CN107804451A - A kind of structure of the mechanical empennage fixed fin that wafts of damping - Google Patents
A kind of structure of the mechanical empennage fixed fin that wafts of damping Download PDFInfo
- Publication number
- CN107804451A CN107804451A CN201711216705.7A CN201711216705A CN107804451A CN 107804451 A CN107804451 A CN 107804451A CN 201711216705 A CN201711216705 A CN 201711216705A CN 107804451 A CN107804451 A CN 107804451A
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- CN
- China
- Prior art keywords
- rib
- damping
- wing
- wafts
- mechanical
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
Abstract
The present invention provides a kind of structure of the mechanical empennage fixed fin that wafts of damping, including fuselage, flank, engine, and wing after longitudinal wing and transverse direction, described flank is arranged on the left and right sides of fuselage；Engine is arranged on the bottom of flank；Longitudinal wing is arranged on rear side of the top of fuselage；Wing is arranged at left and right sides of the rear of fuselage after transverse direction.Second rib of the present invention is provided with multiple, improves the protection effect of the equipment；The setting covered using fiber-reinforced resin is covered, strengthens the damping, buffering effect of the equipment；Fixing hole is additionally provided with rib body, improves the fixed effect of the equipment；Outer breach and interior breach are respectively set to interior arc line type, can reduce the impulsive force of outside, and the present invention can allow between aerial machinery when colliding with each other, and reduce damage.
Description
Technical field
The invention belongs to the mechanical empennage that wafts of frame for movement technical field of wafting, more particularly to a kind of damping vertically to stabilize
The structure in face.
Background technology
Float boat, be it is a kind of can suspension in low latitude and in room, movement, the daily living article of operation, instrument, toy,
The general name of the aerial article of the major class of equipment, instrument, flying robot etc. one, according to function, feature, purposes, navigation of floaing includes in the industry
Have eliminate sound it is quiet float, the room in room floats, it is extreme low-altitude in near-earth float, the light of night operation floats, rapid flight fly
Float, can manned people is floatd, intelligent program is high intelligence float, can enter in water and the skyborne water that can float floats, is deep into cave well
The hole at bottom floatd, be not afraid of baked wheaten cake and the fire of high temperature is floatd, micro- in small space is floatd etc..Navigation industry of floaing has been started people are daily
People and thing in life bring up to a kind of aerial new technology path, and navigation industry of floaing has three with navigation, the difference of civil aviaton, space flight industry
Point：The difference of first mesh, for the purpose of " traveling ", " hanging " is means for navigation, civil aviaton, space flight industry, and navigation industry of floaing is with " outstanding
It is empty " for the purpose of, " movement " is means；The field of second application is different, and navigation, civil aviaton, space flight industry substitutes and of development
It is horizontal and vertical carrier, so application is extremely narrow；Boat of floaing technology almost can apply to all industries, several
Can substitute and develop all industries, the field set foot in is extremely extensive, when an article by its " suspension " in the air when, can produce
Raw many unexpected marvellous effects；3rd culture is different, and navigation, civil aviaton, space technology are entirely to be instructed with Western Culture
Technology caused by lower, inflexible, mechanical, inhumanity, boat of floaing technology are technologies caused by under being instructed with the culture of Chinese root, taking human as
This, it has peace and quiet, safety, daily life, the characteristic of hommization.
Because the extensive appearance for the boat product that floats, and the improvement of ecological environment, birds can be more, and with the sky of human lives
Between closer to, waft machinery when wafting, may be subjected to the collision of more aerial objects, such as birds, boat of floaing product.Work as hair
During raw collision, there is the problem of protection effect difference and high cost for the traditional front-end architecture of machinery that wafts at present.
Because the extensive appearance for the boat product that floats, the improvement of ecological environment, birds can be more, and with the space of human lives more
Closely, machinery is wafted when wafting, and may be subjected to the collision of more aerial objects, such as birds, boat of floaing product.When touching
When hitting, there is the problem of protection effect difference and high cost for the traditional front-end architecture of machinery that wafts at present.
