CN108069361A - aircraft engine maintenance supporting member - Google Patents
aircraft engine maintenance supporting member Download PDFInfo
- Publication number
- CN108069361A CN108069361A CN201611012145.9A CN201611012145A CN108069361A CN 108069361 A CN108069361 A CN 108069361A CN 201611012145 A CN201611012145 A CN 201611012145A CN 108069361 A CN108069361 A CN 108069361A
- Authority
- CN
- China
- Prior art keywords
- engine
- supporting member
- guide rail
- upper boom
- aircraft 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.)
- Pending
Links
- 238000012423 maintenance Methods 0.000 title claims abstract description 26
- 230000007246 mechanism Effects 0.000 claims abstract description 20
- 239000013013 elastic material Substances 0.000 claims abstract description 12
- 230000008439 repair process Effects 0.000 abstract description 2
- 230000008901 benefit Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
- B66F7/06—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
- B66F7/28—Constructional details, e.g. end stops, pivoting supporting members, sliding runners adjustable to load dimensions
Landscapes
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Geology (AREA)
- Mechanical Engineering (AREA)
- Structural Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The present invention provides aircraft engine maintenance supporting members, pass through first support bar and slip of the second support bar on guide rail mechanism, before maintenance support component is moved to aero-engine, the foot-operated pedal that presses causes supporting member to be tilted to engine side, elastic material is made to be in preloading condition, after engine is put into the one side cambered surface of curved support plate, gradually loosens and trampled to pressing pedal so that engine is gradually rolled in curved support plate；Pass through first support bar and slip of the second support bar on guide rail mechanism, engine is moved to spacious position to overhaul, it can be by the first upper boom of adjusting and the locking device of the second upper boom, to adjust the whole height of maintenance support component, to adapt to the repair height of engine.It is foot-operated to press pedal when needing engine removal so that supporting member tilts, and cylindrical engine is helped gradually to rotate out curved support plate.
Description
Technical field
The invention belongs to aircraft engine maintenance device field, more particularly, to aircraft engine maintenance supporting member.
Background technology
Aero-engine is generally when needing repairing, it is necessary to which the separately connection of engine and aircraft/helicopter, then passes through
Aero-engine from piggyback pod is removed, then carries out maintenance work by lifting or lifting device；It will using lifting or lifting gear
The process that motor driven force cabin removes, it is time-consuming and laborious, it is very expensive so as to cause maintenance cost.
The content of the invention
In view of this, the present invention is directed to propose aircraft engine maintenance supporting member, to facilitate aero-engine from power
Cabin removes.
In order to achieve the above objectives, the technical proposal of the invention is realized in this way：
Aircraft engine maintenance supporting member, including guide rail mechanism and curved support plate, curved support plate one end is equipped with perpendicular
Straight backup plate, curved support plate both sides are symmetrically arranged with the baffle being connected with the vertical backup plate, and curved baffle lower part is close to vertical
The one side of backup plate be equipped with first support bar, one side of the curved baffle lower part away from vertical backup plate be equipped with second support bar, first
Strut includes the first upper boom and the first lower beam for being in axial sliding connection with the first upper boom, second support bar include the second upper boom and with
The second lower beam that second upper boom is in axial sliding connection, the second lower beam lower part are equipped with elastic material, first support bar and second support bar
Bottom is equipped with the sliding equipment with guide rail mechanism cooperation.
Further, the curved support plate and vertical backup plate are retractable plate.
Further, the elastic material is spring.
Further, the guide rail mechanism includes guide rail platform and the guide rail being arranged on guide rail platform.
Further, the guide rail is equipped with groove, and sliding equipment is the idler wheel with groove match.
Further, the vertical backup plate is equipped with lamp body.
Further, it is equipped with above the elastic material and presses pedal.
Further, first low stem casing is arranged in the first upper boom, and the second low stem casing is arranged in the second upper boom, on first
Bar is equipped with to fix the retaining mechanism of the first lower beam, and the second upper boom is equipped with to fix the retaining mechanism of the second lower beam.
