CN208165245U - A kind of aircraft tail of the aerospace with function easy to disassemble - Google Patents
A kind of aircraft tail of the aerospace with function easy to disassemble Download PDFInfo
- Publication number
- CN208165245U CN208165245U CN201820391229.6U CN201820391229U CN208165245U CN 208165245 U CN208165245 U CN 208165245U CN 201820391229 U CN201820391229 U CN 201820391229U CN 208165245 U CN208165245 U CN 208165245U
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- disassemble
- cavity
- threaded
- fixedly connected
- block
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Abstract
The utility model provides a kind of aircraft tail of the aerospace with function easy to disassemble, is related to aircraft tail field.Aircraft tail of the aerospace with function easy to disassemble, including base and vertical tail, the front and back of the base is fixedly installed with tailplane, the inside of the base offers cavity, the left wall of the cavity inner cavity is fixedly installed with motor, the output end of the motor is fixedly connected with threaded rod, and the surface screw thread of the threaded rod is equipped with threaded block, is fixedly connected with shank on the right side of the threaded block.Aircraft tail of the aerospace with function easy to disassemble, the rotation of motor output end drives threaded rod to be rotated, threaded rod drives threaded block to be moved to the left on threaded rod, threaded block drives shank to be moved to the left, threaded block drives locating piece to slide to the left on the securing lever, so that shank is detached from fixing groove, lift vertical tail vertically upwards, to reach easy-to-dismount effect.
Description
Technical field
The utility model relates to aircraft tail technical field, specially a kind of aerospace is used with function easy to disassemble
Aircraft tail.
Background technique
Aircraft tail includes tailplane and vertical tail, and tailplane is by the horizontal stabilizer fixed and movable lifting
Rudder composition.Vertical tail includes fixed fixed fin and movable rudder.The major function of empennage is operating aircraft liter
Drop and deflection, and guarantee aircraft smooth flight.Traditional vertical tail is mostly, inconvenient and disassembly integral with fuselage manufacture,
So that maintenance task and maintenance task become complicated, it is therefore desirable to design a kind of easy-to-dismount aircraft tail.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of aerospace and uses and flies with function easy to disassemble
The tail wing solves the problems, such as that existing aircraft tail is not easy to disassembly.
(2) technical solution
In order to achieve the above object, the utility model is achieved by the following technical programs：A kind of aerospace is with having
The aircraft tail of function easy to disassemble, including base and vertical tail, the front and back of the base are fixedly installed with water
The horizontal tail wing, the inside of the base offer cavity, and the left wall of the cavity inner cavity is fixedly installed with motor, the motor it is defeated
Outlet is fixedly connected with threaded rod, and the surface screw thread of the threaded rod is equipped with threaded block, and the right side of the threaded block is fixed to be connected
It is connected to shank, the left wall of the cavity inner cavity is fixedly connected with locating rod, and the locating rod is located at the top of motor, described fixed
The surface activity of position bar is equipped with locating piece, and the bottom of the locating piece is fixedly connected with reinforcing rod, the bottom end of the reinforcing rod
It is fixedly connected at the top of threaded block, the bottom of the vertical tail is fixedly connected with mounting blocks, and the bottom of the mounting blocks is prolonged
The inside of cavity is extended to, the bottom wall of the cavity inner cavity is fixedly installed with docking block, offers docking at the top of the docking block
Slot, one end of the mounting blocks chamber within the cavity extend to the inside of docking groove, the portion of the mounting blocks chamber within the cavity
The left side divided offers fixing groove, and the right end of the shank is plugged on the inside of fixing groove, and the two sides at the top of the base are equal
It is fixedly installed with supporting block, the two sides that the mounting blocks are located at the part of base outer offer thread groove, the supporting block
The inside of thread groove is fixedly mounted on by screw rod.
Preferably, the quantity of the shank and fixing groove is two, and two fixing grooves are respectively positioned on the outer of docking groove
Portion.
Preferably, the right end of the threaded rod is fixedly connected with limited block.
Preferably, the surface of the threaded rod is fixedly installed with gear, and gear is located at the left side of threaded block.
Preferably, one end that the shank is located inside fixing groove is not contacted with the slot bottom of fixing groove.
Preferably, the side of the supporting block is contacted with the side of mounting blocks.
(3) beneficial effect
The utility model provides a kind of aircraft tail of the aerospace with function easy to disassemble.Have following beneficial
Effect：
1, the aerospace use with function easy to disassemble aircraft tail, by setting motor, threaded rod, threaded block,
Shank, locating rod, locating piece and reinforcing rod when needing to dismantle vertical tail, start motor, and the rotation of motor output end drives
Threaded rod is rotated, and threaded rod drives threaded block to be moved to the left on threaded rod, and threaded block drives shank to be moved to the left, spiral shell
Line block drives locating piece to slide to the left on the securing lever, so that shank is detached from fixing groove, lifts vertical tail vertically upwards, from
And easy-to-dismount effect is reached.
2, aircraft tail of the aerospace with function easy to disassemble, by the way that supporting block, thread groove and screw rod is arranged,
When vertical tail is installed, screw rod is tightened, so that screw flight is connected to the inside of thread groove, so that the fixation of vertical tail
It is more stable.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the structure sectional view of the utility model.
In figure：1 base, 2 vertical tails, 3 tailplanes, 4 cavitys, 5 motors, 6 threaded rods, 7 threaded blocks, 8 shanks, 9
Locating rod, 10 locating pieces, 11 reinforcing rods, 12 mounting blocks, 13 docking blocks, 14 docking grooves, 15 fixing grooves, 16 supporting blocks, 17 screw threads
Slot, 18 screw rods, 19 gears.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The utility model embodiment provides a kind of aircraft tail of the aerospace with function easy to disassemble, such as Fig. 1-2
It is shown, including base 1 and vertical tail 2, the front and back of base 1 be fixedly installed with tailplane 3, the inside of base 1
Cavity 4 is offered, the left wall of 4 inner cavity of cavity is fixedly installed with motor 5, the control panel electric connection of motor 5 and peripheral hardware, motor
5 output end is fixedly connected with threaded rod 6, and the right end of threaded rod 6 is fixedly connected with limited block, the surface screw thread peace of threaded rod 6
Equipped with threaded block 7, the surface of threaded rod 6 is fixedly installed with gear 19, and gear 19 is located at the left side of threaded block 7, threaded block 7
Right side is fixedly connected with shank 8, and the left wall of 4 inner cavity of cavity is fixedly connected with locating rod 9, and locating rod 9 is located at the upper of motor 5
Side, the surface activity of locating rod 9 are equipped with locating piece 10, and the bottom of locating piece 10 is fixedly connected with reinforcing rod 11, reinforcing rod 11
Bottom end be fixedly connected with the top of threaded block 7, the bottom of vertical tail 2 is fixedly connected with mounting blocks 12, the bottom of mounting blocks 12
Portion extends to the inside of cavity 4, and the bottom wall of 4 inner cavity of cavity is fixedly installed with docking block 13, and the top of docking block 13 offers pair
Access slot 14, one end that mounting blocks 12 are located at 4 inner cavity of cavity extend to the inside of docking groove 14, and mounting blocks 12 are located at 4 inner cavity of cavity
Part on the left of offer fixing groove 15, the right end of shank 8 is plugged on the inside of fixing groove 15, needs to dismantle vertical tail
When 2, start motor 5, the rotation of 5 output end of motor drives threaded rod 6 to be rotated, and threaded rod 6 drives threaded block 7 in threaded rod
It is moved to the left on 6, threaded block 7 drives shank 6 to be moved to the left, and threaded block 7 drives locating piece 10 to slide to the left in locating rod 9
It is dynamic, so that shank 8 is detached from fixing groove 15, lift vertical tail 2 vertically upwards, to reach easy-to-dismount effect, inserts
The quantity of extension bar 8 and fixing groove 15 is two, and two fixing grooves 15 are respectively positioned on the outside of docking groove 14, and shank 8 is located at
One end inside fixing groove 15 is not contacted with the slot bottom of fixing groove 15, and the two sides at 1 top of base are fixedly installed with supporting block 16,
The two sides that mounting blocks 12 are located at the part outside base 1 offer thread groove 17, and supporting block 16 is fixedly mounted by screw rod 18
In the inside of thread groove 17, the side of supporting block 16 is contacted with the side of mounting blocks 12, when installing vertical tail 2, tightens screw rod
18, so that screw rod 18 is threaded in the inside of thread groove 17, so that the fixation of vertical tail 2 is more stable.
The electric elements occurred in this article are electrically connected with extraneous main controller and 220V alternating current, and main controller can be meter
Calculation machine etc. plays the conventionally known equipment of control.
In conclusion aircraft tail of the aerospace with function easy to disassemble, by the way that motor 5, threaded rod is arranged
6, threaded block 7, shank 8, locating rod 9, locating piece 10 and reinforcing rod 11 when needing to dismantle vertical tail 2, start motor 5, electricity
The rotation of 5 output end of machine drives threaded rod 6 to be rotated, and threaded rod 6 drives threaded block 7 to be moved to the left on threaded rod 6, screw thread
Block 7 drives shank 6 to be moved to the left, and threaded block 7 drives locating piece 10 to slide to the left in locating rod 9, so that shank 8 is detached from
Fixing groove 15 lifts vertical tail 2 vertically upwards, to reach easy-to-dismount effect.
Also, aircraft tail of the aerospace with function easy to disassemble, by the way that supporting block 16, thread groove 17 is arranged
Screw rod 18 is tightened, so that screw rod 18 is threaded in the inside of thread groove 17, to make when vertical tail 2 is installed with screw rod 18
The fixation for obtaining vertical tail 2 is more stable.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of aerospace aircraft tail with function easy to disassemble, including base (1) and vertical tail (2), special
Sign is：The front and back of the base (1) is fixedly installed with tailplane (3), and the inside of the base (1) offers
The left wall of cavity (4), cavity (4) inner cavity is fixedly installed with motor (5), and the output end of the motor (5) is fixedly connected with
The surface screw thread of threaded rod (6), the threaded rod (6) is equipped with threaded block (7), is fixedly connected on the right side of the threaded block (7)
Have shank (8), the left wall of cavity (4) inner cavity is fixedly connected with locating rod (9), and the locating rod (9) is located at motor (5)
Top, the surface activity of the locating rod (9) is equipped with locating piece (10), and the bottom of the locating piece (10) is fixedly connected with
Reinforcing rod (11) is fixedly connected at the top of the bottom end and threaded block (7) of the reinforcing rod (11), the bottom of the vertical tail (2)
Portion is fixedly connected with mounting blocks (12), and the bottom of the mounting blocks (12) extends to the inside of cavity (4), and the cavity (4) is interior
The bottom wall of chamber is fixedly installed with docking block (13), offers docking groove (14), the mounting blocks at the top of the docking block (13)
(12) one end positioned at cavity (4) inner cavity extends to the inside of docking groove (14), and the mounting blocks (12) are located at cavity (4) inner cavity
Part on the left of offer fixing groove (15), the right end of the shank (8) is plugged on the inside of fixing groove (15), the machine
Two sides at the top of seat (1) are fixedly installed with supporting block (16), and the mounting blocks (12) are located at the two of the external part of base (1)
Side offers thread groove (17), and the supporting block (16) is fixedly mounted on the inside of thread groove (17) by screw rod (18).
2. a kind of aircraft tail of the aerospace according to claim 1 with function easy to disassemble, it is characterised in that：
The quantity of the shank (8) and fixing groove (15) is two, and two fixing grooves (15) are respectively positioned on the outer of docking groove (14)
Portion.
3. a kind of aircraft tail of the aerospace according to claim 1 with function easy to disassemble, it is characterised in that：
The right end of the threaded rod (6) is fixedly connected with limited block.
4. a kind of aircraft tail of the aerospace according to claim 1 with function easy to disassemble, it is characterised in that：
The surface of the threaded rod (6) is fixedly installed with gear (19), and gear (19) is located at the left side of threaded block (7).
5. a kind of aircraft tail of the aerospace according to claim 1 with function easy to disassemble, it is characterised in that：
The shank (8) is located at the internal one end of fixing groove (15) and does not contact with the slot bottom of fixing groove (15).
6. a kind of aircraft tail of the aerospace according to claim 1 with function easy to disassemble, it is characterised in that：
The side of the supporting block (16) is contacted with the side of mounting blocks (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820391229.6U CN208165245U (en) | 2018-03-22 | 2018-03-22 | A kind of aircraft tail of the aerospace with function easy to disassemble |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820391229.6U CN208165245U (en) | 2018-03-22 | 2018-03-22 | A kind of aircraft tail of the aerospace with function easy to disassemble |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208165245U true CN208165245U (en) | 2018-11-30 |
Family
ID=64373828
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820391229.6U Expired - Fee Related CN208165245U (en) | 2018-03-22 | 2018-03-22 | A kind of aircraft tail of the aerospace with function easy to disassemble |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208165245U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
-
2018
- 2018-03-22 CN CN201820391229.6U patent/CN208165245U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190521 Address after: 710000 Fu1, No. 361, Ducheng Village, Yanta District, Xi'an City, Shaanxi Province Patentee after: Xi'an Snow Eagle Aviation Technology Co.,Ltd. Address before: 362010 first floor, 128 South Street, Wan An street, Luojiang District, Quanzhou, Fujian. Patentee before: QUANZHOU LUOJIANG KUIFANG SANITATION Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181130 |