CN206366189U - A kind of Fixed Wing AirVehicle is to flap arrangement - Google Patents
A kind of Fixed Wing AirVehicle is to flap arrangement Download PDFInfo
- Publication number
- CN206366189U CN206366189U CN201621444270.2U CN201621444270U CN206366189U CN 206366189 U CN206366189 U CN 206366189U CN 201621444270 U CN201621444270 U CN 201621444270U CN 206366189 U CN206366189 U CN 206366189U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- wing
- spar
- easy
- connector
- 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 is related to a kind of Fixed Wing AirVehicle to flap arrangement, the port wing and starboard wing of fuselage both sides are connected to including fuselage and symmetrical upset, port wing and starboard wing include wing body, the locating piece being be arranged in parallel with wing body plane for being connected to wing body root, through wing body inside and beyond the spar of wing body root, fuselage includes upper fuselage and lower fuselage, and the trailing edge of upper fuselage and lower fuselage is joined together to form by revolving part is easy to folding<The spar connector for being easy to spar to block and be mutually locked together and the locating slot for being easy to locating piece to block are equipped with type, upper fuselage and lower fuselage, spar connector and fuselage surface offer the groove for being easy to spar to block.The beneficial effects of the utility model are：The spar connector of clamping can realize the continuity of complete machine spar, it is ensured that structural strength.This doubling-up device is simple in construction, action is quick, and the transport that can effectively reduce complete machine carries volume, and is easy to the cable between fuselage and wing body to arrange.
Description
Technical field
The utility model is related to a kind of Fixed Wing AirVehicle to flap arrangement.
Background technology
In existing fixed-wing model plane, transport for convenience is carried, use fuselage and wing detachable connection, dismounting more
Process is cumbersome.Wing body is generally disposed with the electronic equipments such as steering wheel, wireless receiving and dispatching, and being dismounted for multiple times is easily caused across wing body and fuselage top-stitching
The loose contact of road socket, influence flight safety and complete machine service life.
Utility model content
The technical problems to be solved in the utility model is：Based on above mentioned problem there is provided a kind of Fixed Wing AirVehicle to flap
Device.
The utility model solves the technical scheme that its technical problem used：A kind of Fixed Wing AirVehicle is filled to flap
Put, including fuselage and symmetrical upset are connected to the port wing and starboard wing of fuselage both sides, port wing and starboard wing include wing body,
Be connected to wing body root with wing body plane be arranged in parallel locating piece, through inside wing body and beyond the spar of wing body root,
Fuselage includes upper fuselage and lower fuselage, and the trailing edge of upper fuselage and lower fuselage is joined together to form by revolving part is easy to folding
<The spar connector for being easy to spar to block and be mutually locked together is equipped with type, upper fuselage and lower fuselage and is easy to determine
The locating slot that position block is blocked, spar connector and fuselage surface offer the groove for being easy to spar to block.
Further, port wing and starboard wing overturn the both sides for being connected to upper fuselage/lower fuselage, hinge one side by hinge
Wing body root bottom surface is fixed on, another side is fixed on fuselage/lower fuselage surface.
Further, locating slot is close to fuselage trailing edge, and spar connector is located at the outside of locating slot.
Further, connected between the spar connector on upper fuselage and lower fuselage by locking member, locking member is in I-shaped
The through hole through upper fuselage and lower fuselage is offered on matrix shape solid construction, spar connector, locking member is through through hole and revolves
Turn to lock between spar connector.
The beneficial effects of the utility model are：The spar connector of clamping can realize the continuity of complete machine spar, it is ensured that knot
Structure intensity.This doubling-up device is simple in construction, action quick, and the transport that can effectively reduce complete machine carries volume, and be easy to fuselage with
Cable arrangement between wing body.
Brief description of the drawings
The utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of port wing/starboard wing；
Fig. 3 is the assembling schematic diagram of upper fuselage/lower fuselage；
Fig. 4 is the assembling schematic diagram of spar and spar connector；
Wherein：1. port wing, 2. starboard wings, 3. wing bodies, 4. hinges, 5. spars, 6. locating pieces, fuselage, 8. times machines on 7.
Body, 9. spar connectors, 10. locating slots, 11. locking members.
Embodiment
The utility model is further described presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram only to show
Meaning mode illustrates basic structure of the present utility model, therefore it only shows the composition relevant with the utility model.
A kind of Fixed Wing AirVehicle as Figure 1-4 is connected to fuselage to flap arrangement, including fuselage and symmetrical upset
The port wing 1 and starboard wing 2 of both sides, port wing 1 and starboard wing 2 include wing body 3, are connected to the flat with wing body 3 of the root of wing body 3
Locating piece 6 that face be arranged in parallel, through the inside of wing body 3 and beyond the spar 5 of the root of wing body 3, fuselage include upper fuselage 7 and under
The trailing edge of fuselage 8, upper fuselage 7 and lower fuselage 8 is joined together to form by revolving part is easy to folding<Type, upper fuselage 7 is with
The spar connector 9 for being easy to spar 5 to block and be mutually locked together is equipped with fuselage 8 and is easy to what locating piece 6 was blocked
Locating slot 10, spar connector 9 and fuselage surface offer the groove for being easy to spar 5 to block.
Port wing 1 and starboard wing 2 overturn the both sides for being connected to upper 7/ time fuselage of fuselage 8 by hinge 4, and hinge 4 is simultaneously solid
Due to the root bottom surface of wing body 3, another side is fixed on the surface of 7/ time fuselage of fuselage 8.
Locating slot 10 is located at the outside of locating slot 10 close to fuselage trailing edge, spar connector 9.It is arranged so as to so that spar connects
Connect device locking more firm.
Connected between spar connector 9 on upper fuselage 7 and lower fuselage 8 by locking member 11, locking member 11 is in I-shaped
The through hole through upper fuselage 7 and lower fuselage 8 is offered on laminated structure, spar connector 9, locking member 11 is through through hole and rotates
It will be locked between spar connector 9.
During action, first wing is flattened, fuselage is closed afterwards, now locating piece falls into locating slot and compressed by fuselage, spar quilt
Spar connector fastening connection, locking member passes through the through hole of spar connector, and rotates and will be locked between spar connector, complete machine
Expansion action is completed.Left and right spar is fallen into the groove of spar connector, left and right spar connector connection left and right spar, spar cap
Whole groove is filled up in portion, it is ensured that the continuity of structure；Locating piece falls into the locating slot of fuselage, can further limit machine
The wing prevents wing from loosening with respect to the position of fuselage.
During transport, wing is folded upward to above body, fuselage is closed, spar connector is fastened, in transport case,
It is readily transported.
The spar connector of clamping can realize the continuity of complete machine spar, it is ensured that structural strength.The letter of this doubling-up device structure
Single, action is quick, and the transport that can effectively reduce complete machine carries volume, and convenient wiring.
Spar connector is embedded at fuselage interior surface, or is integrally formed with fuselage.Spar is in cylinder or square column type, phase
The groove answered is in semi-cylindrical or half square column type.The revolving part of upper fuselage and lower fuselage trailing edge is hinge.
Using it is above-mentioned according to desirable embodiment of the present utility model as enlightenment, pass through above-mentioned description, related work people
Member can carry out various changes and amendments in the range of without departing from this utility model technological thought completely.This reality
The content on specification is not limited to new technical scope, it is necessary to its technology is determined according to right
Property scope.
Claims (4)
1. a kind of Fixed Wing AirVehicle is to flap arrangement, it is characterized in that：Fuselage both sides are connected to including fuselage and symmetrical upset
Port wing (1) and starboard wing (2), port wing (1) and starboard wing (2) include wing body (3), be connected to wing body (3) root with
Locating piece (6) that wing body (3) plane be arranged in parallel, through wing body (3) is internal and spar (5) beyond wing body (3) root, machine
Body includes upper fuselage (7) and lower fuselage (8), and the trailing edge of upper fuselage (7) and lower fuselage (8) is joined together to form by revolving part
It is easy to folding<The wing for being easy to spar (5) to block and be mutually locked together is equipped with type, upper fuselage (7) and lower fuselage (8)
Beam connector (9) and the locating slot (10) for being easy to locating piece (6) to block, spar connector (9) and fuselage surface are offered just
The groove blocked in spar (5).
2. a kind of Fixed Wing AirVehicle according to claim 1 is to flap arrangement, it is characterized in that：Described port wing (1)
The both sides for being connected to upper fuselage (7)/lower fuselage (8) are overturn by hinge (4) with starboard wing (2), hinge (4) is simultaneously fixed on the wing
Body (3) root bottom surface, another side is fixed on fuselage (7)/lower fuselage (8) surface.
3. a kind of Fixed Wing AirVehicle according to claim 1 is to flap arrangement, it is characterized in that：Described locating slot (10)
Close to fuselage trailing edge, spar connector (9) is located at the outside of locating slot (10).
4. a kind of Fixed Wing AirVehicle according to claim 1 is to flap arrangement, it is characterized in that：Described upper fuselage (7)
Connected between the spar connector (9) on lower fuselage (8) by locking member (11), locking member (11) is solid in I-shaped sheet
The through hole through upper fuselage (7) and lower fuselage (8) is offered on structure, spar connector (9), locking member (11) passes through through hole simultaneously
Rotation will be locked between spar connector (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621444270.2U CN206366189U (en) | 2016-12-27 | 2016-12-27 | A kind of Fixed Wing AirVehicle is to flap arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621444270.2U CN206366189U (en) | 2016-12-27 | 2016-12-27 | A kind of Fixed Wing AirVehicle is to flap arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206366189U true CN206366189U (en) | 2017-08-01 |
Family
ID=59393139
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621444270.2U Expired - Fee Related CN206366189U (en) | 2016-12-27 | 2016-12-27 | A kind of Fixed Wing AirVehicle is to flap arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206366189U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106669180A (en) * | 2016-12-27 | 2017-05-17 | 常州大学 | Fixed wing aircraft folded wing device |
-
2016
- 2016-12-27 CN CN201621444270.2U patent/CN206366189U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106669180A (en) * | 2016-12-27 | 2017-05-17 | 常州大学 | Fixed wing aircraft folded wing device |
| CN106669180B (en) * | 2016-12-27 | 2019-12-06 | 常州大学 | Flap aligning device of fixed-wing aircraft |
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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 |
Granted publication date: 20170801 Termination date: 20181227 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |