CN213473537U

CN213473537U - Novel aircraft engine installing support

Info

Publication number: CN213473537U
Application number: CN202021803674.2U
Authority: CN
Inventors: 徐明远; 邓迪波; 廖容; 段春闪
Original assignee: Jiangsu Lingboer Aviation Technology Development Co ltd
Current assignee: Jiangsu Lingboer Aviation Technology Development Co ltd
Priority date: 2020-08-25
Filing date: 2020-08-25
Publication date: 2021-06-18
Anticipated expiration: 2030-08-25

Abstract

The utility model discloses a novel aircraft engine mounting bracket, which comprises an engine body and a mounting mechanism, the engine body is fixedly connected with the mounting mechanism, the mounting mechanism at least comprises a bearing plate clamped with the engine body and a mounting plate fixedly connected with the bearing plate, and a fixing component fixedly connected with the bearing plate, wherein the upper surface of the bearing plate is provided with a placing groove for placing an engine body, the side walls of two opposite ends of the bearing plate are respectively fixedly connected with a mounting plate, the upper surface of the bearing plate is fixedly connected with a fixing component, the fixed assembly at least comprises an accommodating column fixedly connected with the accommodating plate, a movable rod movably sleeved with the accommodating column, an extending plate fixedly connected with the movable rod, a fixing frame fixedly connected with the extending plate, and a first clamping frame and a second clamping frame fixedly connected with the fixing frame. This novel aircraft engine installing support, it is rational in infrastructure, easy operation is favorable to using widely.

Description

Novel aircraft engine installing support

Technical Field

The utility model belongs to the technical field of the engine, concretely relates to novel aircraft engine installing support.

Background

An aircraft engine is a highly complex and precise thermal machine, and is used as the heart of an aircraft, not only as the power for flying the aircraft, but also as an important driving force for promoting the development of aviation industry, and the aircraft engine comprises various types such as a turbofan engine, a turboprop engine, a ram engine, a piston engine and the like.

At present, the installation of current aircraft engine, most direct punching installation on the engine organism, this mounting method's stability is not high, and the department of punching on engine organism surface takes place the corrosion easily, is unfavorable for the long-term use of engine organism, consequently, need to design a novel aircraft engine installing support urgently to improve above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a novel aircraft engine installing support to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a novel aircraft engine mounting bracket comprises an engine body and a mounting mechanism, wherein the engine body is fixedly connected with the mounting mechanism, the mounting mechanism at least comprises a bearing plate clamped with the engine body and a mounting plate fixedly connected with the bearing plate, and a fixing component fixedly connected with the bearing plate, wherein the upper surface of the bearing plate is provided with a placing groove for placing an engine body, the side walls of two opposite ends of the bearing plate are respectively and fixedly connected with a mounting plate, and the two groups of mounting plates are respectively provided with a plurality of groups of mounting holes distributed in an array manner, the upper surface of the bearing plate is fixedly connected with a fixing component, the fixed assembly at least comprises an accommodating column fixedly connected with the accommodating plate, a movable rod movably sleeved with the accommodating column, an extending plate fixedly connected with the movable rod, a fixing frame fixedly connected with the extending plate, and a first clamping frame and a second clamping frame fixedly connected with the fixing frame.

Preferably, the upper surface of the bearing plate is close to the two sets of mounting plates, the two ends of the bearing plate are respectively and fixedly connected with containing columns which are vertically and oppositely distributed, and one ends, far away from the bearing plate, of the containing columns are movably sleeved with the movable rods.

Preferably, the accommodating column is fixedly provided with a fixing bolt at one end of the side wall far away from the bearing plate, and the side wall of the movable rod at one end facing the fixing bolt is provided with a plurality of groups of limit holes which are distributed in a vertical array and matched with the fixing bolt.

Preferably, two sets of the movable rods are respectively and fixedly provided with an extension plate horizontally distributed opposite to the bearing plate at one end far away from the containing column, and two sets of the extension plates are respectively and fixedly connected with a fixing frame at the opposite end side walls.

Preferably, the upper surfaces of the two groups of fixing frames are respectively fixedly connected with two ends of the first clamping frame, and the first clamping frame is relatively distributed with a plurality of groups.

Preferably, the two sets of fixing frames are respectively and fixedly connected with connecting plates at two opposite end side walls far away from one end of the first clamping frame, and the two opposite ends of the connecting plates are respectively and fixedly connected with two end side walls of the second clamping frame.

The utility model discloses a technological effect and advantage: this novel aircraft engine installing support relies on the interact between spacing hole and the fixing bolt, adjusts the movable rod and accepts the relative position between the post to drive first joint frame and second joint frame and reciprocate, be convenient for press from both sides the engine organism of equidimension not tight fixed, rely on mounting panel and mounting hole with engine organism fixed mounting in assigned position department, avoid directly punching the installation on the engine organism, be convenient for protect engine body shell difficult corrosion. This novel aircraft engine installing support, it is rational in infrastructure, easy operation is favorable to using widely.

Drawings

Fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the structure of the installation mechanism of the present invention;

fig. 3 is a schematic structural view of the fixing assembly of the present invention.

In the figure: the engine comprises an engine body 1, an installation mechanism 2, a fixing assembly 3, a placement groove 4, a mounting hole 5, a bearing plate 6, a mounting plate 7, a first clamping frame 8, a second clamping frame 9, a connecting plate 10, a fixing frame 11, an extension plate 12, a limiting hole 13, a movable rod 14, a fixing bolt 15 and a containing column 16.

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.

The utility model provides a as shown in fig. 1-3 a novel aircraft engine installing support, including engine organism 1 and installation mechanism 2, engine organism 1 is the aircraft engine among the prior art, engine organism 1 and installation mechanism 2 fixed connection, installation mechanism 2 includes at least with the engine organism 1 joint accept board 6, with accept board 6 fixed connection's mounting panel 7 to and with accept board 6 fixed connection's fixed subassembly 3, accept the upper surface of board 6 and offer the standing groove 4 that supplies engine organism 1 to place, accept the relative both ends lateral wall of board 6 and be fixedly connected with mounting panel 7 respectively, and two sets of mounting panel 7 is seted up the mounting hole 5 that a plurality of groups array distributes respectively, the upper surface fixed connection who accepts board 6 is connected with fixed subassembly 3, fixed subassembly 3 includes at least and accepts board 6 fixed connection's the post 16 of acceping that accept, The clamping device comprises a movable rod 14 movably sleeved with an accommodating column 16, an extension plate 12 fixedly connected with the movable rod 14, a fixed frame 11 fixedly connected with the extension plate 12, and a first clamping frame 8 and a second clamping frame 9 fixedly connected with the fixed frame 11.

Specifically, accept the upper surface of board 6 and be close to two sets ofly the both ends of mounting panel 7 are the post 16 of acceping of the vertical relative distribution of fixedly connected with respectively, it cup joints with the activity of movable rod 14 to accept the one end that post 16 kept away from and accept board 6, and the top inner wall of acceping post 16 and the bottom of movable rod 14 are the limiting plate (not shown in the figure) of fixedly connected with mutually supporting respectively, avoid movable rod 14 to break away from completely and accept post 16.

Specifically, the accommodating column 16 is far away from one end side wall of the bearing plate 6 and is fixedly provided with a fixing bolt 15, the movable rod 14 is provided with a plurality of groups of limiting holes 13 which are distributed in a vertical array and are matched with the fixing bolt 15 towards one end side wall of the fixing bolt 15, and the position of the movable rod 14 can be fixed through the mutual matching between the fixing bolt 15 and the limiting holes 13.

Specifically, two sets of the one end that the movable rod 14 is far away from accommodating post 16 is fixed mounting respectively and is accepted the extension board 12 that the board 6 level distributes relatively, and is two sets of extension board 12 one end lateral wall in opposite directions is fixedly connected with mount 11 respectively, and extension board 12 is used for connecting movable rod 14, and the movable rod 14 of being convenient for drives first clamp frame 8 and the second clamp frame 9 and reciprocates.

