CN205633077U - Wing anti -icing system flute venturi tube strutting arrangement - Google Patents
Wing anti -icing system flute venturi tube strutting arrangement Download PDFInfo
- Publication number
- CN205633077U CN205633077U CN201620452386.4U CN201620452386U CN205633077U CN 205633077 U CN205633077 U CN 205633077U CN 201620452386 U CN201620452386 U CN 201620452386U CN 205633077 U CN205633077 U CN 205633077U
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- venturi tube
- wing anti
- bourdon
- utility
- tube
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Abstract
The utility model relates to a wing anti -icing system designs field, in particular to wing anti -icing system flute venturi tube strutting arrangement to at least, solve the problem that present flute venturi tube installation device structure is complicated, the installation is inconvenient. Wing anti -icing system flute venturi tube strutting arrangement for in the mounting hole of flute venturi tube fixed stay on the floor, include: the annular supporting board sets up in the mounting hole, just the coaxial setting of flute venturi tube is in in the hole of annular supporting board, cyclic annular bond line, be used for with the outer anchor ring of annular supporting board bonds in the mounting hole. The utility model discloses a wing anti -icing system flute venturi tube strutting arrangement, it is fixed to bond through cyclic annular bond line between annular supporting board and the floor, and installation procedure simplifies, and the installation effectiveness improves, and weight is little.
Description
Technical field
This utility model relates to wing anti-ice system design field, particularly to a kind of wing anti-ice
System bourdon's tube support means.
Background technology
In wing anti-ice system, bourdon's tube along wing exhibition to through multiple floors is in slat
Anti-icing chamber provides anti-icing bleed, owing to bourdon's tube is big along spanwise span, causes footpath after stress
Big to displacement；Therefore, in current wing anti-ice system, especially as it is shown in figure 1, be needs
The gripper shoe 5 of bourdon's tube 2 is affixed on each floor 1, bourdon's tube 2 is played and props up
Support and the effect of Reducing distortion.But this fixing means needs respectively at gripper shoe 5 and floor 1
Surrounding prepares bolt hole, and uses many group bolts 6 as connector.This fixing means operation is multiple
Miscellaneous, bolt time space to be installed narrow and small, use standard component quantity many simultaneously, weight is big.
Summary of the invention
The purpose of this utility model there is provided a kind of wing anti-ice system bourdon's tube support means,
At least to solve the problem that current bourdon's tube erecting device structure is complicated, install inconvenience.
The technical solution of the utility model is:
A kind of wing anti-ice system bourdon's tube support means, for being fixedly supported on rib by bourdon's tube
In installing hole on plate, including:
Annular support plate, is arranged in described installing hole, and described bourdon's tube is co-axially located at institute
State in the endoporus of annular support plate；
Cyclic adhesion layer, for being bonded in described installing hole by the outer ring surface of described annular support plate
In.
Preferably, described cyclic adhesion layer is fluorosioloxane rubber adhesive layer.
Preferably, described annular support plate is politef gripper shoe.
The utility model has the advantage of:
Wing anti-ice system bourdon's tube support means of the present utility model, annular support plate and floor
Between be adhesively fixed by cyclic adhesion layer, installation procedure simplify, installation effectiveness improve, and weight
Measure little.
Accompanying drawing explanation
Fig. 1 is the mounting structure schematic diagram of existing wing anti-ice system bourdon's tube；
Fig. 2 is that bourdon's tube uses this utility model wing anti-ice system bourdon's tube support means to pacify
Structural representation after dress.
Detailed description of the invention
Clearer for the purpose making this utility model implement, technical scheme and advantage, below will
In conjunction with the accompanying drawing in this utility model embodiment, to the technical scheme in this utility model embodiment
It is further described in more detail.In the accompanying drawings, the most same or similar label represents phase
With or similar element or there is the element of same or like function.Described embodiment is this
The a part of embodiment of utility model rather than whole embodiments.Retouch below with reference to accompanying drawing
The embodiment stated is exemplary, it is intended to be used for explaining this utility model, and it is not intended that right
Restriction of the present utility model.Based on the embodiment in this utility model, ordinary skill people
The every other embodiment that member is obtained under not making creative work premise, broadly falls into this
The scope of utility model protection.Below in conjunction with the accompanying drawings embodiment of the present utility model is carried out in detail
Explanation.
In description of the present utility model, it is to be understood that term " " center ", " longitudinally ",
" laterally ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ",
Orientation or the position relationship of the instruction such as " interior ", " outward " are based on orientation shown in the drawings or position
Relation, is for only for ease of description this utility model and simplifies description rather than instruction or hint
The device of indication or element must have specific orientation, with specific azimuth configuration and operation,
Therefore it is not intended that restriction to this utility model protection domain.
