CN110512539A - A kind of all-wing aircraft Shape closed formula gobo - Google Patents
A kind of all-wing aircraft Shape closed formula gobo Download PDFInfo
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- CN110512539A CN110512539A CN201910821053.2A CN201910821053A CN110512539A CN 110512539 A CN110512539 A CN 110512539A CN 201910821053 A CN201910821053 A CN 201910821053A CN 110512539 A CN110512539 A CN 110512539A
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- China
- Prior art keywords
- gobo
- wing aircraft
- sound insulation
- aircraft shape
- wing
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F8/00—Arrangements for absorbing or reflecting air-transmitted noise from road or railway traffic
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
Abstract
The invention discloses a kind of all-wing aircraft Shape closed formula goboes, including all-wing aircraft shape gobo main body, sound insulation periproct, Bian Ping;The all-wing aircraft shape gobo main body includes that multiple all-wing aircraft shape gobo sections are composed;The all-wing aircraft shape gobo section is equipped with left wing's gobo, right flank gobo;Left wing's gobo, the shape of right flank gobo are similar to the shape that wing when sea-gull flight is unfolded;Left wing's gobo is equipped with left front skeleton, left light transmission sound insulation piece;The right flank gobo is equipped with skeleton, right light transmission sound insulation piece before the right side;The beneficial effects of the present invention are: the design incorporates a pair of of all-wing aircraft of seabird in gobo, is composed equipped with all-wing aircraft shape gobo section;Form it into the natural transition in space, vision, light;It is plastic simplicity, slim and graceful;And soundproof effect is more preferable, structure is firmer.
Description
Technical field
The present invention relates to gobo technical field, in particular to a kind of all-wing aircraft Shape closed formula gobo.
Background technique
Sound signal is particularly significant to human normal life.Modern is but often exposed to many to damage human health
In life noise.The mankind experience extraneous vibration and be sent to brain through hair cell sensitive in cochlea is read as sound signal.
But, hair cell can not regenerate, once impaired just can not reply.On the other hand, sound also will affect the blood pressure of the mankind, psychology etc.
Physical condition.Therefore, how the sound of suitable control environment, lower the noise that damages for body, and promote life
Quality just becomes an important topic.With the improvement of living standards, people propose higher want to living and working environment
It asks, control noise becomes more important for the quality for improving people's lives and work;With highway height and rail traffic
Development, the operation of automobile or train, the noise of caused vibration can more acutely, and many traffic routes all pass through
Many cities, the normal life of noise severe jamming Zhe Yan road resident, or even influence nearby school, Research Center, hospital, bank
Deng normal operation;So needing to install abatvoix on its road;Abatvoix is a kind of ideal sound-proof decorative materials.But only
Be only abatvoix soundproof effect it is limited, so needing a kind of closed gobo.
Currently, existing closed gobo is all as house, respectively there is a port on both sides, the disadvantage is that: one, appearance is old
It is old, unsightly;Two, soundproof effect is poor;Three, structure is complicated, and not firm;Four, translucency is bad.
Summary of the invention
The invention mainly solves the technical problem of providing a kind of all-wing aircraft Shape closed formula gobo, structure is beautiful, it is firm,
Succinctly, and soundproof effect is more preferable.
To solve the above-mentioned problems, the present invention provides a kind of all-wing aircraft Shape closed formula gobo, including all-wing aircraft shape gobo master
Body, sound insulation periproct, Bian Ping;The all-wing aircraft shape gobo main body includes that multiple all-wing aircraft shape gobo sections are composed;The all-wing aircraft
Shape gobo section is equipped with left wing's gobo, right flank gobo;Left wing's gobo, the shape of right flank gobo and sea-gull fly
When wing expansion shape it is similar;Left wing's gobo is equipped with left front skeleton, left light transmission sound insulation piece;The right flank gobo is set
There are skeleton, right light transmission sound insulation piece before the right side;The both ends of the left front skeleton are equipped with left fixed feet;The both ends of skeleton are equipped with before the right side
Right fixed feet;It inlays on left front skeleton in the front of the left light transmission sound insulation piece;The front of the right light transmission sound insulation piece is embedded in the right side
On preceding skeleton;The left fixed feet, right fixed feet are for inlaying installation;The side screen includes that multiple noise insulation blocks are composed;Institute
The front for stating noise insulation block is set there are two three arm of angle faces;Three arm of angle face is equipped with sound insulation piece;The side screen is for being mounted on by two
On the both sides of different directions road composition highway, the all-wing aircraft shape gobo main body is mounted in the top of side screen, the sound insulation periproct
It is combined with all-wing aircraft shape gobo main body one end;The left light transmission sound insulation piece, right light transmission sound insulation piece are all that Pierced Aluminum Plank and Asia are made every effort to overcome
Plate is formed by stacking.
Furtherly, the material of skeleton is light steel before the left front skeleton, the right side.
Furtherly, the vertical view of the sound insulation periproct is petal, and material is acoustic material.
Furtherly, the material of the sound insulation piece is acoustic material.
Furtherly, when the multiple all-wing aircraft shape gobo section is combined, a left side for the all-wing aircraft shape gobo section of previous section
The back of light transmission sound insulation piece, right light transmission sound insulation piece, be embedded in the all-wing aircraft shape gobo section of corresponding later section left front skeleton, it is right before
In skeleton.
The invention discloses a kind of all-wing aircraft Shape closed formula goboes, including all-wing aircraft shape gobo main body, sound insulation periproct, side
Screen;The all-wing aircraft shape gobo main body includes that multiple all-wing aircraft shape gobo sections are composed;The all-wing aircraft shape gobo section is equipped with
Left wing's gobo, right flank gobo;The shape and the shape of wing expansion when sea-gull flight of left wing's gobo, right flank gobo
Shape is similar;Left wing's gobo is equipped with left front skeleton, left light transmission sound insulation piece;The right flank gobo is equipped with skeleton, the right side before the right side
Light transmission sound insulation piece;The beneficial effects of the present invention are: the design incorporates a pair of of all-wing aircraft of seabird in gobo, is equipped with all-wing aircraft shape
Gobo section is composed;Form it into the natural transition in space, vision, light;It is plastic simplicity, slim and graceful;And soundproof effect is more
Good, structure is firmer.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, and the attached drawing in describing is of the invention one
A little embodiments to those skilled in the art without creative efforts, can also be according to these
Attached drawing obtains other accompanying drawings.
Fig. 1 is the stereoscopic schematic diagram being mounted on highway of the invention.
Fig. 2 is schematic top plan view of the invention.
Fig. 3 is front schematic view of the invention.
Fig. 4 is left wing's gobo schematic diagram of the invention.
Fig. 5 is right flank gobo schematic diagram of the invention.
Fig. 6 is noise insulation block stereoscopic schematic diagram of the invention.
Fig. 7 is noise insulation block decomposition diagram of the invention.
Fig. 8 is side screen side stereoscopic schematic diagram of the invention.
Below with reference to embodiment, and referring to attached drawing, the realization, the function and the advantages of the object of the present invention are made furtherly
It is bright.
Specific embodiment
In order to keep the purposes, technical schemes and advantages of invention clearer, below in conjunction with attached in the embodiment of the present invention
Figure, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is invention one
Section Example, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not doing
Every other embodiment obtained under the premise of creative work out, shall fall within the protection scope of the present invention.
Embodiment one:
As shown in Figures 1 to 8, a kind of all-wing aircraft Shape closed formula gobo, including all-wing aircraft shape gobo main body 1, sound insulation
Periproct 2, Bian Ping 3;The all-wing aircraft shape gobo main body 1 includes that multiple all-wing aircraft shape gobo sections 10 are composed;The all-wing aircraft shape
Gobo section 10 is equipped with left wing's gobo 11, right flank gobo 12;Left wing's gobo 11, right flank gobo 12 shape with
The shape that wing is unfolded when sea-gull flight is similar;Left wing's gobo 11 is equipped with left front skeleton 111, left light transmission sound insulation piece 112;
The right flank gobo 12 is equipped with skeleton 121, right light transmission sound insulation piece 122 before the right side;The both ends of the left front skeleton 111 are equipped with left solid
Determine foot 1111;The both ends of skeleton 121 are equipped with right fixed feet 1211 before the right side;It inlays in the front of the left light transmission sound insulation piece 112
On left front skeleton 111;The front of the right light transmission sound insulation piece 122 is embedded in front of the right side on skeleton 121;The left fixed feet 1111,
Right fixed feet 1211 is for inlaying installation;The side screen 3 includes that multiple noise insulation blocks 31 are composed;The front of the noise insulation block 31
If there are two three arm of angle faces 311;Three arm of angle face 311 is equipped with sound insulation piece 3111;The side screen 3 is for being mounted on by two not
On the both sides of equidirectional road composition highway, the all-wing aircraft shape gobo main body 1 is mounted in the top of side screen 3, the sound insulation periproct 2 with
The combination of 1 one end of all-wing aircraft shape gobo main body;The left light transmission sound insulation piece 112, right light transmission sound insulation piece 122 are all Pierced Aluminum Plank and Asia
Plate is made every effort to overcome to be formed by stacking.
As shown in Figures 1 to 5, the material of skeleton 121 is light steel before the left front skeleton 111, the right side.
As shown in Fig. 2, the vertical view of the sound insulation periproct 2 is petal, and material is acoustic material.
Such as Fig. 1, Fig. 3, Fig. 6, shown, the material of the sound insulation piece 3111 is acoustic material.
As shown in Figures 1 to 5, when the multiple all-wing aircraft shape gobo section 10 is combined, the all-wing aircraft shape sound insulation of previous section
Screen saves 10 left light transmission sound insulation piece 112, the back of right light transmission sound insulation piece 122, is embedded in the all-wing aircraft shape gobo of corresponding later section
The left front skeleton 111 of section 10, it is right before in skeleton 121.
The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations;Although with reference to the foregoing embodiments
Invention is explained in detail, those skilled in the art should understand that: it still can be to aforementioned each implementation
Technical solution documented by example is modified or equivalent replacement of some of the technical features, and these are modified or replace
It changes, the spirit and scope for technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution.
Claims (5)
1. a kind of all-wing aircraft Shape closed formula gobo, which is characterized in that including all-wing aircraft shape gobo main body (1), sound insulation periproct (2),
Bian Ping (3);The all-wing aircraft shape gobo main body (1) includes that multiple all-wing aircraft shape gobo sections (10) are composed;The all-wing aircraft shape
Gobo section (10) is equipped with left wing's gobo (11), right flank gobo (12);Left wing's gobo (11), right flank gobo
(12) shape is similar to the shape that wing when sea-gull flight is unfolded;Left wing's gobo (11) be equipped with left front skeleton (111),
Left light transmission sound insulation piece (112);The right flank gobo (12) is equipped with skeleton (121), right light transmission sound insulation piece (122) before the right side;It is described
The both ends of left front skeleton (111) are equipped with left fixed feet (1111);The both ends of skeleton (121) are equipped with right fixed feet before the right side
(1211);It inlays on left front skeleton (111) in the front of the left light transmission sound insulation piece (112);The right light transmission sound insulation piece (122)
Front is embedded in front of the right side on skeleton (121);The left fixed feet (1111), right fixed feet (1211) are for inlaying installation;It is described
Bian Ping (3) includes that multiple noise insulation blocks (31) are composed;The front of the noise insulation block (31) is set there are two three arm of angle faces (311);
Three arm of angle face (311) is equipped with sound insulation piece (3111);The side screen (3) forms public affairs by two different directions roads for being mounted on
On the both sides on road, the all-wing aircraft shape gobo main body (1) is mounted in the top of side screen (3), the sound insulation periproct (2) and all-wing aircraft shape every
The combination of sound screen main body (1) one end;The left light transmission sound insulation piece (112), right light transmission sound insulation piece (122) are all Pierced Aluminum Plank and sub- power
Gram plate is formed by stacking.
2. a kind of all-wing aircraft Shape closed formula gobo according to claim 1, which is characterized in that the left front skeleton (111), the right side
The material of preceding skeleton (121) is light steel.
3. a kind of all-wing aircraft Shape closed formula gobo according to claim 1, which is characterized in that sound insulation periproct (2) bow
Be considered as it is petal, and material be acoustic material.
4. a kind of all-wing aircraft Shape closed formula gobo according to claim 1, which is characterized in that the material of the sound insulation piece (3111)
Matter is acoustic material.
5. a kind of all-wing aircraft Shape closed formula gobo according to claim 1, which is characterized in that the multiple all-wing aircraft shape gobo
When section (10) is combined, the left light transmission sound insulation piece (112) of the all-wing aircraft shape gobo section (10) of previous section, right light transmission sound insulation piece
(122) back, be embedded in the all-wing aircraft shape gobo section (10) of corresponding later section left front skeleton (111), it is right before skeleton (121)
It is interior.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201910821053.2A CN110512539B (en) | 2019-08-28 | 2019-08-28 | Closed sound insulation screen of all-wing aircraft shape |
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CN201910821053.2A CN110512539B (en) | 2019-08-28 | 2019-08-28 | Closed sound insulation screen of all-wing aircraft shape |
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CN110512539A true CN110512539A (en) | 2019-11-29 |
CN110512539B CN110512539B (en) | 2021-05-28 |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2703027Y (en) * | 2003-08-15 | 2005-06-01 | 程越 | Combined whole-sound shadow protective screen |
CN102182152A (en) * | 2011-04-06 | 2011-09-14 | 上海船舶运输科学研究所 | Whole image sound barrier for urban quick lane and tunnel portal |
CN203475335U (en) * | 2013-08-16 | 2014-03-12 | 赖庆国 | Totally-closed composite sound absorbing and insulating screen unit and sound insulating system with same |
CN204676446U (en) * | 2015-04-21 | 2015-09-30 | 上海中驰集团有限公司 | The totally-enclosed sound barrier of ventilated type |
CN108611998A (en) * | 2018-05-23 | 2018-10-02 | 江苏金阳交通工程有限公司 | A kind of highway sound barrier |
-
2019
- 2019-08-28 CN CN201910821053.2A patent/CN110512539B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2703027Y (en) * | 2003-08-15 | 2005-06-01 | 程越 | Combined whole-sound shadow protective screen |
CN102182152A (en) * | 2011-04-06 | 2011-09-14 | 上海船舶运输科学研究所 | Whole image sound barrier for urban quick lane and tunnel portal |
CN203475335U (en) * | 2013-08-16 | 2014-03-12 | 赖庆国 | Totally-closed composite sound absorbing and insulating screen unit and sound insulating system with same |
CN204676446U (en) * | 2015-04-21 | 2015-09-30 | 上海中驰集团有限公司 | The totally-enclosed sound barrier of ventilated type |
CN108611998A (en) * | 2018-05-23 | 2018-10-02 | 江苏金阳交通工程有限公司 | A kind of highway sound barrier |
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