Specifically, it is two sets of the upper surface of mount 11 respectively with the both ends fixed connection of first joint frame 8, just 8 relative distributions of first joint frame have a plurality of groups, through the interact between first joint frame 8 and standing groove 4, with the chucking of engine organism 1 fixed.

Specifically, it is two sets of the both ends lateral wall in opposite directions that first joint frame 8 one end was kept away from to mount 11 is fixedly connected with connecting plate 10 respectively, and is two sets of the both ends in opposite directions of connecting plate 10 respectively with the both ends lateral wall fixed connection of second joint frame 9, the radius of second joint frame 9 is less in the radius of first joint frame 8 for the afterbody of chucking engine organism 1 increases engine organism 1 and accepts the stability of being connected of board 6.

The working principle is as follows: this novel aircraft engine installing support, during the use, place engine organism 1 on standing groove 4, then through the movable rod 14 and accommodate mutually supporting between the post 16, thereby it removes to remove movable rod 14 and drive extension board 12, it is fixed to press from both sides engine organism 1 clamp until first joint frame 8 and second joint frame 9, then through mutually supporting between fixing bolt 15 and spacing hole 13, screw up fixing bolt 15 with the rigidity of movable rod 14, then through mutually supporting between mounting hole 5 and the screw, be fixed in assigned position department with mounting panel 7, thereby accomplish the fixed mounting of engine organism 1. This novel aircraft engine installing support, it is rational in infrastructure, easy operation is favorable to using widely.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims

1. The utility model provides a novel aircraft engine installing support, includes engine organism (1) and installation mechanism (2), its characterized in that: engine organism (1) and installation mechanism (2) fixed connection, installation mechanism (2) include at least with engine organism (1) joint accept board (6), with accept board (6) fixed connection's mounting panel (7) to and with accept board (6) fixed connection's fixed subassembly (3), accept standing groove (4) that supply engine organism (1) to place are seted up to the upper surface of board (6), accept both ends lateral wall difference fixedly connected with mounting panel (7) that board (6) is relative, and two sets of mounting hole (5) that a plurality of groups array distributes are seted up respectively to mounting panel (7), the upper surface fixedly connected with fixed subassembly (3) of accepting board (6), fixed subassembly (3) include at least with accept board (6) fixed connection accept post (16), with accommodate movable rod (14) that post (16) activity cup jointed, The extension plate (12) is fixedly connected with the movable rod (14), the fixing frame (11) is fixedly connected with the extension plate (12), and the first clamping frame (8) and the second clamping frame (9) are fixedly connected with the fixing frame (11).

2. A novel aircraft engine mounting bracket according to claim 1, wherein: the upper surface of the bearing plate (6) is close to two sets of the two ends of the mounting plate (7) are fixedly connected with containing columns (16) which are vertically and oppositely distributed, and one end, away from the bearing plate (6), of each containing column (16) is movably sleeved with the movable rod (14).

3. A novel aircraft engine mounting bracket according to claim 1, wherein: the side wall of one end, far away from the bearing plate (6), of the accommodating column (16) is fixedly provided with a fixing bolt (15), and the side wall of one end, facing the fixing bolt (15), of the movable rod (14) is provided with a plurality of groups of limiting holes (13) which are distributed in a vertical array and matched with the fixing bolt (15).

4. A novel aircraft engine mounting bracket according to claim 1, wherein: two sets of one end that accommodate post (16) was kept away from in movable rod (14) is fixed mounting respectively and is accepted extension board (12) that board (6) level distributed relatively, two sets of one end lateral wall in opposite directions of extension board (12) is fixedly connected with mount (11) respectively.

5. A novel aircraft engine mounting bracket according to claim 1, wherein: the upper surfaces of the two groups of fixing frames (11) are fixedly connected with the two ends of the first clamping frame (8) respectively, and a plurality of groups are distributed on the first clamping frame (8) in a relative mode.

6. A novel aircraft engine mounting bracket according to claim 1, wherein: two sets of both ends lateral wall in opposite directions that first joint frame (8) one end was kept away from in mount (11) is fixedly connected with connecting plate (10) respectively, and is two sets of both ends in opposite directions of connecting plate (10) respectively with the both ends lateral wall fixed connection of second joint frame (9).