Therefore, the structure for inventing a kind of mechanical empennage fixed fin that wafts of damping seems very necessary.
The content of the invention
The present invention provides a kind of structure of the mechanical empennage fixed fin that wafts of damping, when the machinery that wafts is collided
The front-end architecture of energy-absorbing, to solve, the existing mechanical front-end architecture protection effect that wafts is poor and cost is high asks
Topic.
In order to achieve the above object, the present invention uses following technical scheme.
A kind of structure of the mechanical empennage fixed fin that wafts of damping, including fuselage, flank, engine, longitudinal wing and
Wing after transverse direction, described flank are arranged on the left and right sides of fuselage；Described engine is arranged on the bottom of flank；Described is vertical
It is arranged on to wing on rear side of the top of fuselage；Wing is arranged at left and right sides of the rear of fuselage after described transverse direction；Described is vertical
Include wing-body, crossbeam, the first rib, second rib and covering to wing, described crossbeam is arranged on a left side for wing-body
Side；The first described rib is arranged on the top of crossbeam；Described covering is installed in the lower section of crossbeam；Described second rib peace
Mounted in the centre position of crossbeam.
Preferably, described second rib is provided with multiple.
Preferably, the spacing between described second rib is arranged to 20cm to 40cm.
Preferably, described covering is covered using fiber-reinforced resin.
Preferably, described second rib includes rib body, outer breach and interior breach, and rib body is arranged on crossbeam
On；Described outer breach is opened in the top of rib body；Described interior breach is opened in the bottom of rib body.
Preferably, it is additionally provided with fixing hole on described rib body.
Preferably, described outer breach and interior breach are respectively set to interior arc line type.
A kind of structure of the mechanical empennage fixed fin that wafts of damping of the present invention, the feelings that article is widely present in the air
Under condition, mechanical front-end architecture technical field of wafting can be applied to, the present invention can allow between aerial machinery when colliding with each other, and reduce
Damage.Meanwhile beneficial effects of the present invention are：
1. in the present invention, described second rib is provided with multiple, is advantageous to improve the protection effect of the equipment.
2. in the present invention, described covering is advantageous to strengthen subtracting for the equipment using the setting of fiber-reinforced resin covering
Shake buffering effect.
3. in the present invention, fixing hole is additionally provided with described rib body, be advantageous to improve the fixed effect of the equipment
Fruit.
4. in the present invention, described outer breach and interior breach are respectively set to interior arc line type, be advantageous to that outside can be reduced
Impulsive force.
Brief description of the drawings
Fig. 1 is the schematic diagram of one embodiment.
Fig. 2 is the structural representation of longitudinal wing of the present invention.
Fig. 3 is the structural representation of the second rib of the present invention.
In figure：
1st, fuselage；2nd, flank；3rd, engine；4th, longitudinal wing；41st, wing-body；42nd, crossbeam；43rd, the first rib；44th, the second rib
Bone；441st, rib body；4411st, fixing hole；442nd, outer breach；443rd, interior breach；45th, cover；5th, wing after transverse direction.
Embodiment
The present invention is described further below in conjunction with accompanying drawing：
Embodiment：
As shown in accompanying drawing 1 to accompanying drawing 3
The present invention provides a kind of structure of the mechanical empennage fixed fin that wafts of damping, including fuselage 1, flank 2, engine 3, indulges
Wing 5 after to wing 4 and transverse direction, described flank 2 are arranged on the left and right sides of fuselage 1；Described engine 3 is arranged on flank 2
Bottom；Described longitudinal wing 4 is arranged on rear side of the top of fuselage 1；After wing 5 is arranged on fuselage 1 after described transverse direction
The side left and right sides；Described longitudinal wing 4 includes wing-body 41, crossbeam 42, the first rib 43, second rib 44 and covering
45, described crossbeam 42 is arranged on the left side of wing-body 41；The first described rib 43 is arranged on the top of crossbeam 42；It is described
Covering 45 be arranged on crossbeam 42 lower section；Described second rib 44 is arranged on the centre position of crossbeam 42.
In above-described embodiment, specifically, described second rib 44 be provided with it is multiple.
In above-described embodiment, specifically, the spacing between described second rib 44 is arranged to 20cm to 40cm.
In above-described embodiment, specifically, described covering 45 is covered using fiber-reinforced resin.
In above-described embodiment, specifically, described second rib 44 includes rib body 441, outer breach 442 and interior breach
443, rib body 441 is arranged on crossbeam 42；Described outer breach 442 is opened in the top of rib body 441；Described is interior
Breach 443 is opened in the bottom of rib body 441.
In above-described embodiment, specifically, being additionally provided with fixing hole 4411 on described rib body 441.
In above-described embodiment, specifically, described outer breach 442 and interior breach 443 is respectively set to interior arc line type.
Operation principle
In the course of the work, second rib 44 sets multiple protection effects for improving the equipment to the present invention, and it is fiber to cover 45
Reinforced resin covers the damping, buffering effect that can strengthen the equipment；Fixing hole 4411 is provided with rib body 441 to be carried
The fixed effect of the high equipment；Outer breach 442 and interior breach 443, which are respectively set to interior arc line type, can reduce the impact of outside
Power.
Using technical solutions according to the invention, or those skilled in the art is under the inspiration of technical solution of the present invention,
Similar technical scheme is designed, and reaches above-mentioned technique effect, is to fall into protection scope of the present invention.
Claims (7)
1. a kind of structure of the aircraft tail fixed fin of damping and its a kind of mechanical empennage that wafts of damping of shock-dampening method hang down
The structure of straight stabilization, it is characterised in that it includes fuselage（1）, flank（2）, engine（3）, longitudinal wing（4）With machine after transverse direction
The wing（5）, described flank（2）Installed in fuselage（1）The left and right sides；Described engine（3）Installed in flank（2）Bottom；
Described longitudinal wing（4）Installed in fuselage（1）Top on rear side of；Wing after described transverse direction（5）Installed in fuselage（1）After
The side left and right sides；Described longitudinal wing（4）Including wing-body（41）, crossbeam（42）, the first rib（43）, second rib
（44）And covering（45）, described crossbeam（42）Installed in wing-body（41）Left side；The first described rib（43）Installation
In crossbeam（42）Top；Described covering（45）Installed in crossbeam（42）Lower section；Described second rib（44）It is arranged on
Crossbeam（42）Centre position.
2. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 1, it is characterised in that described
Second rib（44）It is provided with multiple.
3. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 1, it is characterised in that described
Second rib（44）Between spacing be arranged to 20cm to 40cm.
4. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 1, it is characterised in that described
Covering（45）Covered using fiber-reinforced resin.
5. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 1, it is characterised in that described
Second rib（44）Including rib body（441）, outer breach（442）With interior breach（443）, rib body（441）It is arranged on
Crossbeam（42）On；Described outer breach（442）It is opened in rib body（441）Top；Described interior breach（443）It is opened in
Rib body（441）Bottom.
6. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 5, it is characterised in that described
Rib body（441）On be additionally provided with fixing hole（4411）.
7. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 5, it is characterised in that described
Outer breach（442）With interior breach（443）It is respectively set to interior arc line type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711216705.7A CN107804451A (en) | 2017-11-28 | 2017-11-28 | A kind of structure of the mechanical empennage fixed fin that wafts of damping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711216705.7A CN107804451A (en) | 2017-11-28 | 2017-11-28 | A kind of structure of the mechanical empennage fixed fin that wafts of damping |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107804451A true CN107804451A (en) | 2018-03-16 |
Family
ID=61590179
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711216705.7A Withdrawn CN107804451A (en) | 2017-11-28 | 2017-11-28 | A kind of structure of the mechanical empennage fixed fin that wafts of damping |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107804451A (en) |
-
2017
- 2017-11-28 CN CN201711216705.7A patent/CN107804451A/en not_active Withdrawn
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180316 |
|
| WW01 | Invention patent application withdrawn after publication |