Compared with the prior art, aircraft engine maintenance supporting member of the present invention has the advantage that：
Aircraft engine maintenance supporting member of the present invention by the setting of guide rail and supporting rod, is realized to hair
The level of motivation and the adjusting of vertical position, the setting of arc expansion plate and telescopic backrest are realized to different size of cylinder
The carrying of shape engine；Simultaneously by setting spring on telescopic rod, contribute to the handling of cylindrical engine；The equipment designs
Rationally, it is easy to operate, the maintenance efficiency of engine is substantially increased, it is time saving and energy saving.
Description of the drawings
The attached drawing for forming the part of the present invention is used for providing a further understanding of the present invention, schematic reality of the invention
Example and its explanation are applied for explaining the present invention, is not constituted improper limitations of the present invention.In the accompanying drawings：
Fig. 1 is the aircraft engine maintenance supporting member structure diagram described in the embodiment of the present invention；
Reference sign：
1- guide rail mechanisms；11- guide rail platforms；12- guide rails；2- curved support plates；The vertical backup plates of 3-；4- baffles；5- first
Supporting rod；The first upper booms of 51-；The first lower beams of 52-；6- second support bars；The second upper booms of 61-；The second lower beams of 62-；7- elastic materials；
8- presses pedal.
Specific embodiment
It should be noted that in the case where there is no conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.
In the description of the present invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instructions such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of the description present invention and simplifies description rather than instruction or dark
Show that signified device or element there must be specific orientation, with specific azimuth configuration and operation, thus it is it is not intended that right
The limitation of the present invention.In addition, term " first ", " second " etc. are only used for description purpose, and it is not intended that instruction or hint phase
To importance or the implicit quantity for indicating indicated technical characteristic.The feature for defining " first ", " second " etc. as a result, can
To express or implicitly include one or more this feature.In the description of the present invention, unless otherwise indicated, " multiple "
It is meant that two or more.
In the description of the present invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or be integrally connected；It can
To be mechanical connection or be electrically connected；It can be directly connected, can also be indirectly connected by intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood by concrete condition
Concrete meaning in the present invention.
The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
Aircraft engine maintenance supporting member, as shown in Figure 1, including guide rail mechanism 1 and curved support plate 2, curved support
2 one end of plate is equipped with vertical backup plate 3, and 2 both sides of curved support plate are symmetrically arranged with the baffle 4 being connected with vertical backup plate 3, curved baffle
2 lower parts are equipped with first support bar 5 close to the one side of vertical backup plate 3, and one side of 2 lower part of curved baffle away from vertical backup plate 3 is equipped with
Second support bar 6, first support bar 5 include the first upper boom 51 and the first lower beam 52 being in axial sliding connection with the first upper boom 51,
Second support bar 6 includes the second upper boom 61 and the second lower beam 62 for being in axial sliding connection with the second upper boom 61, under the second lower beam 62
Portion is equipped with elastic material 7, and first support bar 5 and 6 bottom of second support bar are equipped with the sliding equipment coordinated with guide rail mechanism 1.
Curved support plate 2 and vertical backup plate 3 are retractable plate.To adapt to the transport of different size engine.
Elastic material 7 is spring.
Guide rail mechanism 1 includes guide rail platform 11 and the guide rail 12 being arranged on guide rail platform 11.
Guide rail 12 is equipped with groove, and sliding equipment is the idler wheel with groove match.
Backup plate 3 is equipped with lamp body.When enging cabin environment is dark, lamp body can be opened, illuminates ambient enviroment.
Elastic material 7 is equipped with and presses pedal 8.
First lower beam 52 is sheathed in first upper boom 51, and the second lower beam 62 is sheathed in second upper boom 61, the
One upper boom 51 is equipped with to fix the retaining mechanism of the first lower beam 52, and the second upper boom 61 is equipped with to fix the second lower beam 62
Retaining mechanism.
The specific workflow of this example is as follows：
By first support bar 5 and slip of the second support bar 6 on guide rail mechanism 1, maintenance support component is moved to
Before aero-engine, the foot-operated pedal 8 that presses causes supporting member to be tilted to engine side, and elastic material is made to be in preloading condition,
After engine is put into the one side cambered surface of curved support plate 2, gradually loosen to pressing trampling for pedal 8 so that engine by
It is gradually rolled in curved support plate 2；By first support bar 5 and slip of the second support bar 6 on guide rail mechanism 1, will start
Machine is moved to spacious position and is overhauled, can be by the first upper boom 51 of adjusting and the locking device of the second upper boom 61, to adjust
The whole height of maintenance support component is saved, to adapt to the repair height of engine.It is foot-operated to press when needing engine removal
Pedal 8 so that supporting member tilts, and cylindrical engine is helped gradually to rotate out curved support plate 2.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modifications, equivalent replacements and improvements are made should all be included in the protection scope of the present invention god.
