CN206502033U - A kind of installing mechanism of high reliability aircraft engine - Google Patents
A kind of installing mechanism of high reliability aircraft engine Download PDFInfo
- Publication number
- CN206502033U CN206502033U CN201720188051.0U CN201720188051U CN206502033U CN 206502033 U CN206502033 U CN 206502033U CN 201720188051 U CN201720188051 U CN 201720188051U CN 206502033 U CN206502033 U CN 206502033U
- Authority
- CN
- China
- Prior art keywords
- mounting bracket
- installing mechanism
- high reliability
- bottom plate
- engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Abstract
The utility model belongs to technical field of aircraft design, and in particular to a kind of installing mechanism of high reliability aircraft engine, it is characterised in that including：It is fixed on carry-on two bottom plates be arrangeding in parallel, the buffer board being horizontally set on above the bottom plate, sequentially passes through the bottom plate and the support column of buffer board, the shock structure that is erected between the bottom plate and buffer board and is set on the support column and the first mounting bracket and the second mounting bracket that are vertically set on buffer board two ends, engine is arranged on the first mounting bracket and the second mounting bracket.Engine is arranged on the top of aircraft by the utility model by installing mechanism, and by shock structure damping, and installing mechanism is not allowed yielding, is easily installed and dismantles, aircraft is more stable.
Description
Technical field
A kind of the utility model aircraft devices field, and in particular to installing mechanism of high reliability aircraft engine.
Background technology
Installed more than the installing mechanism of the engine of conventional aircraft using suspension beam structure, the hanging stress of engine, engine
Installing mechanism be easily deformed and influence the installation accuracy of engine.In addition, install engine support directly with engine and
Aircraft is contacted firmly, and the life-span of aircraft can also be given a shock influence.
Utility model content
The utility model is easily deformed for overarm mounting bracket set forth above, and the service life of influence aircraft
Problem, and a kind of installing mechanism of research and design is not allowed yielding and can be effectively isolated engine high-frequency vibration, it is to avoid to flight
Device produces the installing mechanism of the high reliability aircraft engine of influence.
The utility model solves the technical scheme that its technical problem used：
A kind of installing mechanism of high reliability aircraft engine, it is characterised in that including：It is fixed on carry-on two
The bottom plate that be arranged in parallel, the buffer board being horizontally set on above the bottom plate, the support for sequentially passing through the bottom plate and buffer board
Post, the shock structure for being erected between the bottom plate and buffer board and being set on the support column and it is vertically set on buffering
First mounting bracket and the second mounting bracket at plate two ends, engine are arranged on the first mounting bracket and the second mounting bracket.
Further, there are four screw holes for being used for stationary engine on first mounting bracket.
Further, there are two to be used for installing the bearing mounting holes of bearing on first mounting bracket, engine it is defeated
Shaft and reducer shaft are erected on first mounting bracket by bearing respectively.
Further, it is characterised in that there are multiple lightening holes on second mounting bracket.
Further, the installing mechanism also includes the steering wheel fixed mount being fixedly connected with steering wheel, the steering wheel fixed mount
It is fixedly connected on the bottom of the first mounting bracket.
Further, the shock structure is six.
A kind of beneficial effect of the installing mechanism of high reliability aircraft engine of the present utility model is：
The 1st, installing mechanism is arranged on to the top of aircraft, engine is horizontally arranged on installing mechanism, be easily installed and
Dismounting, and engine acts perpendicularly to support and aircraft, it is more reliable and more stable.
2nd, by shock structure between engine and aircraft, realization is flexible coupling, and six shock structures are effectively isolated engine production
Raw dither, reduces the infringement to engine and aircraft, improves service life.
3rd, lightening hole is set on the second mounting bracket, while support engine is ensured, reduces the load of whole aircraft.
Brief description of the drawings
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Fig. 1 is the stereogram that the utility model embodiment installing mechanism is connected with engine；
Fig. 2 is the preceding visual angle stereogram of the utility model embodiment installing mechanism；
Fig. 3 is the utility model embodiment installing mechanism back angle stereogram.
Wherein：1st, bottom plate, the 2, first mounting bracket, 21, bearing mounting hole, 22, screw hole, the 3, second mounting bracket, 31, loss of weight
Hole, 4, buffer board, 5, support column, 6, shock structure, 7, engine, 8, steering wheel fixed mount.
Embodiment
The utility model is described in further detail presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram,
Only illustrate basic structure of the present utility model in a schematic way, therefore it only shows the composition relevant with the utility model.
The installing mechanism of high reliability aircraft engine as shown in Figure 1-Figure 3, including：Bottom plate 1, the first mounting bracket 2,
Second mounting bracket 3, buffer board 4, support column 5, shock structure 6 and steering wheel fixed mount 8.Referring to Fig. 2 and Fig. 3, the horizontal parallel of two bottom plate 1
Set, bottom plate 1 is fixed on board the aircraft, and buffer board 4 is horizontally set on the top of bottom plate 1, and support column 5 sequentially passes through the He of bottom plate 1
Buffer board 4, shock structure 6 is folded between bottom plate 1 and buffer board 4 and is set on support column 5, the first mounting bracket 2 and the second peace
3 two ends for being vertically arranged buffer board 4 are shelved, two mounting brackets, which are used for being fixedly mounted on engine 7, the first mounting bracket 2, has two
Bearing mounting hole 21 and four screw holes 22, four screw holes 22 are used for the shell of engine 7 being fixed on the first mounting bracket 2
On, two bearing mounting holes 21 are respectively intended to place the bearing for being used for installing engine output shaft and reducer shaft.
From figure 3, it can be seen that having multiple lightening holes on the load in order to reduce whole aircraft, the second mounting bracket 3
31。
Steering wheel fixed mount 8 is fixed on the lower section of the first mounting bracket 2, for being fixedly connected with steering wheel.Shock structure 6 is six,
It is symmetricly set between two bottom plates 1 and buffer board 4, effectively the pressure between buffering engine 7 and bottom plate 1 (aircraft).
It should be appreciated that specific embodiment described above is only used for explaining the utility model, it is not used to limit this reality
With new.The obvious changes or variations extended out by spirit of the present utility model is still in protection of the present utility model
Among scope.
Claims (6)
1. a kind of installing mechanism of high reliability aircraft engine, it is characterised in that including：It is fixed on carry-on two flat
Row set bottom plate (1), be horizontally set on above the bottom plate (1) buffer board (4), sequentially pass through the bottom plate (1) ease up
The support column (5) of punching (4), it is erected between the bottom plate (1) and buffer board (4) and is set on the support column (5)
Shock structure (6) and the first mounting bracket (2) and the second mounting bracket (3) for being vertically set on buffer board (4) two ends, engine (7)
On the first mounting bracket (2) and the second mounting bracket (3).
2. the installing mechanism of high reliability aircraft engine according to claim 1, it is characterised in that first peace
Shelving on (2) has four screw holes (22) for being used for stationary engine (7).
3. the installing mechanism of high reliability aircraft engine according to claim 1 or 2, it is characterised in that described
There are two bearing mounting holes (21) for being used for installing bearing, the output shaft and reducer shaft of engine (7) on one mounting bracket (2)
It is erected at respectively by bearing on first mounting bracket (2).
4. the installing mechanism of high reliability aircraft engine according to claim 3, it is characterised in that second peace
Shelving has multiple lightening holes (31) on (3).
5. the installing mechanism of high reliability aircraft engine according to claim 1, it is characterised in that the fitting machine
Structure also includes the steering wheel fixed mount (8) being fixedly connected with steering wheel, and the steering wheel fixed mount (8) is fixedly connected with the first mounting bracket (2)
Bottom.
6. the installing mechanism of high reliability aircraft engine according to claim 1, it is characterised in that the shock structure
(6) it is six.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188051.0U CN206502033U (en) | 2017-02-28 | 2017-02-28 | A kind of installing mechanism of high reliability aircraft engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188051.0U CN206502033U (en) | 2017-02-28 | 2017-02-28 | A kind of installing mechanism of high reliability aircraft engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206502033U true CN206502033U (en) | 2017-09-19 |
Family
ID=59841022
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720188051.0U Active CN206502033U (en) | 2017-02-28 | 2017-02-28 | A kind of installing mechanism of high reliability aircraft engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206502033U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697304A (en) * | 2017-02-28 | 2017-05-24 | 天峋（常州）智能科技有限公司 | High-reliability aircraft engine mounting mechanism |
-
2017
- 2017-02-28 CN CN201720188051.0U patent/CN206502033U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697304A (en) * | 2017-02-28 | 2017-05-24 | 天峋（常州）智能科技有限公司 | High-reliability aircraft engine mounting mechanism |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103879253A (en) | Connecting structure for independent suspension of overweight special vehicle | |
| CN202991989U (en) | Integral installation type metal mesh vibration isolator | |
| CN206502033U (en) | A kind of installing mechanism of high reliability aircraft engine | |
| CN105864341A (en) | High-reliability combined type shock absorber | |
| CN106697304A (en) | High-reliability aircraft engine mounting mechanism | |
| CN108180320A (en) | A kind of long-life fixing device for the installation connection of antidetonation suspension and support | |
| CN205581756U (en) | Desktop computer mainframe box damper | |
| CN203818966U (en) | Independent suspension connecting structure of extra-heavy special vehicle | |
| CN201421170Y (en) | Foldable air-conditioner mounting rack | |
| CN103410902A (en) | Composite damping shock absorber for textile machinery | |
| CN201800525U (en) | Mounting structure of front-end cooling module | |
| CN204852450U (en) | Anti -vibration cross valve | |
| CN105114702A (en) | Spring supporting and hanging bracket for gas compression pipeline and installation technology of spring supporting and hanging bracket | |
| CN108278472B (en) | A kind of architectural electricity equipment vibration isolation mounting device | |
| CN103832600B (en) | A kind of hanging jockey | |
| CN201503672U (en) | Fast connection structure of LED display module group | |
| CN204979260U (en) | Helicopter carries equipment rack | |
| CN203487668U (en) | Hanging member for glass curtain wall | |
| CN203650361U (en) | Oil pumping unit balance block fixing nut wrench | |
| CN216131308U (en) | Pin-connected panel damping frame | |
| CN204061578U (en) | Use more stable coupling bearing support | |
| CN203331811U (en) | Combined type engine back suspension supporting structure | |
| CN204126849U (en) | A kind of compressor shock-absorbing pin | |
| CN208228562U (en) | A kind of hair dryer motor bracket mounting structure | |
| CN203747248U (en) | Relay rack |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221223 Address after: Room 2211, 22nd Floor, Block D, Zhizhen Building, No. 7 Zhichun Road, Haidian District, Beijing 100088 Patentee after: TIANXUN INNOVATION (BEIJING) TECHNOLOGY CO.,LTD. Address before: Building A1, Zhongke entrepreneurship center, Changzhou science and Education City, No.18, middle Changwu Road, Changzhou City, Jiangsu Province, 213000 Patentee before: VOLITATION (CHANGZHOU) INTELLIGENT TECHNOLOGY CO.,LTD. |