CN110203122A - A kind of radome of fighter dismounting unwheeling - Google Patents
A kind of radome of fighter dismounting unwheeling Download PDFInfo
- Publication number
- CN110203122A CN110203122A CN201910437595.XA CN201910437595A CN110203122A CN 110203122 A CN110203122 A CN 110203122A CN 201910437595 A CN201910437595 A CN 201910437595A CN 110203122 A CN110203122 A CN 110203122A
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- CN
- China
- Prior art keywords
- radome
- unwheeling
- fighter
- fixed
- guide rail
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
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- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Details Of Aerials (AREA)
Abstract
The invention belongs to airplane design technical fields, and in particular to a kind of radome of fighter dismounting unwheeling；Radome of fighter dismounting unwheeling of the invention includes transmission mechanism, guide rail, radome bracket, fixed device, height adjustment mechanism, ground surface platform；The transmission mechanism and the radome bracket are mounted on the guide rail, and the transmission mechanism drives the radome bracket to move along the guide rail；With the fixed device of fixed radar cover on the radome bracket；The guide rail is fixed by height adjustment mechanism and ground surface platform；Radome of fighter of the invention dismounts unwheeling device, and using the form of bracket combination guide rail, with origin reference location plus the thinking of relative motion, radome of fighter is conveniently dismantled or installed by fixing force transfer direction, is provided simultaneously with radome storage unwheeling function.
Description
Technical field
The invention belongs to airplane design technical fields, are related to Aircraft Flight Test auxiliary mould technology, and in particular to a kind of aircraft
Radome dismounts unwheeling.
Background technique
The dismounting tooling of radome of fighter has the disadvantage in that (1) fixed bracket is not firm at present, easily shakes；(2) bracket
Lifting is inconvenient, and lifting is slow；(3) safety is bad, is easy to shake, there is security risk；(4) operability is poor, is not easy to personnel behaviour
Make；(5) mobile inconvenient than cumbersome.
Dismount tooling due to lacking simple and practical radome, take a flight test at present stand engineering radome dismounting work very not
Just, it is many times dismounted using mobile platform combination manpower, it is not only troublesome in poeration, but also have security risk.
Summary of the invention
The purpose of the present invention is: a kind of radome of fighter dismounting unwheeling device is designed, to realize that it is fast that radome of fighter facilitates
Prompt disassembly or installation, while the equipment has both radome storage unwheeling function.
To solve this technical problem, the technical scheme is that a kind of radome of fighter dismounts unwheeling, the aircraft
Radome dismounting unwheeling includes: that transmission mechanism 1, guide rail 2, radome bracket 3, fixed device 4, height adjustment mechanism, ground are flat
Platform；Transmission mechanism 1 is mounted on guide rail 2, and radome bracket 3 is mounted on guide rail 2, driver for propping up radome of fighter
Structure 1 drives radome bracket 3 to move along guide rail 2；With the fixation device 4 of fixed radar cover on radome bracket 3；Guide rail 2
It is fixed by height adjustment mechanism and ground surface platform.
Radome of fighter dismounts unwheeling further include: is mounted on the positioning supporting plate of 2 front end of guide rail, the positioning surface for positioning supporting plate is
The datum clamp face of radome.For being positioned with radome datum clamp face.
The positioning supporting plate is coated by flexible material, prevents aircaft configuration of damaging.
Transmission mechanism 1 includes drive lead screw and the runner for being fixed on drive lead screw end；Drive lead screw is mounted on guide rail 2
On, and it is fixed with radome bracket 3.It can be allowed to move along guide rail 2 with power transmission to radome bracket 3 by can be manually rotated runner
It is dynamic.
Height adjustment mechanism is made of extension sleeve 5, height adjustment screw rod 6, pillar 7, and extension sleeve 5 and ground surface platform are solid
Fixed, pillar 7 is mounted on inside extension sleeve 5；6 lower end of height adjustment screw rod is fixed with ground surface platform, and upper end passes through bracket and branch
Column 7 is fixed.6 riser guide 2 of screw rod can be adjusted by rotation height, to adapt to aircraft altitude.
Extension sleeve 5 is self-lubricating extension sleeve；
Ground surface platform has upper table rank 8 of standing in locomotive work, facilitates operation transmission mechanism 1.
Ground surface platform is equipped with ground fixing device 10 and roller group is fixed, and realizes the mobile turning of radome dismounting unwheeling
It is fixed with ground.
Roller group includes universal wheel 9.
Fixed device 4 is Fixed latches, and Fixed latches are adapted to the dismounting hole on radome；Fixed latches are inserted into radome
On dismounting hole be fixed.
The beneficial effects of the present invention are: radome of fighter of the invention dismounts unwheeling device, using bracket combination guide rail
Form, with origin reference location plus the thinking of relative motion, radome of fighter is conveniently dismantled or is pacified by fixing force transfer direction
Dress is provided simultaneously with radome storage unwheeling function.
Detailed description of the invention
It, below will be to be used to being needed in example of the invention in order to illustrate more clearly of the technical solution that the present invention is implemented
Attached drawing makees simple explain.It is clear that drawings described below is only some embodiments of the present invention, for this field
Technical staff for, without creative efforts, be also possible to obtain other drawings based on these drawings.
Fig. 1 is that rebecca dismounts unwheeling overall structure figure；
Fig. 2 is that rebecca dismounts unwheeling front view；
Fig. 3 is that rebecca dismounts unwheeling left view；
Fig. 4 is that rebecca dismounts unwheeling top view；
Fig. 5 is rebecca assembling and disassembling stand vehicle operation schematic diagram；
Fig. 6 is that radome of fighter dismounts unwheeling installation positioning operation schematic diagram.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.Obviously, described embodiment is
A part of the embodiments of the present invention, rather than whole embodiments.Based on the embodiments of the present invention, the ordinary skill people of this field
Without making creative work, every other embodiment obtained shall fall within the protection scope of the present invention member.
The feature of the various aspects of the embodiment of the present invention is described more fully below.In the following detailed description, it proposes
Many concrete details, so as to complete understanding of the present invention.But for those of ordinary skill in the art, very bright
Aobvious, the present invention can also be implemented in the case where not needing these details.Below to the description of embodiment
Just for the sake of being better understood by showing example of the invention to the present invention.The present invention is not limited to presented below any
Specific setting and method, but cover all product structures covered without departing from the spirit of the invention, method
Any improvement, replacement etc..
In each attached drawing and following description, well known structure and technology is not shown, is caused to avoid to the present invention
It is unnecessary fuzzy.
Radome of fighter assembling and disassembling stand bassinet structure schematic diagram of the invention is as shown in Figure 1, specifically include: transmission mechanism 1, guide rail
2, radome bracket 3, fixed device 4, height adjustment mechanism, ground surface platform；Transmission mechanism 1 is mounted on guide rail 2 by bearing,
Radome bracket 3 is mounted on guide rail 2, transmission mechanism 1 drives radome bracket 3 along guide rail 2 for propping up radome of fighter
It is mobile；With the fixation device 4 of fixed radar cover on radome bracket 3；Guide rail 2 is solid by height adjustment mechanism and ground surface platform
It is fixed.
It can be allowed to move along guide rail with power transmission to radome bracket 3 by can be manually rotated runner.
Guide rail 2 is in addition to mobile for director radar cover bracket 3, and front end is there are one supporting plate is positioned, for pacifying with radome
Datum level positioning is filled, positioning supporting plate has flexible material cladding, prevents aircaft configuration of damaging.Radome bracket 3 is for propping up aircraft
Radome, and be fixed by the dismounting hole that radome Fixed latches are inserted on radome.
Self-lubricating extension sleeve 5, height adjustment screw rod 6 combine to form a set of height adjustment mechanism with pillar 7, can pass through
Rotation height adjusts the runner riser guide 2 of screw rod 6, to adapt to aircraft altitude.
Can stand upper table rank 8 in locomotive work, facilitate the runner of operation drive lead screw.Pass through universal wheel 9 and ground
The mobile turning of radome dismounting unwheeling may be implemented in fixed device 10 and ground is fixed.
Radome of fighter dismounting unwheeling of the invention is as follows in radome of fighter installation process:
After radome is removed from aircraft, this unwheeling is used as storage unwheeling, and radome is still fixed with radome slotting
Pin is fixed on radome bracket 3.In the work of installation radome, unwheeling is pushed into radome of fighter datum clamp face first
Near.The position of height is currently parked to suitable aircraft using the adjusting guide rail 2 of height adjustment screw rod 6.Slowly unwheeling is pushed to fly
Machine radome datum clamp face determines the opposite position of unwheeling Yu radome datum clamp face using the positioning supporting plate of 2 front end of guide rail
It sets, and fixes unwheeling with ground fixing device 10.The runner of rotary drive screw rod, by radome bracket 3 toward radome installation side
To movement, radome is installed in place.Radome Fixed latches are finally removed, installation unwheeling are removed, radome is installed.
Finally it should be noted that: the above embodiments are merely illustrative of the technical solutions of the present invention, but protection of the invention
Range is not limited thereto, and anyone skilled in the art in the technical scope disclosed by the present invention, can be thought easily
It is modified or replaceed to various equivalent, these, which are modified or replaceed, should all be included within the scope of the present invention.Example
Such as: because of the difference of different type of machines radome contour structures, the structure type of radome bracket can also be different, such as
In above-described embodiment, change radome bracket shape and structure, can the radome to different type of machines carry out dismounting work.
Claims (10)
1. a kind of radome of fighter dismounts unwheeling, it is characterised in that: the radome of fighter dismounting unwheeling includes transmission mechanism
(1), guide rail (2), radome bracket (3), fixed device (4), height adjustment mechanism, ground surface platform；The transmission mechanism (1) and
The radome bracket (3) is mounted on the guide rail (2), the transmission mechanism (1) drive the radome bracket (3) along
The guide rail (2) is mobile；With the fixed device (4) of fixed radar cover on the radome bracket (3)；The guide rail
(2) it is fixed by height adjustment mechanism and ground surface platform.
2. radome of fighter according to claim 1 dismounts unwheeling, it is characterised in that: the radome of fighter assembling and disassembling stand
Vehicle further includes the positioning supporting plate for being mounted on the guide rail (2) front end, and the positioning surface of the positioning supporting plate is the installation base of radome
Quasi- face.
3. radome of fighter according to claim 2 dismounts unwheeling, it is characterised in that: the positioning supporting plate passes through soft
Material cladding.
4. radome of fighter according to claim 1 dismounts unwheeling, it is characterised in that: the transmission mechanism (1) includes
Drive lead screw and the runner for being fixed on drive lead screw end；The drive lead screw is mounted on the guide rail (2), and with the thunder
It is fixed up to cover bracket (3).
5. radome of fighter according to claim 1 dismounts unwheeling, it is characterised in that: the height adjustment mechanism is by stretching
Contracting sleeve (5), height adjustment screw rod (6), pillar (7) composition, extension sleeve (5) lower end are fixed with the ground surface platform,
It is internal that the pillar (7) is mounted on the extension sleeve (5)；Height adjustment screw rod (6) lower end and the ground surface platform are solid
Fixed, upper end and pillar (7) are fixed.
6. radome of fighter according to claim 5 dismounts unwheeling, it is characterised in that: the extension sleeve (5) is certainly
Lubricate extension sleeve.
7. radome of fighter according to claim 1 dismounts unwheeling, it is characterised in that: the fixation device (4) is solid
Determine bolt, the Fixed latches are adapted to the dismounting hole on radome.
8. radome of fighter according to any one of claims 1 to 7 dismounts unwheeling, it is characterised in that: the ground is flat
Platform has upper table rank of standing in locomotive work.
9. radome of fighter according to any one of claims 1 to 7 dismounts unwheeling, it is characterised in that: the ground is flat
Platform is equipped with ground fixing device (10) and roller group is fixed.
10. radome of fighter according to claim 9 dismounts unwheeling, it is characterised in that: the roller group includes universal
It takes turns (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910437595.XA CN110203122A (en) | 2019-05-24 | 2019-05-24 | A kind of radome of fighter dismounting unwheeling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910437595.XA CN110203122A (en) | 2019-05-24 | 2019-05-24 | A kind of radome of fighter dismounting unwheeling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110203122A true CN110203122A (en) | 2019-09-06 |
Family
ID=67788547
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910437595.XA Pending CN110203122A (en) | 2019-05-24 | 2019-05-24 | A kind of radome of fighter dismounting unwheeling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110203122A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111843913A (en) * | 2020-08-26 | 2020-10-30 | 中国航空工业集团公司济南特种结构研究所 | A auxiliary device for antenna house dismouting |
| CN112441252A (en) * | 2020-10-14 | 2021-03-05 | 广州飞机维修工程有限公司 | Dismounting method of aircraft engine |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202367674U (en) * | 2011-11-11 | 2012-08-08 | 中国飞行试验研究院 | Vehicle for disassembling and assembling radar cover |
| CN207896521U (en) * | 2018-02-09 | 2018-09-21 | 泉州亿兴电力有限公司 | A kind of transport carriage |
| CN208393414U (en) * | 2018-04-13 | 2019-01-18 | 成都鑫盛生物科技有限公司 | A kind of surgical operation flask for medicinal preparations transfer carriage |
| CN208559466U (en) * | 2018-05-16 | 2019-03-01 | 苏州奥曼恩自动化科技有限公司 | A kind of positioning device of production line circulation |
-
2019
- 2019-05-24 CN CN201910437595.XA patent/CN110203122A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202367674U (en) * | 2011-11-11 | 2012-08-08 | 中国飞行试验研究院 | Vehicle for disassembling and assembling radar cover |
| CN207896521U (en) * | 2018-02-09 | 2018-09-21 | 泉州亿兴电力有限公司 | A kind of transport carriage |
| CN208393414U (en) * | 2018-04-13 | 2019-01-18 | 成都鑫盛生物科技有限公司 | A kind of surgical operation flask for medicinal preparations transfer carriage |
| CN208559466U (en) * | 2018-05-16 | 2019-03-01 | 苏州奥曼恩自动化科技有限公司 | A kind of positioning device of production line circulation |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111843913A (en) * | 2020-08-26 | 2020-10-30 | 中国航空工业集团公司济南特种结构研究所 | A auxiliary device for antenna house dismouting |
| CN112441252A (en) * | 2020-10-14 | 2021-03-05 | 广州飞机维修工程有限公司 | Dismounting method of aircraft engine |
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| 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 |
Application publication date: 20190906 |
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| RJ01 | Rejection of invention patent application after publication |