CN209523810U - Aircraft engine installing mechanism - Google Patents
Aircraft engine installing mechanism Download PDFInfo
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- CN209523810U CN209523810U CN201920136558.0U CN201920136558U CN209523810U CN 209523810 U CN209523810 U CN 209523810U CN 201920136558 U CN201920136558 U CN 201920136558U CN 209523810 U CN209523810 U CN 209523810U
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Abstract
The utility model discloses aircraft engine installing mechanisms, including engine main body, the side of the engine main body is provided with installing mechanism, the installing mechanism includes that connecting rod, fixed plate, the first resilient cushion, fixed column, fixed auricle, connecting hole, the second resilient cushion, crossbeam and vertical plate, the connecting rod are symmetrically installed the upper surface for being fixed on engine main body；The second resilient cushion installation of the utility model is set in the surface of crossbeam and is located at the inside of vertical plate, help to increase crossbeam in the buffer capacity of the inside of vertical plate, prevent crossbeam damaged in collision during installation, extend the service life of crossbeam, and engine main body is facilitated to be fixed on fixed frame by vertical plate and crossbeam, abrasion when preventing connecting rod from connecting with fixed auricle by the buffer capacity of the first resilient cushion simultaneously, and connecting rod is facilitated to connect with fixed auricle, and reduce difficulty and the installation effectiveness for improving worker that engine main body is mounted on fixed frame.
Description
Technical field
The utility model belongs to aircraft engine technical field, and in particular to aircraft engine installing mechanism.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed, on ground or machine tool
Remote control station personnel track it, are positioned, are remotely controlled, telemetering and Digital Transmission by the equipment such as radar, can Reusability it is more
It is secondary, it is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc., engine is the power resources of aircraft, therefore is sent out
The superiority and inferiority of motivation quality is directly related to the quality of aircraft.
Existing aircraft engine is when on mounting and fixing support, since installation difficulty is larger and time-consuming and laborious, and worker
It is easy the problem that fault causes the installation effectiveness of worker low during installation, thus it is proposed that aircraft engine installing mechanism.
Utility model content
The purpose of this utility model is to provide aircraft engine installing mechanisms, to solve to propose in above-mentioned background technique
For existing aircraft engine when on mounting and fixing support, since installation difficulty is larger and time-consuming and laborious, and worker is during installation
The easy problem for causing the installation effectiveness of worker low of making mistakes.
To achieve the above object, the utility model provides the following technical solutions: aircraft engine installing mechanism, including hair
Motivation main body, the side of the engine main body are provided with installing mechanism, and the installing mechanism includes connecting rod, fixed plate, first
Resilient cushion, fixed column, fixed auricle, connecting hole, the second resilient cushion, crossbeam and vertical plate, the connecting rod, which is symmetrically installed, is fixed on hair
The upper surface of motivation main body, one end of the connecting rod are fixedly connected on the engine main body upper surface other end and are connected with fixed ear
Piece, the connecting hole are provided with the inside of fixed auricle and through the two sides of fixed auricle, and the first resilient cushion installation is fixed
Connecting hole inner surface and be set in the surface of fixed column, the fixed column is fixed on the inner surface of connecting rod, described solid
Fixed board is fixed on the bottom end of fixed auricle, and the fixed plate is mutually perpendicular to be fixedly connected with fixed auricle, the vertical plate peace
Dress is fixed on the side bottom position of engine main body, and one end of the crossbeam runs through the inside of vertical plate and extends outwardly, described
The installation of second resilient cushion is set in the surface of crossbeam and is located at the inside of vertical plate, and the surface of the fixed plate is provided with connection machine
Structure.
Preferably, the bindiny mechanism include connecting plate, retention bead, T-type locating slot, hexagon-headed bolt, threaded hole and
Thread groove, the connecting plate are connected together by fixed plate and T-type locating slot and are fixed on the bottom end of fixed auricle, and the T-type is fixed
Position slot is symmetrically provided with the side of connecting plate, and the retention bead is symmetrically installed the two sides for being fixed on fixed plate and is placed on T-type
The inside of locating slot, one end of the hexagon-headed bolt are placed on the inside of thread groove, the screw thread through the inside of threaded hole
Hole is symmetrically provided with the side of fixed plate and is located at the two sides of fixed auricle, and the thread groove is symmetrically provided with T-type locating slot
Inner surface.