1 and Fig. 2 this utility model wing anti-ice system bourdon's tube is supported dress below in conjunction with the accompanying drawings
Put and be described in further details.
This utility model provides a kind of wing anti-ice system bourdon's tube support means, for by flute
Shape pipe 2 is fixedly supported in the installing hole on floor 1, including annular support plate 3, ring-type viscous
Close layer 4.
Annular support plate 3 (being cylindrical shape) is arranged in installing hole, and bourdon's tube 2 is coaxial
It is arranged in the endoporus of annular support plate 3, thus bourdon's tube 2 is fixed.
Cyclic adhesion layer 4 (being cylindrical shape) is for by bonding for the outer ring surface of annular support plate 3
In installing hole (on the inner ring surface of installing hole).
Wing anti-ice system bourdon's tube support means of the present utility model, annular support plate 3 and rib
Using cyclic adhesion layer 4 to be adhesively fixed between plate 1, this fixed structure need not at circumferential support
Plate 3 and floor 1 surrounding prepare bolt hole, it is not necessary to use bolt, and installation procedure simplifies, peace
Dress efficiency improves, and weight is little, reduces manufacturing cost and use cost.
In wing anti-ice system bourdon's tube support means of the present utility model, cyclic adhesion layer 4 can
To use the multiple applicable material with binding function to make, in the present embodiment, the most ring-type
Adhesive layer 4 is fluorosioloxane rubber adhesive layer, heat-resisting ability is higher and adhesive effect more preferably.Equally,
Annular support plate 3 can also use multiple applicable material to make, the most ring-type of the present embodiment
Fagging 3 is politef gripper shoe, has certain deflection, and after ensure that installation
Structural strength, weight can be made again lighter.
During wing anti-ice system bourdon's tube support means installation process of the present utility model, by poly-four
Fluorothene annular support plate 3 is arranged in the installing hole of floor 1, then the slat structure at them
Use resistant to elevated temperatures fluorosioloxane rubber glue to fill, wait that fluorosioloxane rubber glue is fully cured rear (shape
Adhesive layer 4 circlewise)；The most again bourdon's tube 2 is carried out through the endoporus of annular support plate 3
Fixed installation, aircraft bourdon's tube 2 in flight course produces radial displacement with slat malformation
Time, bourdon's tube 2 can be played support and the effect of Reducing distortion by annular support plate 3.
The above, detailed description of the invention the most of the present utility model, but guarantor of the present utility model
The scope of protecting is not limited thereto, and any those familiar with the art is at this utility model
In the technical scope disclosed, the change that can readily occur in or replacement, all should contain in this practicality new
Within the protection domain of type.Therefore, protection domain of the present utility model should be with described claim
Protection domain be as the criterion.
Claims (3)
1. a wing anti-ice system bourdon's tube support means, for fixing bourdon's tube (2)
It is supported in the installing hole on floor (1), it is characterised in that including:
Annular support plate (3), is arranged in described installing hole, and described bourdon's tube (2) is same
Axle is arranged in the endoporus of described annular support plate (3)；
Cyclic adhesion layer (4), for being bonded in the outer ring surface of described annular support plate (3)
In described installing hole.
Wing anti-ice system bourdon's tube support means the most according to claim 1, it is special
Levying and be, described cyclic adhesion layer (4) is fluorosioloxane rubber adhesive layer.
Wing anti-ice system bourdon's tube support means the most according to claim 1, it is special
Levying and be, described annular support plate (3) is politef gripper shoe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620452386.4U CN205633077U (en) | 2016-05-18 | 2016-05-18 | Wing anti -icing system flute venturi tube strutting arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620452386.4U CN205633077U (en) | 2016-05-18 | 2016-05-18 | Wing anti -icing system flute venturi tube strutting arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633077U true CN205633077U (en) | 2016-10-12 |
Family
ID=57056553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620452386.4U Active CN205633077U (en) | 2016-05-18 | 2016-05-18 | Wing anti -icing system flute venturi tube strutting arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205633077U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850159A (en) * | 2019-02-18 | 2019-06-07 | 广西大学 | One kind is based on the recoverable unmanned plane during flying winterization system of heat |
-
2016
- 2016-05-18 CN CN201620452386.4U patent/CN205633077U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850159A (en) * | 2019-02-18 | 2019-06-07 | 广西大学 | One kind is based on the recoverable unmanned plane during flying winterization system of heat |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |