CN207791134U - A kind of radome fairing for placing lock - Google Patents
A kind of radome fairing for placing lock Download PDFInfo
- Publication number
- CN207791134U CN207791134U CN201721629844.8U CN201721629844U CN207791134U CN 207791134 U CN207791134 U CN 207791134U CN 201721629844 U CN201721629844 U CN 201721629844U CN 207791134 U CN207791134 U CN 207791134U
- Authority
- CN
- China
- Prior art keywords
- lock
- radome fairing
- cloth prepreg
- glass cloth
- mounting groove
- 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.)
- Active
Links
Landscapes
- Details Of Aerials (AREA)
Abstract
The utility model provides a kind of radome fairing for placing lock, is related to helicopter structure design field.Including rectification cover body, and the lock mounting groove being arranged on rectification cover body, the rectification cover body includes glass cloth prepreg, and the paper honeycomb coated by the glass cloth prepreg, the lock mounting groove includes glass cloth prepreg and the carbon cloth prepreg that is coated by the glass cloth prepreg, it is provided with through-hole on the lock mounting groove, for installing hook lock.The utility model is simple in structure, without reinforcing body rigid structure, remains use and the installation function of former radome fairing, and weight is light, entire bottom rectifying cover is that glass cloth adds paper honeycomb structure, weight relatively light.Corresponding lock mounting surface, carbon cloth reinforce the weight very little generated, and secondly, lock is rest directly upon on radome fairing, and cooperation hook lock being capable of quick-release installation.
Description
Technical field
The utility model is related to helicopter structure design fields, and in particular to a kind of radome fairing for placing lock.
Background technology
The radome fairing of aircraft is for adjusting air-flow, and in order to reduce in the skyborne resistance of aircraft, radome fairing is as possible with streamline
Type designs, and enables air-flow is smooth to pass through.
When Helicopter Dome is opened, system maintenance channel can be used as；When closing, built-in system and equipment are protected, and subtract
Aerodynamic drag in few flight course, radome fairing generally use hinge or locking mechanism are connect with housing construction, therefore radome fairing
It is movable part.The locking mechanism of existing helicopter fuselage bottom rectifying cover uses hanging-ring type locking mechanism, lock point installation
Tapered platform, heavier-weight are enriched in face using filler, and its lock point opening need to break rectification shroud rim, affect radome fairing
Edge integrity, rigidity and mechanical property are poor.In contrast, the lock point mounting surface lighter in weight of existing design, rigidity is preferable,
Remain the integrality of rectification shroud rim, specious smoothness.
Utility model content
The utility model designs a kind of radome fairing for placing lock, under the premise of meeting radome fairing basic function, increases by 6
Place the mounting surface of hook lock in place.It is designed by profile optimization, according to a lock point position at 6, in the bottom rectifying cover of smooth surface
Invagination installation lock platform at upper design 6, the platform are that curved surface smoothly transits to invagination plane, are used in combination the double-deck carbon cloth to around it
Reinforced.
The utility model places the radome fairing of lock, including rectification cover body, and the lock being arranged on rectification cover body
Seat mounting groove, the rectification cover body includes glass cloth prepreg, and the paper honeycomb coated by the glass cloth prepreg, institute
It includes glass cloth prepreg and the carbon cloth prepreg that is coated by the glass cloth prepreg to state lock mounting groove, the lock peace
Through-hole is provided on tankage, for installing hook lock.
Preferably, at least two layers of the carbon cloth prepreg.
In said program preferably, the carbon cloth prepreg is layer 2-4.
In said program preferably, the thickness of the lock mounting groove is generally the thickness of radome fairing having at cell
The 1/6-1/5 of degree.
In said program preferably, the glass cloth prepreg is at least 8 layers.
In said program preferably, the lock mounting groove on the radome fairing for placing lock is towards internal body
Groove depth is more than it in the groove depth towards engine body exterior.
Key point of the present invention：Installation requirement is locked according to hook, invagination lock platform at 6 is designed on the radome fairing of curved surface,
And lock point cooperation position is locked according to hook, trepanning is carried out in mounting platform, realizes that hook locks locking functions.
Lock mounting surface is plane：Due to locking locking mechanism using hook-type, work(is installed and used for guarantee hook-type lock button
Can, it is more difficult that lock mounting surface is directly designed on the curved surface of bottom rectifying cover.Therefore, surface blending is used on radome fairing
Lock mounting surface is designed as plane by the design method for plane of invaginating, and the lock of connection hook-type lock then directly falls within lock installation
On face.
