CN208931679U - Canopy for aircraft maintenance - Google Patents
Canopy for aircraft maintenance Download PDFInfo
- Publication number
- CN208931679U CN208931679U CN201821627603.4U CN201821627603U CN208931679U CN 208931679 U CN208931679 U CN 208931679U CN 201821627603 U CN201821627603 U CN 201821627603U CN 208931679 U CN208931679 U CN 208931679U
- Authority
- CN
- China
- Prior art keywords
- telescopic rod
- sliding
- canopy
- slide bar
- cleaning disk
- 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.)
- Expired - Fee Related
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Abstract
The utility model relates to overhaul canopy technical field, it is particularly used for the canopy of aircraft maintenance, including canopy body, cleaning disk is equipped in the canopy body, the center on the downside of the cleaning disk is vertically equipped with slide bar, and the edge on the downside of the cleaning disk is hinged with the first telescopic rod, it is slidably connected on the slide bar equipped with sliding part, the second telescopic rod is hinged on the sliding part, the telescopic end and the first telescopic rod of second telescopic rod are hinged, and the telescopic end of first telescopic rod is equipped with cleaning sponge；To solve the problems, such as that aircraft maintenance canopy squadron aircraft is cleaned.
Description
Technical field
The utility model relates to overhaul canopy technical field, it is particularly used for the canopy of aircraft maintenance.
Background technique
Engineering maintenance is generally divided into two kinds, and one is line maintenances, and one is regular inspection, line maintenance is the boat for ensureing flight
Before, miss the stop and navigate after inspection and troubleshooting, generally carry out wage on machine level ground, regular inspection be mainly aircraft flight for a period of time after
Large size maintenance is generally carried out in maintenance canopy, but can not also be cleaned to aircraft in current canopy, is completed in maintenance
It is also needed afterwards by aircraft handling into cleaning storehouse, is sprayed water and scrubbed after then being powered off to aircraft, can not only wasted in this way
Time also will increase oil consumption.
Utility model content
The purpose of this utility model is to provide the canopies overhauled for aircraft, to solve aircraft maintenance canopy squadron aircraft
The problem of being cleaned.
In order to solve the above technical problems, the utility model uses following technical scheme:
A kind of canopy for aircraft maintenance, including canopy body, interior be equipped with of the canopy body cleans disk, under the cleaning disk
The center of side is vertically equipped with slide bar, and the edge on the downside of the cleaning disk is hinged with the first telescopic rod, the company of sliding on the slide bar
It is equipped with sliding part, the second telescopic rod, the telescopic end and the first telescopic rod of second telescopic rod are hinged on the sliding part
Hingedly, the telescopic end of first telescopic rod is equipped with cleaning sponge.
Preferably, further technical solution is, the upper end of side is equipped with sliding rail in the canopy body, slides on the sliding rail
It is connected with connector, the lower end of the connector is connected with cleaning disk.
Further technical solution is that the sliding rail sets there are two and is oppositely arranged, and the sliding rail is in " L " font,
Including integrally formed vertical part and transverse part, the upper end of the vertical part is connected with the upper end of side in canopy body, the lower end of the vertical part with
One end of transverse part is connected, and the transverse part is equipped with sliding slot；
There are gaps between the transverse part of described two sliding rails；
The connector includes integrally formed transverse slat and vertical bar, the upper end of the vertical bar and the middle section phase on the downside of transverse slat
Even, the transverse slat is set to the upside of transverse part, and the lower end of the vertical bar is pierced by from gap and is connected with cleaning disk, the cross
The lower end of plate is equipped with pulley, and the pulley is set in sliding slot.
Further technical solution is that the inner hollow of the slide bar forms vertical cavity, rotation in the cavity
It is connected with screw rod, flange nut is arranged on the screw rod, it is logical that the connection being connected with cavity is vertically equipped on the slide bar
Road is connected with connecting rod on the flange nut, and the connecting rod is pierced by cavity from interface channel and is connected with sliding part.
Further technical solution is, the sliding part in a ring and is set on slide bar, and the interface channel is set
There are two above and along the radially uniform distribution of slide bar, the connecting rod is adapted with interface channel, the connecting rod and cunning
The inner wall of moving part is connected, and the fixing end of second telescopic rod is hinged on the outer wall of sliding part.
Further technical solution is that first telescopic rod is equipped with side more than two and on the downside of cleaning disk
The distribution of edge annular array, second telescopic rod are adapted with the first telescopic rod.
Compared with prior art, the utility model has the beneficial effects that by the way that cleaning disk is arranged in canopy body, and clear
Slide bar is arranged in center on the downside of clean disk, is slidably connected on slide bar and sliding part is arranged, and hinged second flexible on sliding part
In hinged first telescopic rod in downside of cleaning disk cleaning sponge is arranged in the telescopic end of the first telescopic rod, and second is stretched in bar
The telescopic end of contracting bar is hinged on the first telescopic rod, and turning for the first telescopic rod can be driven by the stretching motion of the second telescopic rod
It is dynamic, and the angle that the first telescopic rod rotates is adjusted with the second telescopic rod stretching motion by sliding of the sliding part on slide bar
Degree, while being shortened by the elongation of the first telescopic rod itself, to adjust the position of cleaning sponge, to enable cleaning sponge to winged
It is cleaned outside machine, and guarantees to carry out comprehensive cleaning.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the canopy overhauled for aircraft.
Fig. 2 is the connection schematic diagram of sliding rail and connector.
Fig. 3 is the structural schematic diagram of slide bar and sliding part.
Fig. 4 is the structural schematic diagram of slide bar.
In figure: 1, canopy body；2, disk is cleaned；3, slide bar；4, sliding part；5, the first telescopic rod；6, the second telescopic rod；7, clear
Clean sponge；8, connector；9, sliding rail；31, cavity；32, screw rod；33, flange nut；34, interface channel；35, connecting rod；81,
Transverse slat；82, vertical bar；83, pulley；91, vertical part；92, transverse part；93, sliding slot；94, gap.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only used to explain
The utility model is not used to limit the utility model.
Fig. 1-4 shows the embodiment of the canopy for aircraft maintenance.
Embodiment one:
A kind of canopy for aircraft maintenance, including canopy body 1, the canopy body 1 is interior to be equipped with cleaning disk 2, the cleaning circle
The center of 2 downside of disk is vertically equipped with slide bar 3, and the edge of 2 downside of cleaning disk is hinged with the first telescopic rod 5, the slide bar 3
On be slidably connected equipped with sliding part 4, be hinged with the second telescopic rod 6, the telescopic end of second telescopic rod 6 on the sliding part 4
Hinged with the first telescopic rod 5, the telescopic end of first telescopic rod 5 is equipped with cleaning sponge 7.
Referring to attached drawing 1, slide bar is set by the way that cleaning disk 2 is arranged in canopy body 1, and at the center of 2 downside of cleaning disk
3, it is slidably connected on slide bar 3 and sliding part 4 is set, and hinged second telescopic rod 6 on sliding part 4, in the downside of cleaning disk 2
Hinged first telescopic rod 5 is arranged cleaning sponge 7 in the telescopic end of the first telescopic rod 5, and the telescopic end of the second telescopic rod 6 is cut with scissors
It connects on the first telescopic rod 5, the rotation of the first telescopic rod 5 can be driven by the stretching motion of the second telescopic rod 6, and pass through
Sliding of the sliding part 4 on slide bar 3 adjusts the angle of the first telescopic rod 5 rotation with 6 stretching motion of the second telescopic rod, leads to simultaneously
The elongation for crossing the first telescopic rod 5 itself is shortened, to adjust the position of cleaning sponge 7, to enable cleaning sponge 7 to aircraft exterior
It is cleaned, and guarantees to carry out comprehensive cleaning.
It cleans disk 2 and is flexibly connected and be arranged in canopy body 1, can be driven by activity of the cleaning disk 2 in canopy body 1 clear
The movement of clean sponge 7, comprehensive cleaning can be carried out to aircraft exterior by being further ensured that.
Before being cleaned using cleaning sponge 7 to aircraft exterior, first aircraft exterior can also be rinsed, specifically
Sliding rail can be set in the downside of canopy body 1, and the water pipe for setting " door " font that is slidably connected on sliding rail, on water pipe
Water outlet is set, and sprinkler head is set on water outlet, drives sprinkler head to aircraft by water pipe sliding on sliding rail
External upside and the left and right sides carries out hydro-peening, in order to which cleaning sponge 7 cleans aircraft exterior later, and cleans sea
Silk floss 7 may also function as the effect of water suction, the remaining moisture of aircraft exterior can be siphoned away.
First telescopic rod 5 includes pars contractilis and fixed part, and one end of fixed part is hinged on the downside of cleaning disk 2, fixed
Telescopic cavity is provided in portion, pars contractilis, which is flexibly connected, to be arranged in telescopic cavity, and the telescopic end of the second telescopic rod 6 is mutually cut with scissors with fixed part
It connects.
Supporting steel frame can be set in canopy body 1, supporting steel frame plays the role of firm canopy body 1.
Embodiment two:
The upper end of 1 inside of canopy body is equipped with sliding rail 9, is slidably connected on the sliding rail 9 equipped with connector 8, the connection
The lower end of part 8 is connected with cleaning disk 2.
On the basis of example 1, referring to attached drawing 1, cunning can specifically be passed through by cleaning disk 2 with being flexibly connected for canopy body 1
Rail 9 and connector 8 are realized, drive the movement of cleaning disk 2, by sliding of the connector 8 on sliding rail 9 to realize cleaning sponge
7 can carry out comprehensive cleaning to aircraft exterior.
