with a front guide hole and a rear guide hole which are symmetrical, and the guide rods are located in the guide holes and matched with the guide holes in an inserted mode. The damping device has a certain buffering and damping effect and is convenient to assemble and use.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of aircraft parts, and more particularly to a small airplane fuel selector support. BACKGROUND

[0002] In the design and manufacturing process of small airplanes, the fuel selector support is a crucial component that is responsible for supporting and fixing the fuel selector to ensure accurate and reliable selection of the required fuel source during flight. Currently, most small airplane fuel selector supports on the market are made of metal structures and assembled through welding or bolt connection. These supports can meet the basic support and fixing requirements to some extent.

[0003] However, when these supports are fixedly installed on external frame bodies, they are usually directly fixed with fastening bolts. Since the supports are made of metal structures and the corresponding external frame bodies are also made of metal structures, there are no corresponding force relief and buffering components between the metal and metal, which cannot perform certain buffering and shock absorption protection operations. Direct rigid connection can easily cause the external frame bodies to transmit force directly to the supports after being stressed, which can adversely affect the supports and the installed components on the supports, further affecting the service life. In view of this, we propose a small airplane fuel selector support. SUMMARY

[0004] The utility model aims at providing a small airplane fuel selector support to solve the defects proposed in the background art.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme:

[0006] A small airplane fuel selector support, comprising a selector support main body, the bottom of the selector support main body is fixedly installed with two left and right symmetrical bottom plates, two the mutually close side surfaces of the bottom plates are fixedly installed with two front and rear symmetrical guide rods, a fixed base is arranged below the bottom plate, a rubber pad groove is arranged in the fixed base, a buffer shock pad is arranged in the rubber pad groove, an upper pad plate is arranged above the buffer shock pad, a side shock pad is fixedly installed on the left and right side surfaces of the upper pad plate, the bottom plate and the side shock pad are fixedly installed on the buffer shock pad, two front and rear symmetrical guide holes are arranged on the left and right side surfaces of the upper pad plate, and the guide rods are inserted and matched with the guide holes.

[0007] Preferably, the cross sections of the guide rods and the guide holes are semicircular, and the sizes of the guide rods are matched with the sizes of the guide holes.

[0008] Preferably, the upper surface of the upper backing plate abuts against the bottom surface of the selector support body, and a central assembly chamber is arranged at the central position of the selector support body.

[0009] Preferably, a plurality of shaft holes communicating with the outside are arranged on the left and right side plate bodies of the selector support body, and a plurality of hollow holes communicating with the outside are also arranged on the left and right side plate bodies of the selector support body.

[0010] Preferably, side edge blocking strips are fixedly installed on the front and rear end groove walls of the rubber pad groove, and the buffer shock pad is clamped between the two side edge blocking strips.

[0011] Preferably, a plurality of expansion and contraction grooves communicating with the outside are arranged on the left and right side groove walls of the rubber pad groove, and the cross section of the expansion and contraction groove is arc-shaped.

[0012] Preferably, a plurality of central heat dissipation grooves arranged in a linear and equidistant manner are arranged on the upper surface of the buffer shock pad, and a plurality of side edge heat dissipation holes communicating with the corresponding central heat dissipation grooves are arranged in the left and right side plate bodies of the fixed base.

[0013] Preferably, front and rear two mutually symmetrical fixed protrusions are fixedly installed on the left and right side surfaces of the fixed base, and the fixed protrusions are fixedly installed on the external frame body.

[0014] Compared with the prior art, the utility model has the beneficial effects that:

[0015] 1、The fixed base is used for supporting, and the buffer shock pad is arranged in the fixed base, in addition, the upper backing plate and the side edge shock pad are arranged above the buffer shock pad, the upper backing plate is used for directly supporting the bottom of the selector support body, the side edge shock pad and the buffer shock pad can realize buffering protection, and the effect of buffering and shock relief to a certain extent and removing the direct rigid force between metal connecting pieces is achieved.