The advantages of the utility model is：
1) installation of the hook-type lock lock in the curved surface radome fairing of greater curvature is realized；
2) plane of mounting platform be by original by curved surface influenced everywhere in a lock point lock be designed as that same part is suitble to lock
Seat provides precondition；
3) the rectification cover outer surface (surface blending to the platform that invaginates) in lock point region is smooth complete, beautiful smooth.
The rigidity of lock mounting surface is reinforced.
The radome fairing that lock can be placed has following advantages：
1. simple in structure：Structure remains using and installing for former radome fairing without reinforcing body rigid structure
Function；
2. weight is light：Entire bottom rectifying cover is glass cloth+paper honeycomb structure, and weight is relatively light.Corresponding lock peace
Dress face, carbon cloth reinforce the weight very little generated；
3. easy for installation：Lock is rest directly upon on radome fairing, cooperation hook lock quick-release installation.
In contrast, the lock point mounting surface lighter in weight of existing design, rigidity is preferable, remains the complete of rectification shroud rim
Property, specious smoothness
Description of the drawings
Fig. 1 is the structural schematic diagram of a preferred embodiment of the radome fairing that the utility model places lock.
Fig. 2 is the radome fairing body construction schematic diagram of embodiment illustrated in fig. 1.
Fig. 3 is the lock mounting groove and radome fairing other structures position relationship schematic diagram of embodiment illustrated in fig. 1.
Wherein, 1 is rectification cover body, and 2 be lock mounting groove, and 3 be glass cloth prepreg, and 4 be paper honeycomb, and 5 is pre- for carbon cloth
Leaching material.
Specific implementation mode
To keep the purpose, technical scheme and advantage that the utility model is implemented clearer, below in conjunction with the utility model
Attached drawing in embodiment, is further described in more detail the technical scheme in the embodiment of the utility model.In the accompanying drawings, from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Described reality
It is the utility model a part of the embodiment to apply example, instead of all the embodiments.Below with reference to the embodiment of attached drawing description
It is exemplary, it is intended to for explaining the utility model, and should not be understood as limiting the present invention.It is new based on this practicality
Embodiment in type, the every other implementation that those of ordinary skill in the art are obtained without creative efforts
Example, shall fall within the protection scope of the present invention.The embodiments of the present invention are described in detail below in conjunction with the accompanying drawings.
In the description of the present invention, it should be understood that term "center", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown, is merely for convenience of describing the present invention and simplifying the description, rather than indicates or imply and is signified
Device or element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as to this practicality
The limitation of novel protected range.
The utility model places the radome fairing of lock, as shown in Figure 1, including rectification cover body 1, and is arranged in radome fairing
Lock mounting groove 2 on ontology, lock mounting groove 2 are invagination mounting surface, according to lock point position, simulation hook lock locking mechanism fortune
Dynamic path, designs lock platform on radome fairing appearance curved surface, lock platform relative surface invagination, i.e., from curved surface smoothly transit to
Invagination plane.Invagination region is square planar, and platform middle opening, aperture area is hook lock handle region, and flush.It is interior
It is corresponding lock mounting plane to fall into square planar.According to lock installation point, each mounting surface that invaginates installs lock, amounts in 6
Fall into mounting surface.6 rectangular platforms of invagination are all laminate structure.
With reference to figure 2, the rectification cover body includes glass cloth prepreg 3, and coated by the glass cloth prepreg 3
Paper honeycomb 4, with reference to figure 3, the lock mounting groove 2 includes glass cloth prepreg 3 and is coated by the glass cloth prepreg 3
Carbon cloth prepreg 5 is provided with through-hole 6 on the lock mounting groove 2, for installing hook lock.
In the present embodiment, at least two layers of the carbon cloth prepreg, such as layer 2-4, the glass cloth prepreg are at least 8
Layer.The utility model radome fairing is that composite material realizes its basic function using glass cloth+honeycomb.It is main to use 8 layers
(localised reinforced areas increases by 2 layers of carbon cloth prepreg by glass cloth prepreg 3233/EW110C and single layer paper honeycomb NH-1-2.75-32
Laying, vacuum pressed heating, curing molding 3234/CF3052) are carried out on mold.
In lock mounting surface and its peripheral region, in basic laying (3233/EW110C+1 layers of paper of 8 layers of glass cloth prepreg
Honeycomb NH-1-2.75-32) on the basis of, increase by 2 layers of carbon cloth prepreg 3234/CF3052, to enhance the rigidity in the region and strong
Degree, ensures the placement of lock and the locking of locking mechanism.
In the present embodiment, the thickness of the lock mounting groove is generally the 1/6- with the thickness at cell of radome fairing
1/5。
In the present embodiment, with reference to figure 3, the lock mounting groove on the radome fairing for placing lock is towards internal body
Groove depth is more than it in the groove depth towards engine body exterior.
The radome fairing that lock can be placed has following advantages：
1. simple in structure：Structure remains using and installing for former radome fairing without reinforcing body rigid structure
Function；
2. weight is light：Entire bottom rectifying cover is glass cloth+paper honeycomb structure, and weight is relatively light.Corresponding lock peace
Dress face, carbon cloth reinforce the weight very little generated；
3. easy for installation：Lock is rest directly upon on radome fairing, cooperation hook lock quick-release installation.
Compared with prior art, the lock point mounting surface lighter in weight of existing design, rigidity is preferable, remains rectification shroud rim
Integrality, specious smoothness.
It is last it is to be noted that：Above example is only to illustrate the technical solution of the utility model, rather than limits it
System.Although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art should manage
Solution：Its still can with technical scheme described in the above embodiments is modified, or to which part technical characteristic into
Row equivalent replacement；And these modifications or replacements, various embodiments of the utility model that it does not separate the essence of the corresponding technical solution
The spirit and scope of technical solution.
Claims (6)
1. a kind of radome fairing for placing lock, which is characterized in that including rectification cover body, and be arranged on rectification cover body
Lock mounting groove, the rectification cover body includes glass cloth prepreg, and the paper honeycomb coated by the glass cloth prepreg,
The lock mounting groove includes glass cloth prepreg and the carbon cloth prepreg that is coated by the glass cloth prepreg, the lock
Through-hole is provided on mounting groove, for installing hook lock.
2. placing the radome fairing of lock as described in claim 1, which is characterized in that at least two layers of the carbon cloth prepreg.
3. placing the radome fairing of lock as described in claim 1, which is characterized in that the carbon cloth prepreg is layer 2-4.
4. placing the radome fairing of lock as described in claim 1, which is characterized in that the thickness of the lock mounting groove is rectification
The 1/6-1/5 with the thickness at cell of cover.
5. placing the radome fairing of lock as described in claim 1, which is characterized in that the glass cloth prepreg is at least 8 layers.
6. placing the radome fairing of lock as described in claim 1, which is characterized in that the lock on the radome fairing for placing lock
Seat mounting groove is more than it in the groove depth towards engine body exterior in the groove depth towards internal body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721629844.8U CN207791134U (en) | 2017-11-29 | 2017-11-29 | A kind of radome fairing for placing lock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721629844.8U CN207791134U (en) | 2017-11-29 | 2017-11-29 | A kind of radome fairing for placing lock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791134U true CN207791134U (en) | 2018-08-31 |
Family
ID=63285007
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721629844.8U Active CN207791134U (en) | 2017-11-29 | 2017-11-29 | A kind of radome fairing for placing lock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207791134U (en) |
-
2017
- 2017-11-29 CN CN201721629844.8U patent/CN207791134U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9902483B2 (en) | Window panel for an airframe and method of producing same | |
| Ghori et al. | The role of advanced polymer materials in aerospace | |
| US7968170B2 (en) | Composite single pane window for an aircraft and method of making same | |
| US20130232883A1 (en) | Composite access door | |
| EP3635815A1 (en) | Accessible radome assembly | |
| US20080283664A1 (en) | Aircraft Fuselage Structure | |
| US9682765B2 (en) | Aircraft door and aircraft comprising such an aircraft door | |
| US10745105B2 (en) | Thermoplastic moulded injected tip structure for an aircraft | |
| US9034453B2 (en) | Reinforced aircraft fuselage panel and method of manufacture | |
| US20140242896A1 (en) | Ventilation conduit for an aircraft | |
| US20090294579A1 (en) | Primary engine strut structure of an aircraft | |
| US11613376B2 (en) | Aircraft wing box | |
| JP2016147613A (en) | Reinforcement structure of aircraft | |
| US9102393B2 (en) | Seal assembly for an aircraft wing | |
| US20150004348A1 (en) | Panel member for an airframe | |
| CN207791134U (en) | A kind of radome fairing for placing lock | |
| CN106507751B (en) | SUAV fuselage | |
| EP3424813B1 (en) | Skin-panel interface of an aircraft | |
| CN108481762A (en) | A kind of rocket composite core grade cover board and preparation method thereof | |
| EP3095590B1 (en) | A carbon fiber reinforced polymer panel arrangement and method | |
| US20220118727A1 (en) | Composite stiffener | |
| US20200023933A1 (en) | Pressure bulkhead and method of installation | |
| CN213139123U (en) | Landing gear cabin door | |
| CA2423665A1 (en) | Composite skin panel opening edge and method for manufacture | |
| EP1958874A2 (en) | Lightweight composite material and metal thrust recovery flapper valve |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |