CN207595238U - 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
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- CN207595238U CN207595238U CN201721615663.XU CN201721615663U CN207595238U CN 207595238 U CN207595238 U CN 207595238U CN 201721615663 U CN201721615663 U CN 201721615663U CN 207595238 U CN207595238 U CN 207595238U
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- wafts
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Abstract
The utility model provides a kind of structure of aircraft tail fixed fin of damping and its a kind of structure of the mechanical empennage fixed fin that wafts of damping of shock-dampening method, including fuselage, flank, engine, wing after longitudinal wing and transverse direction, flank are mounted on the left and right sides of fuselage；Engine is mounted on the lower part of flank；Longitudinal wing is mounted on rear side of the top of fuselage；Wing is mounted at left and right sides of the rear of fuselage after transverse direction.The utility model second rib is provided with multiple, improves the protection effect of the equipment；The setting covered using fiber-reinforced resin is covered, enhances the damping, buffering effect of the equipment；Mounting hole is additionally provided on rib cage ontology, improves the fixed effect of the equipment；Outer notch and interior notch are respectively set to interior arc line type, external impact force can be reduced, the utility model can allow aerial because all rib cages all support the contact with covering of traditional front-end architecture also in solvent front, the support for covering both ends is to be adjoined by rib cage to carrying out, since the fracture of covering will before a solvent rib fastener be starting point, if collided with each other between a flight machinery, damage is reduced.
Description
Technical field
The mechanical empennage that wafts that the utility model belongs to waft frame for movement technical field more particularly to a kind of damping is vertical
The structure of stabilization.
Background technology
Float boat, be it is a kind of can suspension in low latitude and in room, movement, the daily necessities of operation, tool, toy,
The general name of the aerial article of one major class such as equipment, instrument, flying robot, 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 floats, be not afraid of baked wheaten cake and the fire of high temperature floats, micro- in small space is floatd etc..Navigation industry of floaing has been started people are daily
People and object 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 range is extremely narrow；Boat of floaing technology almost can be applied 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；Third culture is different, and navigation, civil aviaton, space technology are entirely to be instructed with Western Culture
The technology of lower generation, inflexible, mechanical, inhumanity, boat of floaing technology are to instruct the lower technology generated with Chinese root culture, taking human as
This, has the characteristic of peace and quiet, safety, daily life, hommization.
Because the float extensive appearance of boat product and the improvement of ecological environment, birds can be more, and with the sky of human lives
Between closer to wafting 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, wafting at present, there is the problem of protection effect difference and high cost for the traditional front-end architecture of machinery.
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, wafting at present, there is the problem of protection effect difference and high cost for the traditional front-end architecture of machinery.
Therefore, the structure for inventing a kind of mechanical empennage fixed fin that wafts of damping is very necessary.
Utility model content
The utility model provides a kind of structure of the mechanical empennage fixed fin that wafts of damping, and wafting, machinery is touched
The front-end architecture of energy-absorbing when hitting, with solve it is existing waft mechanical front-end architecture protection effect difference and cost it is high
Problem.
In order to achieve the above object, the utility model 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, the flank are mounted on the left and right sides of fuselage；The engine is mounted on the lower part of flank；Described is vertical
It is mounted on to wing on rear side of the top of fuselage；Wing is mounted at left and right sides of the rear of fuselage after the transverse direction；Described is vertical
Include wing-body, crossbeam, the first rib cage, second rib and covering to wing, the crossbeam is mounted on a left side for wing-body
Side；First rib cage is mounted on the top of crossbeam；The covering is mounted on the lower section of crossbeam；The second rib peace
Mounted in the centre position of crossbeam.
Preferably, the second rib is provided with multiple.
Preferably, the spacing between the second rib is set as 20cm to 40cm.
Preferably, the covering is covered using fiber-reinforced resin.
Preferably, the second rib includes rib cage ontology, outer notch and interior notch, and rib cage ontology is mounted on crossbeam
On；The outer notch is opened in the top of rib cage ontology；The interior notch is opened in the lower part of rib cage ontology.
Preferably, it is additionally provided with mounting hole on the rib cage ontology.
Preferably, the outer notch and interior notch are respectively set to interior arc line type.
A kind of structure of the mechanical empennage fixed fin that wafts of the damping of the utility model, in the air article be widely present
In the case of, it can be applied to mechanical front-end architecture technical field of wafting, the utility model, which can allow between aerial machinery, mutually collides
When hitting, damage is reduced.Meanwhile the beneficial effects of the utility model are：
1. in the utility model, the second rib is provided with multiple, is conducive to improve the protection effect of the equipment.
2. in the utility model, the covering is conducive to enhance the equipment using the setting of fiber-reinforced resin covering
Damping, buffering effect.
3. in the utility model, mounting hole is additionally provided on the rib cage ontology, is conducive to improve the fixation of the equipment
Effect.
4. in the utility model, the outer notch and interior notch are respectively set to interior arc line type, be conducive to reduce
External impact force.
Description of the drawings
Fig. 1 is the schematic diagram of one embodiment.
Fig. 2 is the structure diagram of longitudinal wing of the utility model.
Fig. 3 is the structure diagram of the second rib of the utility model.
In figure：
1st, fuselage；2nd, flank；3rd, engine；4th, longitudinal wing；41st, wing-body；42nd, crossbeam；43rd, the first rib cage；44th,
Two rib cages；441st, rib cage ontology；4411st, mounting hole；442nd, outer notch；443rd, interior notch；45th, it covers；5th, wing after transverse direction.
Specific embodiment
The utility model is described further below in conjunction with attached drawing：
Embodiment：
As shown in attached drawing 1 to attached drawing 3
The utility model provides a kind of structure of the mechanical empennage fixed fin that wafts of damping, including fuselage 1, flank 2,
Engine 3, wing 5 after longitudinal wing 4 and transverse direction, the flank 2 are mounted on the left and right sides of fuselage 1；The engine 3 is installed
In the lower part of flank 2；Longitudinal wing 4 is mounted on rear side of the top of fuselage 1；Wing 5 is mounted on machine after the transverse direction
At left and right sides of the rear of body 1；Longitudinal wing 4 includes wing-body 41, crossbeam 42, the first rib cage 43, second rib 44
With covering 45, the crossbeam 42 is mounted on the left side of wing-body 41；First rib cage 43 is mounted on the upper of crossbeam 42
Portion；The covering 45 is mounted on the lower section of crossbeam 42；The second rib 44 is mounted on the centre position of crossbeam 42.
In above-described embodiment, specifically, the second rib 44 be provided with it is multiple.
In above-described embodiment, specifically, the spacing between the second rib 44 is set as 20cm to 40cm.
In above-described embodiment, specifically, the covering 45 is covered using fiber-reinforced resin.
In above-described embodiment, specifically, the second rib 44 includes rib cage ontology 441, outer notch 442 and interior notch
443, rib cage ontology 441 is mounted on crossbeam 42；The outer notch 442 is opened in the top of rib cage ontology 441；Described is interior
Notch 443 is opened in the lower part of rib cage ontology 441.
In above-described embodiment, specifically, being additionally provided with mounting hole 4411 on the rib cage ontology 441.
In above-described embodiment, specifically, the outer notch 442 and interior notch 443 is respectively set to interior arc line type.
Operation principle
During the work time, second rib 44 sets multiple protection effects for improving the equipment to the utility model, covers
45 can enhance the damping, buffering effect of the equipment for fiber-reinforced resin covering；Mounting hole is provided on rib cage ontology 441
4411 can improve the fixed effect of the equipment；Outer notch 442 and interior notch 443, which are respectively set to interior arc line type, can be reduced outside
The impact force in portion.
Using technical solution described in the utility model or those skilled in the art in technical solutions of the utility model
Under inspiration, similar technical solution is designed, and reaches above-mentioned technique effect, is the protection model for falling into the utility model
It encloses.
Claims (7)
1. the structure of the mechanical empennage fixed fin that wafts of a kind of damping, which is characterized in that it includes fuselage（1）, flank
（2）, engine（3）, longitudinal wing（4）With wing after transverse direction（5）, the flank（2）Mounted on fuselage（1）The left and right sides；
The engine（3）Mounted on flank（2）Lower part；Longitudinal wing（4）Mounted on fuselage（1）Top on rear side of；Institute
Wing after the transverse direction stated（5）Mounted on fuselage（1）Rear at left and right sides of；Longitudinal wing（4）Including wing-body
（41）, crossbeam（42）, the first rib cage（43）, second rib（44）And covering（45）, the crossbeam（42）Mounted on wing sheet
Body（41）Left side；First rib cage（43）Mounted on crossbeam（42）Top；The covering（45）Mounted on crossbeam
（42）Lower section；The second rib（44）Mounted on crossbeam（42）Centre position.
2. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as described in claim 1, which is characterized 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 described in claim 1, which is characterized in that described
Second rib（44）Between spacing be set as 20cm to 40cm.
4. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as described in claim 1, which is characterized in that described
Covering（45）It is covered using fiber-reinforced resin.
5. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as described in claim 1, which is characterized in that described
Second rib（44）Including rib cage ontology（441）, outer notch（442）With interior notch（443）, rib cage ontology（441）It is mounted on
Crossbeam（42）On；The outer notch（442）It is opened in rib cage ontology（441）Top；The interior notch（443）It is opened in
Rib cage ontology（441）Lower part.
6. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 5, which is characterized in that described
Rib cage ontology（441）On be additionally provided with mounting hole（4411）.
7. the structure of the mechanical empennage fixed fin that wafts of a kind of damping as claimed in claim 5, which is characterized in that described
Outer notch（442）With interior notch（443）It is respectively set to interior arc line type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721615663.XU CN207595238U (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 |
|---|---|---|---|
| CN201721615663.XU CN207595238U (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 |
|---|---|
| CN207595238U true CN207595238U (en) | 2018-07-10 |
Family
ID=62761345
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721615663.XU Active CN207595238U (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) | CN207595238U (en) |
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2017
- 2017-11-28 CN CN201721615663.XU patent/CN207595238U/en active Active
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