[0016] 2、The guide rod and the guide hole are arranged, so that the bottom plate is conveniently fixed and installed, in addition, the central heat dissipation groove and the side edge heat dissipation hole are arranged, so that heat dissipation operation is carried out on the buffer shock pad part, and the expansion and contraction groove is arranged, so that expansion and contraction protection operation is carried out on the buffer shock pad. DRAWINGS

[0017] Figure 1 It is a whole structure schematic view of the utility model;

[0018] Figure 2 It is an explosion structure schematic view of the utility model;

[0019] Figure 3Part structure schematic diagram one of the utility model;

[0020] Figure 4 Part structure schematic diagram two of the utility model;

[0021] Figure 5 Part structure schematic diagram of the utility model Figure 4 Enlarged view of A in the middle;

[0022] The meaning of each reference numeral in the figure is as follows:

[0023] 1, selector support main body;10, shaft hole;11, hollow hole;12, center assembly chamber;13, bottom plate;131, guide rod;

[0024] 2, fixed base;20, rubber pad groove;21, side edge blocking strip;22, expansion groove;23, buffer shock pad;24, center heat dissipation groove;25, side edge heat dissipation hole;26, fixed protrusion;

[0025] 3, upper pad plate;30, side edge shock pad;31, guide hole. Specific implementation

[0026] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0027] Please refer to Figures 1-5 The utility model provides a kind of technical scheme: a small aircraft fuel selector support, including selector support main body 1, the bottom of selector support main body 1 is fixedly installed with left and right two mutually symmetrical bottom plate 13, two bottom plate 13 mutually close side is fixedly installed with front and rear two mutually symmetrical guide rod 131, the bottom of bottom plate 13 is provided with fixed base 2, fixed base 2 is provided with rubber pad groove 20 in it, rubber pad groove 20 is provided with buffer shock pad 23 in it, the top of buffer shock pad 23 is provided with upper pad plate 3, the left and right sides of upper pad plate 3 are fixedly installed with side edge shock pad 30, the bottom surface of upper pad plate 3 is on buffer shock pad 23, the top surface of upper pad plate 3 is on the bottom surface of selector support main body 1, for supporting operation;

[0028] Specifically, bottom plate 13 and side edge shock pad 30 are fixedly installed on buffer shock pad 23 by multiple fastening bolts, realize fixed operation, the left and right sides of upper pad plate 3 are provided with front and rear two mutually symmetrical guide holes 31, guide rod 131 is located in guide hole 31 and is inserted with guide hole 31, realize guide assembly operation.

[0029] In this embodiment, the cross section of the guide rod 131 and the guide hole 31 is semicircular, and the size of the guide rod 131 is matched with the size of the guide hole 31, which is used for stabilizing the plug-in guide operation.

[0030] Specifically, the center of the selector support body 1 is provided with a center assembly chamber 12, and the left and right side plates of the selector support body 1 are provided with a plurality of shaft holes 10 connected with the outside, and a plurality of hollow holes 11 connected with the outside are also arranged on the left and right side plates of the selector support body 1, and the hollow holes 11 are used to reduce the weight.

[0031] Further, the front and rear end walls of the rubber pad groove 20 are fixedly installed with side blocking strips 21, and the buffer shock pad 23 is clamped between the two side blocking strips 21, which can limit the buffer shock pad 23 and make the buffer shock pad 23 more stable when installed in the rubber pad groove 20.

[0032] In addition, the left and right side walls of the rubber pad groove 20 are provided with a plurality of expansion grooves 22 connected with the outside, and the cross section of the expansion groove 22 is arc-shaped, and the expansion groove 22 is used for the expansion protection operation of the buffer shock pad 23, so that the buffer shock pad 23 can be deformed to one side of the expansion groove 22 after expansion.

[0033] It is worth noting that the upper surface of the buffer shock pad 23 is provided with a plurality of center heat dissipation grooves 24 arranged in a linear and equidistant manner, and the left and right side plates of the fixed base 2 are provided with a plurality of side heat dissipation holes 25 connected with the corresponding center heat dissipation grooves 24, which can realize the heat dissipation operation of the buffer shock pad 23.

[0034] It is worth noting that the left and right side surfaces of the fixed base 2 are fixedly installed with front and rear two mutually symmetrical fixed protrusions 26, and the fixed protrusions 26 are fixedly installed on the external frame by fastening bolts.

[0035] When the small aircraft fuel selector support of the utility model is used, the fixed protrusions 26 are fixedly installed on the external frame by fastening bolts, then the buffer shock pad 23 is clamped into the rubber pad groove 20, the buffer shock pad 23 is ensured to be between the two side blocking strips 21, then the upper pad plate 3 is placed on the buffer shock pad 23, and the side shock pad 30 is also clamped into the rubber pad groove 20, finally, the guide rod 131 is inserted into the guide hole 31, and the bottom plate 13, the side shock pad 30 and the buffer shock pad 23 are fixedly installed on the fixed base 2 by fastening bolts at the same time, and the fixing operation is completed.

[0036] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely preferred examples of the present invention and are not intended to limit the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.

Claims

1. A light aircraft fuel selector yoke comprising a yoke body (1) characterised in that: The bottom of the selector support body (1) is fixedly installed with two left and right symmetrical bottom plates (13), two front and back symmetrical guide rods (131) are fixedly installed on the mutually close sides of the two bottom plates (13), a fixed base (2) is arranged below the bottom plate (13), a rubber pad groove (20) is arranged in the fixed base (2), a buffer shock pad (23) is arranged in the rubber pad groove (20), an upper pad plate (3) is arranged above the buffer shock pad (23), a side shock pad (30) is fixedly installed on the left and right sides of the upper pad plate (3), the bottom plate (13) and the side shock pad (30) are fixedly installed on the buffer shock pad (23), two front and back symmetrical guide holes (31) are arranged on the left and right sides of the upper pad plate (3), and the guide rod (131) is inserted and matched with the guide hole (31).

2. A light aircraft fuel selector yoke according to claim 1 wherein: The cross sections of the guide rod (131) and the guide hole (31) are semicircular, and the size of the guide rod (131) is matched with the size of the guide hole (31).

3. The ultralight aircraft fuel selector yoke of claim 1, wherein: The upper surface of the upper pad plate (3) abuts against the bottom surface of the selector support body (1), and a center assembly chamber (12) is arranged at the center position of the selector support body (1).

4. The light aircraft fuel selector yoke of claim 1 wherein: A plurality of shaft holes (10) communicating with the outside are arranged on the left and right side plate bodies of the selector support body (1), and a plurality of hollow holes (11) communicating with the outside are also arranged on the left and right side plate bodies of the selector support body (1).

5. The light aircraft fuel selector yoke of claim 1 wherein: Side blocking strips (21) are fixedly installed on the front and back end groove walls of the rubber pad groove (20), and the buffer shock pad (23) is clamped between the two side blocking strips (21).

6. A light aircraft fuel selector yoke according to claim 5 wherein: A plurality of expansion grooves (22) communicating with the outside are arranged on the left and right side groove walls of the rubber pad groove (20), and the cross section of the expansion groove (22) is arc-shaped.

7. The light aircraft fuel selector yoke of claim 1 wherein: A plurality of center heat dissipation grooves (24) arranged in a linear and equidistant manner are arranged on the upper surface of the buffer shock pad (23), and a plurality of side heat dissipation holes (25) communicating with the corresponding center heat dissipation grooves (24) are arranged in the left and right side plate bodies of the fixed base (2).

8. The light aircraft fuel selector yoke of claim 1 wherein: Front and back symmetrical fixed protrusions (26) are fixedly installed on the left and right sides of the fixed base (2), and the fixed protrusions (26) are fixedly installed on the outer frame.

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