CN207046803U - A kind of airframe jack top pad - Google Patents
A kind of airframe jack top pad Download PDFInfo
- Publication number
- CN207046803U CN207046803U CN201720956697.9U CN201720956697U CN207046803U CN 207046803 U CN207046803 U CN 207046803U CN 201720956697 U CN201720956697 U CN 201720956697U CN 207046803 U CN207046803 U CN 207046803U
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- China
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- top pad
- airframe
- rubber ring
- annular groove
- pad body
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Abstract
The utility model discloses a kind of airframe jack top pad, belong to aircraft testing technical field.The top pad includes pushing up pad body (1) and rubber ring (2), wherein, the top pad body (1) includes bulb part and column part, the ball head is divided into the hemispherical configuration with curved surface and plane composition, the column part is arranged on the side with plane of the bulb part, and annular groove is provided with the column part, rubber ring (2) adaptation is arranged in the annular groove.The utility model is fixed by pushing up the rubber ring tensioner of pad body cylindrical end, can easily and efficiently realize that airframe jack top pad is connected with aircraft fuselage structure.In addition, top pad body bulb part can fully be engaged with jack top nest, increase forced contact area, reduce pressure.
Description
Technical field
The utility model belongs to aircraft testing technical field, and in particular to a kind of airframe jack top pad.
Background technology
(guarantee for jacking up aircraft is set aircraft fuselage structure with jack when airframe jack top pad is aircraft jacking
It is standby) bearing of excessively transferring, general airframe jack top pad is used cooperatively with jack, the support top at wing or fuselage
Aircraft.Fast and effectively realize that airframe jack top pad is connected with aircraft fuselage structure during use however, how can guarantee that
It is the difficulties of airframe jack top pad design.
In the prior art, jack top pad is typically fixed on by fuselage bottom using bolt, such a structure is needed in aircraft
Upper reserved fixed end structure, damages to fuselage appearance structure, aircraft aerodynamic effect can be influenceed when serious.
Utility model content
In order to solve the above problems, the utility model proposes a kind of airframe jack top pad, compared to routine
Be spirally connected fixation, and the utility model offer employs rubber ring tensioner and fixed so that connection is more efficiently, fast.
The utility model airframe jack top is padded, including top pad body and rubber ring, wherein, the top pad body bag
Bulb part and column part are included, the ball head is divided into the hemispherical configuration with curved surface and plane composition, the cylindrical portion
Divide the side with plane for being arranged on the bulb part, and annular groove is provided with the column part, the rubber ring is fitted
With in the annular groove.
Preferably, it is provided with lightening hole on the bulb part of the top pad body.
Preferably, the internal diameter of the rubber ring is less than the groover rot diameter of the annular groove, and the external diameter of the rubber ring is more than
The diameter of section of the column part.
Preferably, the rubber ring is O-ring.
Preferably, the annular groove is provided with multiple, and with some rubber rings for being adapted to the annular groove quantity.
Preferably, the diameter of section of the column part is less than the planar diameter of the bulb part.
The utility model is fixed by pushing up the rubber ring tensioner of pad body cylindrical end, can easily and efficiently realize aircraft machine
Body jack top pad is connected with aircraft fuselage structure.In addition, top pad body bulb part can fully contact with jack top nest and match somebody with somebody
Close, increase forced contact area, reduce pressure.Compared to the fixation that is spirally connected of routine, the utility model provides and employs rubber ring
Tensioner is fixed so that connection is more efficient, quick, therefore the very convenient use of the utility model, practical.
Brief description of the drawings
Fig. 1 is the top mat structure axonometric drawing according to a preferred embodiment of the utility model airframe jack top pad.
Fig. 2 is the use schematic diagram of the better embodiment of the utility model one.
Wherein, 1- pushes up pad body, 2- rubber rings, 3- aircraft skins, 4- aircraft fuselage structures.
Embodiment
To make the purpose, technical scheme and advantage that the utility model is implemented clearer, below in conjunction with the utility model
Accompanying drawing in embodiment, the technical scheme in the embodiment of the utility model is further described in more detail.In the accompanying drawings, from beginning
Same or similar element is represented to same or similar label eventually or there is the element of same or like function.Described reality
It is the utility model part of the embodiment to apply example, rather than whole embodiments.Below with reference to the embodiment of accompanying drawing description
It is exemplary, it is intended to for explaining the utility model, and it is not intended that to limitation of the present utility model.It is new based on this practicality
Embodiment in type, the every other implementation that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example, belong to the scope of the utility model protection.Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, it is for only for ease of description the utility model and simplifies description, rather than indicates or imply and be signified
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The limitation of novel protected scope.
The utility model proposes a kind of airframe jack top pad, as shown in figure 1, including top pad body 1 and rubber
Circle 2, wherein, the top pad body 1 includes bulb part and column part, and the ball head is divided into curved surface and plane composition
Hemispherical configuration, the column part is arranged on the side with plane of the bulb part, and on the column part
Annular groove is provided with, the adaptation of rubber ring 2 is arranged in the annular groove.
With reference to figure 1, the diameter of section of the column part is less than the planar diameter of the bulb part, also, cylindrical portion
The diameter of section divided is consistent with the preformed hole internal diameter of aircraft fuselage structure 4, with reference to figure 2, so as to which the column part is stretched
Enter into the preformed hole, in the present embodiment, the use-case of the top pad first fills in the top Upper cylindrical of pad body 1 with reference to figure 2
In the reserved mounting hole of aircraft fuselage structure 4, until the upper end of the top bottom bulb of pad body 1 fully contacts with aircraft skin 3.It
Afterwards, top pad body 1 is fixed in the preformed hole of aircraft fuselage structure 4 by the tensioner of rubber ring 2.
In the present embodiment, lightening hole is provided with the bulb part of the top pad body.It is understood that lightening hole can
To be a blind hole or through hole as described in Figure 1 or multiple, it is necessary to which explanation, the top pad body 1 is metal material
Matter, there is good hardness and wearability, when setting lightening hole, it is impossible to destroy the structural strength of top pad body.
In the present embodiment, the internal diameter of the rubber ring is less than the groover rot diameter of the annular groove, and the external diameter of the rubber ring is big
In the diameter of section of the column part.By this tight fit, top pad body 1 can be made to be fixed on by the tensioner of rubber ring 2
In the preformed hole of aircraft fuselage structure 4.
In the present embodiment, the rubber ring is O-ring, and is standard component.
In the present embodiment, the annular groove can have it is multiple, along it is described top pad body column part axial direction arrange,
And with some rubber rings for being adapted to the annular groove quantity.
The utility model is fixed by pushing up the rubber ring tensioner of pad body cylindrical end, can easily and efficiently realize aircraft machine
Body jack top pad is connected with aircraft fuselage structure.In addition, top pad body bulb part can fully contact with jack top nest and match somebody with somebody
Close, increase forced contact area, reduce pressure.Compared to the fixation that is spirally connected of routine, the utility model provides and employs rubber ring
Tensioner is fixed so that connection is more efficient, quick, therefore the very convenient use of the utility model, practical.
It is last it is to be noted that：Above example is only to illustrate the technical solution of the utility model, rather than it is limited
System.Although the utility model is described in detail with reference to the foregoing embodiments, one of ordinary skill in the art should manage
Solution：It can still be modified to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered
Row equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from various embodiments of the utility model
The spirit and scope of technical scheme.
Claims (6)
- A kind of 1. airframe jack top pad, it is characterised in that including top pad body (1) and rubber ring (2), wherein, it is described Top pad body (1) includes bulb part and column part, and the ball head is divided into the hemispherical knot with curved surface and plane composition Structure, the column part are arranged on the side with plane of the bulb part, and are provided with annular groove on the column part, Rubber ring (2) adaptation is arranged in the annular groove.
- 2. airframe jack top pad as claimed in claim 1, it is characterised in that the ball head of the top pad body (1) Lightening hole is provided with point.
- 3. airframe jack top pad as claimed in claim 1, it is characterised in that the internal diameter of the rubber ring (2) is less than The groover rot diameter of the annular groove, the external diameter of the rubber ring (2) are more than the diameter of section of the column part.
- 4. airframe jack top pad as claimed in claim 1, it is characterised in that the rubber ring is O-ring.
- 5. airframe jack top as claimed in claim 1 pad, it is characterised in that the annular groove is provided with multiple, and has There are some rubber rings for being adapted to the annular groove quantity.
- 6. airframe jack top pad as claimed in claim 1, it is characterised in that the diameter of section of the column part is small Planar diameter in the bulb part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720956697.9U CN207046803U (en) | 2017-08-02 | 2017-08-02 | A kind of airframe jack top pad |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720956697.9U CN207046803U (en) | 2017-08-02 | 2017-08-02 | A kind of airframe jack top pad |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207046803U true CN207046803U (en) | 2018-02-27 |
Family
ID=61499057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720956697.9U Active CN207046803U (en) | 2017-08-02 | 2017-08-02 | A kind of airframe jack top pad |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207046803U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109305382A (en) * | 2018-10-17 | 2019-02-05 | 江西洪都航空工业集团有限责任公司 | Tie-down point and jacking bracket structure on a kind of aircraft |
-
2017
- 2017-08-02 CN CN201720956697.9U patent/CN207046803U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109305382A (en) * | 2018-10-17 | 2019-02-05 | 江西洪都航空工业集团有限责任公司 | Tie-down point and jacking bracket structure on a kind of aircraft |
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