Preferably, one end top position installation settings driving gear of the engine main body, the side of the driving gear
Face is fixed with shaft and is placed on the inside of engine main body.
Preferably, fixation hole is offered at the surface corner location of the connecting plate.
Preferably, the surface of the vertical plate symmetrically offers mounting hole.
Preferably, the surface of the engine main body is provided with atomizer, and described atomizer one end is connected with spray bar.
Preferably, the side of the engine main body is symmetrically arranged with lifting lug.
Compared with prior art, the utility model has the beneficial effects that
(1) the second resilient cushion installation of the utility model is set in the surface of crossbeam and is located at the inside of vertical plate, facilitates
Increase crossbeam in the buffer capacity of the inside of vertical plate, prevent crossbeam damaged in collision during installation, extend the service life of crossbeam,
And engine main body is facilitated to be fixed on fixed frame by vertical plate and crossbeam, while passing through the buffer capacity of the first resilient cushion
Abrasion when preventing connecting rod from connecting with fixed auricle, and facilitate connecting rod to connect with fixed auricle, and reduce engine main body installation
The installation effectiveness of difficulty and raising worker on fixed frame.
(2) fixed plate of the utility model is inserted into T by being fixed with T-type locating slot convenient for fixed plate from top to bottom
The inside of type locating slot, and fixed plate loose or dislocation during installation is prevented by the limit effect of retention bead, pacify convenient for worker
Assembly and disassembly, while increasing fixed plate in the stability of connecting plate side, while threaded hole and spiral shell are run through by hexagon-headed bolt
Groove screws fixation, and fixed plate is facilitated to be fixed on the side of connecting plate, improves the installation speed of worker.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the area the Tu1Zhong A enlarged structure schematic diagram of the utility model；
Fig. 3 is the connecting plate local overlooking the schematic diagram of the section structure of the utility model；
In figure: 1, engine main body；2, connecting rod；3, fixed plate；4, connecting plate；5, the first resilient cushion；6, fixed column；7, solid
Determine auricle；8, connecting hole；9, the second resilient cushion；10, crossbeam；11, vertical plate；12, driving gear；13, retention bead；14, T-type is fixed
Position slot；15, hexagon-headed bolt；16, threaded hole；17, thread groove.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1, Fig. 2 and Fig. 3 are please referred to, the utility model provides a kind of technical solution: aircraft engine installing mechanism, packet
Engine main body 1 is included, the side of engine main body 1 is provided with installing mechanism, and installing mechanism includes connecting rod 2, fixed plate 3, first
Resilient cushion 5, fixed column 6, fixed auricle 7, connecting hole 8, the second resilient cushion 9, crossbeam 10 and vertical plate 11, connecting rod 2 are symmetrically installed solid
It is scheduled on the upper surface of engine main body 1, one end of connecting rod 2 is fixedly connected on the 1 upper surface other end of engine main body and is connected with admittedly
Determine auricle 7, connecting hole 8 is provided with the inside of fixed auricle 7 and through the two sides of fixed auricle 7, and the installation of the first resilient cushion 5 is fixed
Connecting hole 8 inner surface and be set in the surface of fixed column 6, fixed column 6 is fixed on the inner surface of connecting rod 2, fixed plate 3
It is fixed on the bottom end of fixed auricle 7, fixed plate 3 is mutually perpendicular to be fixedly connected with fixed auricle 7, and vertical plate 11 is fixed on
The side bottom position of engine main body 1, one end of crossbeam 10 run through the inside of vertical plate 11 and extend outwardly, the second resilient cushion 9
Installation is set in the surface of crossbeam 10 and is located at the inside of vertical plate 11, helps to increase crossbeam 10 in the buffering of the inside of vertical plate 11
Ability prevents the damaged in collision during installation of crossbeam 10, extends the service life of crossbeam 10, and engine main body 1 is facilitated to pass through
Vertical plate 11 and crossbeam 10 are fixed on fixed frame, while being prevented connecting rod 2 by the buffer capacity of the first resilient cushion 5 and being fixed
Auricle 7 is worn when connecting, and facilitates connecting rod 2 to connect with fixed auricle 7, and reduce engine main body 1 and be mounted on fixed frame
Difficulty and improve worker installation effectiveness, the surface of fixed plate 3 is provided with bindiny mechanism.
In the present embodiment, it is preferred that bindiny mechanism includes connecting plate 4, retention bead 13, T-type locating slot 14, turret head spiral shell
Bolt 15, threaded hole 16 and thread groove 17, connecting plate 4 are connected together by fixed plate 3 and T-type locating slot 14 and are fixed on fixed auricle
7 bottom end, T-type locating slot 14 are symmetrically provided with the side of connecting plate 4, and retention bead 13, which is symmetrically installed, is fixed on fixed plate 3
One end of two sides and the inside for being placed on T-type locating slot 14, hexagon-headed bolt 15 is placed on screw thread through the inside of threaded hole 16
The inside of slot 17, threaded hole 16 are symmetrically provided with the side of fixed plate 3 and are located at the two sides of fixed auricle 7, and thread groove 17 is symmetrical
It is provided with the inner surface of T-type locating slot 14, fixed plate 3 with T-type locating slot 14 by being fixed, convenient for fixed plate 3 from upper past
The inside of lower insertion T-type locating slot 14, and prevent fixed plate 3 from loosening during installation by the limit effect of retention bead 13 and take off
It falls, is mounted and dismounted convenient for worker, while increasing fixed plate 3 in the stability of 4 side of connecting plate, while passing through hexagon-headed bolt
15 screw fixation through threaded hole 16 and thread groove 17, and fixed plate 3 is facilitated to be fixed on the side of connecting plate 4, improve worker
Installation speed.
In the present embodiment, it is preferred that one end top position installation settings driving gear 12 of engine main body 1, driving tooth
The side of wheel 12 is fixed with shaft and is placed on the inside of engine main body 1, drives convenient for the mechanical energy that engine main body 1 generates
Driving gear 12 rotates.
In the present embodiment, it is preferred that fixation hole is offered at the surface corner location of connecting plate 4, it is logical convenient for connecting plate 4
Bolt is crossed to be mounted on Der Motortraeger.
In the present embodiment, it is preferred that the surface of vertical plate 11 symmetrically offers mounting hole, is bolted convenient for vertical plate 11
On Der Motortraeger and increase the stability of engine main body 1.
In the present embodiment, it is preferred that the surface of engine main body 1 is provided with atomizer, and atomizer one end is connected with oil spout
Pipe enters 1 internal-combustion of engine main body generation thermal energy convenient for fuel oil and is converted to mechanical energy by engine main body 1.
In the present embodiment, it is preferred that the side of engine main body 1 is symmetrically arranged with lifting lug, and engine main body 1 is facilitated to pass through
Suspension hook slings carrying movement.