Claims (8)
1. aircraft engine maintenance supporting member, it is characterised in that：Including guide rail mechanism (1) and curved support plate (2), the arc
Shape support plate (2) one end is equipped with vertical backup plate (3), and curved support plate (2) both sides are symmetrically arranged with and the vertical backup plate
(3) connected baffle (4), curved support plate (2) lower part are equipped with first support bar (5) close to the one side of vertical backup plate (3),
The one side of curved support plate (2) lower part away from vertical backup plate (3) is equipped with second support bar (6), the first support bar (5)
The first lower beam (52) being in axial sliding connection including the first upper boom (51) and with first upper boom (51), the second support bar
(6) the second upper boom (61) and the second lower beam (62) for being in axial sliding connection with second upper boom (61) are included, under described second
Bar (62) lower part is equipped with elastic material (7), and first lower beam (52) and the second lower beam (62) bottom are equipped with and guide rail mechanism (1)
The sliding equipment of cooperation.
2. aircraft engine maintenance supporting member according to claim 1, it is characterised in that：The curved support plate (2)
And vertical backup plate (3) is retractable plate.
3. aircraft engine maintenance supporting member according to claim 1, it is characterised in that：The elastic material (7) is bullet
Spring.
4. aircraft engine maintenance supporting member according to claim 1, it is characterised in that：Guide rail mechanism (1) bag
Include guide rail platform (11) and the guide rail (12) being arranged on the guide rail platform (11).
5. aircraft engine maintenance supporting member according to claim 4, it is characterised in that：The guide rail (12) is equipped with
Groove, the sliding equipment are the idler wheel with the groove match.
6. the aircraft engine maintenance supporting member stated according to claim 1, it is characterised in that：The backup plate (3) is equipped with lamp
Body.
7. aircraft engine maintenance supporting member according to claim 1, it is characterised in that：Above the elastic material (7)
Equipped with pressing pedal (8).
8. aircraft engine maintenance supporting member according to claim 1, it is characterised in that：First lower beam (52) set
In first upper boom (51), second lower beam (62) is sheathed in second upper boom (61), first upper boom
(51) equipped with for fixing the retaining mechanism of first lower beam (52), second upper boom (61) is equipped with to fix second
The retaining mechanism of lower beam (62).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611012145.9A CN108069361A (en) | 2016-11-17 | 2016-11-17 | aircraft engine maintenance supporting member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611012145.9A CN108069361A (en) | 2016-11-17 | 2016-11-17 | aircraft engine maintenance supporting member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108069361A true CN108069361A (en) | 2018-05-25 |
Family
ID=62163503
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611012145.9A Pending CN108069361A (en) | 2016-11-17 | 2016-11-17 | aircraft engine maintenance supporting member |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108069361A (en) |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3605947A1 (en) * | 1986-02-25 | 1987-08-27 | Retter Gerhard Dipl Ing Fh | Device for checking the uncertainty in length measurement of coordinate measuring machines |
| CN203359903U (en) * | 2013-06-21 | 2013-12-25 | 泸州华西机械有限责任公司 | Hydraulic lifting platform used for aloft work |
| CN203754004U (en) * | 2014-04-01 | 2014-08-06 | 上海化学工业区升达废料处理有限公司 | Emptying device for ton barrel |
| CN203945859U (en) * | 2014-07-14 | 2014-11-19 | 莆田学院 | A kind of writing implement fixed mechanism |
| CN104438873A (en) * | 2014-11-18 | 2015-03-25 | 常州市立威刀具有限公司 | Rolling type die holder |
| CN204600282U (en) * | 2015-05-07 | 2015-09-02 | 常州白相相文化传媒有限公司 | Spray Flavouring jar |
| CN204754216U (en) * | 2015-07-30 | 2015-11-11 | 广西建工集团第五建筑工程有限责任公司 | But telescopic tube |
| CN205023542U (en) * | 2015-08-04 | 2016-02-10 | 中国人民解放军91829部队 | Fixed adjustable loading platform |
| CN205325792U (en) * | 2015-12-09 | 2016-06-22 | 重庆顺泰食品有限公司 | Skin of soya -bean milk cutting device |
| CN205383397U (en) * | 2015-12-03 | 2016-07-13 | 中国航空动力机械研究所 | Aeroengine maintains supporting member |
| CN206634973U (en) * | 2016-11-17 | 2017-11-14 | 天津奥华通航科技有限公司 | Aero-engine support meanss |
-
2016
- 2016-11-17 CN CN201611012145.9A patent/CN108069361A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3605947A1 (en) * | 1986-02-25 | 1987-08-27 | Retter Gerhard Dipl Ing Fh | Device for checking the uncertainty in length measurement of coordinate measuring machines |
| CN203359903U (en) * | 2013-06-21 | 2013-12-25 | 泸州华西机械有限责任公司 | Hydraulic lifting platform used for aloft work |
| CN203754004U (en) * | 2014-04-01 | 2014-08-06 | 上海化学工业区升达废料处理有限公司 | Emptying device for ton barrel |
| CN203945859U (en) * | 2014-07-14 | 2014-11-19 | 莆田学院 | A kind of writing implement fixed mechanism |
| CN104438873A (en) * | 2014-11-18 | 2015-03-25 | 常州市立威刀具有限公司 | Rolling type die holder |
| CN204600282U (en) * | 2015-05-07 | 2015-09-02 | 常州白相相文化传媒有限公司 | Spray Flavouring jar |
| CN204754216U (en) * | 2015-07-30 | 2015-11-11 | 广西建工集团第五建筑工程有限责任公司 | But telescopic tube |
| CN205023542U (en) * | 2015-08-04 | 2016-02-10 | 中国人民解放军91829部队 | Fixed adjustable loading platform |
| CN205383397U (en) * | 2015-12-03 | 2016-07-13 | 中国航空动力机械研究所 | Aeroengine maintains supporting member |
| CN205325792U (en) * | 2015-12-09 | 2016-06-22 | 重庆顺泰食品有限公司 | Skin of soya -bean milk cutting device |
| CN206634973U (en) * | 2016-11-17 | 2017-11-14 | 天津奥华通航科技有限公司 | Aero-engine support meanss |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203826828U (en) | Maintenance and conveyance platform for switch cabinet breaker | |
| CN105489808B (en) | A kind of battery component for engineering truck | |
| CN102101531B (en) | Lift device for replacing dynamic or static components of helicopter-type aircraft | |
| CN210761056U (en) | Large airplane fuselage transport vehicle | |
| CN104843038A (en) | Cart with extension-type wheels | |
| KR102433584B1 (en) | Airliftable forklifts and loading methods | |
| CN107293979B (en) | Auxiliary device for replacing and loading transformer | |
| CN206542102U (en) | A kind of universal electronic inspection trolley of middle-placed switch cabinet | |
| CN106532526B (en) | A kind of switch cabinet combining auxiliary device | |
| CN206634973U (en) | Aero-engine support meanss | |
| CN108069361A (en) | aircraft engine maintenance supporting member | |
| CN214044700U (en) | Special trolley for replacing current transformer of armored switch cabinet | |
| CN108860648A (en) | A kind of Filtting device of the main landing gear for aviation field | |
| CN112134199A (en) | Automatic turning device of handcart circuit breaker | |
| KR101854093B1 (en) | The fit jack of commercial vehicle | |
| CN209159746U (en) | A kind of device at handtruck of supporting engine assembly | |
| CN110509241A (en) | Tooling is gone up and down online for accessory under locomotive | |
| CN103738884A (en) | Double-column gantry double-cylinder hydraulic lifting machine | |
| CN206096183U (en) | On -vehicle full -automatic collapsible convertible test bench | |
| KR101198732B1 (en) | Method for set up transformer of ship | |
| CN205542946U (en) | A battery pack for engineering vehicle | |
| CN210505390U (en) | Dismounting and mounting vehicle for main landing gear of airplane | |
| CN210092704U (en) | Detachable portable overhauls device | |
| CN202753951U (en) | Auxiliary inclined shaft construction platform car | |
| CN202139003U (en) | Lifting device for automobiles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180525 |