Embodiment three:
The sliding rail 9 sets there are two and is oppositely arranged, and the sliding rail 9 is in " L " font, including integrally formed vertical part 91
It is connected with the upper end of transverse part 92, the vertical part 91 with the upper end of 1 inside of canopy body, the lower end of the vertical part 91 and one end of transverse part 92
It is connected, the transverse part 92 is equipped with sliding slot 93；
There are gaps 94 between the transverse part 92 of described two sliding rails 9；
The connector 8 includes integrally formed transverse slat 81 and vertical bar 82,81 downside of upper end and transverse slat of the vertical bar 82
Middle section be connected, the transverse slat 81 is set to the upside of transverse part 92, the lower end of the vertical bar 82 be pierced by from gap 94 and with it is clear
Clean disk 2 is connected, and the lower end of the transverse slat 81 is equipped with pulley 83, and the pulley 83 is set in sliding slot 93.
On the basis of example 2, referring to attached drawing 1 and attached drawing 2, connector 8 specifically includes transverse slat 81 and vertical bar 82, sliding
There are two can specifically include vertical part 91 and transverse part 92 sliding slot 93 is arranged, and in the downside of transverse slat 81 in the setting of rail 9 on transverse part 92
Pulley 83 is set, pulley 83 is slidably connected and is set in sliding slot 93, can be driven by sliding of the pulley 83 in sliding slot 93
The sliding of connector 8, to realize being slidably connected between connector 8 and sliding rail 9.
Two sliding rails 9 are oppositely arranged, and two sliding rails 9 can be symmetrical along the vertical center in gap 94, two transverse parts
92 between two vertical parts 91, and gap 94 is adapted with vertical bar 82, guarantee that the lower end of vertical bar 82 can be pierced by from gap 94, and
Guarantee that gap 92 does not influence the movement of vertical bar 82.
Example IV:
The inner hollow of the slide bar 3 forms vertical cavity 31, and rotation connection is equipped with screw rod 32, institute in the cavity 31
It states and is arranged with flange nut 33 on screw rod 32, the interface channel 34 being connected with cavity 31 is vertically equipped on the slide bar 3, it is described
Connecting rod 35 is connected on flange nut 33, the connecting rod 35 is pierced by cavity 31 from interface channel 34 and is connected with sliding part 4.
On the basis of embodiment three, referring to attached drawing 3 and attached drawing 4, vertical cavity 31 is set inside slide bar 3, and
Screw rod 32 is set in cavity 31, flange nut 33 is arranged on screw rod 32, cavity 31 is set on the side wall of slide bar 3 and wants to be connected to
Interface channel 34, and the connecting rod 35 being connected on flange nut 33 is pierced by from interface channel 34, make connecting rod 35 with
Sliding part 4 is connected, and flange nut 33 can be driven to move up and down by the rotation of screw rod 32 in this way, to drive on sliding part 4
Lower movement is realized and slides up and down connection between sliding part 4 and slide bar 3.
The upper end of slide bar 3 is provided with motor, and the output shaft of motor is connected with screw rod 32, and motor can rotate and reverse
Motor.
Embodiment five:
The sliding part 4 in a ring and is set on slide bar 3, and the interface channel 34 is equipped with more than two and along cunning
The radially uniform distribution of bar 3, the connecting rod 35 are adapted with interface channel 34, the inner wall of the connecting rod 35 and sliding part 4
It is connected, the fixing end of second telescopic rod 6 is hinged on the outer wall of sliding part 4.
On the basis of example IV, referring to attached drawing 1, attached drawing 3 and attached drawing 4, interface channel 34 are set as two or more simultaneously
Along the radially uniform distribution of slide bar 3, and by more than two connecting rods 35 come connecting flange nut 33 and sliding part 4, into
One step guarantees the stability connected between sliding part 4 and flange nut 33.
Connecting rod 35 is adapted with interface channel 34, first is that being quantitatively adapted, guarantees that each interface channel 34 is right
Ying Yigen connecting rod 35 guarantees that connecting rod 35 can play connection method second is that guaranteeing that connecting rod 35 can be pierced by from interface channel 34
The effect of blue nut 33 and sliding part 4.
Embodiment six:
First telescopic rod 5 is equipped with edge annular array distribution more than two and in 2 downside of cleaning disk, described
Second telescopic rod 6 is adapted with the first telescopic rod 5.
On the basis of embodiment five, referring to attached drawing 1, the distribution of the edge circular array formula of 2 downside of disk is cleaned
There are two the first above telescopic rod 5, the second telescopic rod 6 is adapted with the first telescopic rod 5, guarantees the first telescopic rod 5 and second
The quantity of telescopic rod 6 is identical.
First telescopic rod 5 and the second telescopic rod 6 are existing electric telescopic rod, are by the way that battery is arranged in canopy body 1
First telescopic rod 5 and the second telescopic rod 6 provide electric energy.
Although reference be made herein to the utility model is described in multiple explanatory embodiments of the utility model, still,
It should be understood that those skilled in the art can be designed that a lot of other modification and implementations, these modifications and implementations
It will fall within scope and spirit disclosed in the present application.More specifically, it discloses in the application, drawings and claims
In range, can building block to theme combination layout and/or layout carry out a variety of variations and modifications.In addition to building block
And/or outside the modification and improvement of layout progress, to those skilled in the art, other purposes also be will be apparent.
Claims (6)
1. a kind of canopy for aircraft maintenance, including canopy body (1), it is characterised in that: be equipped with cleaning disk in the canopy body (1)
(2), the center on the downside of cleaning disk (2) is vertically equipped with slide bar (3), and the edge on the downside of cleaning disk (2) is hinged with
First telescopic rod (5) is slidably connected on the slide bar (3) equipped with sliding part (4), is hinged with second on the sliding part (4) and stretches
Contracting bar (6), the telescopic end and the first telescopic rod (5) of second telescopic rod (6) hingedly, stretch by first telescopic rod (5)
End is equipped with cleaning sponge (7).
2. the canopy according to claim 1 for aircraft maintenance, it is characterised in that: the upper end on the inside of the canopy body (1)
Equipped with sliding rail (9), it is slidably connected on the sliding rail (9) equipped with connector (8), the lower end of the connector (8) and cleaning disk
(2) it is connected.
3. the canopy according to claim 2 for aircraft maintenance, it is characterised in that: the sliding rail (9) sets there are two simultaneously
And be oppositely arranged, the sliding rail (9) is in " L " font, including integrally formed vertical part (91) and transverse part (92), the vertical part (91)
Upper end be connected with the upper end on the inside of canopy body (1), the lower end of the vertical part (91) is connected with one end of transverse part (92), the transverse part
(92) sliding slot (93) are equipped with；
There are gap (94) between the transverse part (92) of described two sliding rails (9)；
The connector (8) includes integrally formed transverse slat (81) and vertical bar (82), the upper end of the vertical bar (82) and transverse slat
(81) middle section on the downside of is connected, and the transverse slat (81) is set to the upside of transverse part (92), and the lower end of the vertical bar (82) is from gap
(94) it is pierced by and is connected with cleaning disk (2), the lower end of the transverse slat (81) is equipped with pulley (83), pulley (83) setting
In sliding slot (93).
4. the canopy according to claim 1 for aircraft maintenance, it is characterised in that: the inner hollow of the slide bar (3)
It is formed vertical cavity (31), rotation connection is equipped with screw rod (32) in the cavity (31), is arranged with method on the screw rod (32)
Blue nut (33) is vertically equipped with the interface channel (34) being connected with cavity (31), the flange nut on the slide bar (3)
(33) be connected on connecting rod (35), the connecting rod (35) from interface channel (34) be pierced by cavity (31) and with sliding part (4)
It is connected.
5. the canopy according to claim 4 for aircraft maintenance, it is characterised in that: the sliding part (4) is in a ring simultaneously
And be set on slide bar (3), the interface channel (34) is equipped with two or more and along the radially uniform distribution of slide bar (3), institute
Connecting rod (35) to be stated to be adapted with interface channel (34), the connecting rod (35) is connected with the inner wall of sliding part (4), and described second
The fixing end of telescopic rod (6) is hinged on the outer wall of sliding part (4).
6. the canopy according to claim 1 for aircraft maintenance, it is characterised in that: first telescopic rod (5) is equipped with
Edge annular array distribution more than two and on the downside of cleaning disk (2), second telescopic rod (6) and the first telescopic rod
(5) it is adapted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821627603.4U CN208931679U (en) | 2018-10-08 | 2018-10-08 | Canopy for aircraft maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821627603.4U CN208931679U (en) | 2018-10-08 | 2018-10-08 | Canopy for aircraft maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208931679U true CN208931679U (en) | 2019-06-04 |
Family
ID=66723679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821627603.4U Expired - Fee Related CN208931679U (en) | 2018-10-08 | 2018-10-08 | Canopy for aircraft maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208931679U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109094813A (en) * | 2018-10-08 | 2018-12-28 | 成都戎创航空科技有限公司 | Canopy for aircraft maintenance |
-
2018
- 2018-10-08 CN CN201821627603.4U patent/CN208931679U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109094813A (en) * | 2018-10-08 | 2018-12-28 | 成都戎创航空科技有限公司 | Canopy for aircraft maintenance |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190604 Termination date: 20191008 |