The working principle and process for using of the utility model: the utility model when in use, is first installed the first resilient cushion 5
It is set in the surface of fixed column 6 and fixed column 6 is followed to be fixed on the inside of connecting hole 8,3 bottom end of fixed plate is then placed on T
The inside of type locating slot 14 is simultaneously slided from top to bottom, while retention bead 13 being allowed to be fastened on the inside of T-type locating slot 14, then
Threaded hole 16 and thread groove 17 are aligned, then the inside of threaded hole 16 is run through in one end of hexagon-headed bolt 15 and is revolved with thread groove 17
It closes and fixes, connecting plate 4 is mounted on fixed frame by bolt then, then the vertical plate 11 of 1 side of engine main body is led to again
It crosses bolt to be fixed on fixed frame, the utility model can be used after being installed.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (7)
1. aircraft engine installing mechanism, including engine main body (1), it is characterised in that: the side of the engine main body (1)
Face is provided with installing mechanism, and the installing mechanism includes connecting rod (2), fixed plate (3), the first resilient cushion (5), fixed column (6), consolidates
Determine auricle (7), connecting hole (8), the second resilient cushion (9), crossbeam (10) and vertical plate (11), the connecting rod (2) is symmetrically installed fixation
In the upper surface of engine main body (1), one end of the connecting rod (2) is fixedly connected on engine main body (1) upper surface other end
It is connected with fixed auricle (7), the connecting hole (8) is provided with the inside of fixed auricle (7) and through the two of fixed auricle (7)
Side, first resilient cushion (5) is fixed on the inner surface of connecting hole (8) and is set in the surface of fixed column (6), described solid
Fixed column (6) is fixed on the inner surface of connecting rod (2), and the fixed plate (3) is fixed on the bottom end of fixed auricle (7), institute
It states fixed plate (3) to be mutually perpendicular to be fixedly connected with fixed auricle (7), the vertical plate (11) is fixed on engine main body (1)
Side bottom position, one end of the crossbeam (10) through vertical plate (11) inside and extend outwardly, second resilient cushion
(9) installation is set in the surface of crossbeam (10) and is located at the inside of vertical plate (11), and the surface of the fixed plate (3) is provided with connection
Mechanism.
2. aircraft engine installing mechanism according to claim 1, it is characterised in that: the bindiny mechanism includes connection
Plate (4), retention bead (13), T-type locating slot (14), hexagon-headed bolt (15), threaded hole (16) and thread groove (17), the company
Fishplate bar (4) is connected together by fixed plate (3) and T-type locating slot (14) and is fixed on the bottom end of fixed auricle (7), and the T-type is fixed
Position slot (14) is symmetrically provided with the side of connecting plate (4), and the retention bead (13), which is symmetrically installed, is fixed on the two of fixed plate (3)
It is put through the inside of threaded hole (16) one end of side and the inside for being placed on T-type locating slot (14), the hexagon-headed bolt (15)
The inside in thread groove (17) is set, the threaded hole (16) is symmetrically provided with the side of fixed plate (3) and is located at fixed auricle (7)
Two sides, the thread groove (17) is symmetrically provided with the inner surfaces of T-type locating slot (14).
3. aircraft engine installing mechanism according to claim 1, it is characterised in that: the engine main body (1)
One end top position installation settings driving gear (12), the side of the driving gear (12), which is fixed with shaft and is placed on, starts
The inside of owner's body (1).
4. aircraft engine installing mechanism according to claim 2, it is characterised in that: the surface of the connecting plate (4)
Fixation hole is offered at corner location.
5. aircraft engine installing mechanism according to claim 1, it is characterised in that: the surface pair of the vertical plate (11)
Title offers mounting hole.
6. aircraft engine installing mechanism according to claim 1, it is characterised in that: the engine main body (1)
Surface is provided with atomizer, and described atomizer one end is connected with spray bar.
7. aircraft engine installing mechanism according to claim 1, it is characterised in that: the engine main body (1)
Side is symmetrically arranged with lifting lug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920136558.0U CN209523810U (en) | 2019-01-27 | 2019-01-27 | Aircraft engine installing mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920136558.0U CN209523810U (en) | 2019-01-27 | 2019-01-27 | Aircraft engine installing mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209523810U true CN209523810U (en) | 2019-10-22 |
Family
ID=68230899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920136558.0U Active CN209523810U (en) | 2019-01-27 | 2019-01-27 | Aircraft engine installing mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209523810U (en) |
-
2019
- 2019-01-27 CN CN201920136558.0U patent/CN209523810U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200527 Address after: 243000 Huitong standardized workshop 5, Zhongfei Avenue, zhengpugang New District, Ma'anshan City, Anhui Province Patentee after: Anhui Zhixiang Aviation Technology Co., Ltd Address before: 723000 Aircraft Intelligence New Town of Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee before: SHAANXI ZHIXIANG AVIATION TECHNOLOGY DEVELOPMENT Co.,Ltd. |
|
| TR01 | Transfer of patent right |