CN110512539A - A kind of all-wing aircraft Shape closed formula gobo - Google Patents

A kind of all-wing aircraft Shape closed formula gobo Download PDF

Info

Publication number
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
Authority
CN
China
Prior art keywords
gobo
wing aircraft
sound insulation
aircraft shape
wing
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.)
Granted
Application number
CN201910821053.2A
Other languages
Chinese (zh)
Other versions
CN110512539B (en
Inventor
禹道锋
黄英华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Yuking Sound Barrier Engineering Technology Co Ltd
Original Assignee
Shenzhen Yuking Sound Barrier Engineering Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenzhen Yuking Sound Barrier Engineering Technology Co Ltd filed Critical Shenzhen Yuking Sound Barrier Engineering Technology Co Ltd
Priority to CN201910821053.2A priority Critical patent/CN110512539B/en
Publication of CN110512539A publication Critical patent/CN110512539A/en
Application granted granted Critical
Publication of CN110512539B publication Critical patent/CN110512539B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01FADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F8/00Arrangements for absorbing or reflecting air-transmitted noise from road or railway traffic

Landscapes

  • 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

A kind of all-wing aircraft Shape closed formula gobo
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.
CN201910821053.2A 2019-08-28 2019-08-28 Closed sound insulation screen of all-wing aircraft shape Active CN110512539B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910821053.2A CN110512539B (en) 2019-08-28 2019-08-28 Closed sound insulation screen of all-wing aircraft shape

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910821053.2A CN110512539B (en) 2019-08-28 2019-08-28 Closed sound insulation screen of all-wing aircraft shape

Publications (2)

Publication Number Publication Date
CN110512539A true CN110512539A (en) 2019-11-29
CN110512539B CN110512539B (en) 2021-05-28

Family

ID=68630111

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910821053.2A Active CN110512539B (en) 2019-08-28 2019-08-28 Closed sound insulation screen of all-wing aircraft shape

Country Status (1)

Country Link
CN (1) CN110512539B (en)

Citations (5)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
CN110512539B (en) 2021-05-28

Similar Documents

Publication Publication Date Title
CN208346666U (en) A kind of sound barrier mounting structure
CN210216199U (en) Composite sound-absorbing board
CN110512539A (en) A kind of all-wing aircraft Shape closed formula gobo
CN204662293U (en) Road and bridge sound arrester
CN207663760U (en) A kind of car holographic projector facilitating adjusting
CN204402293U (en) Door bottom crack sound arrester
CN111335197B (en) Suppression type sound insulation screen
CN211897932U (en) Inverted trapezoidal closed sound-proof screen
CN211395424U (en) Triangular closed sound insulation screen
CN211472227U (en) Bionic closed sound-proof screen
CN207512950U (en) Three-dimensional alliteration impedance micropunch period ultrabroad band flush sound absorption structure
CN212336370U (en) Sound-insulation noise-reduction plate
CN210216200U (en) Composite acoustic board embedded with ya li ke board
CN212103724U (en) Inhibition type sound insulation screen
CN214089549U (en) Built-in fixed steel cable's concatenation sound insulation screen
CN205636377U (en) Railway roadbed abatvoix
CN109989364A (en) A kind of compoiste sound-absorbing board
CN108133681A (en) A kind of car holographic projector for facilitating adjusting
CN108423033A (en) A kind of rail traffic signal of communication processing method and processing system
CN202925485U (en) Landscape composite sound barrier
CN210766463U (en) Building gives sound insulation with acoustic celotex board that has guard action
CN201685498U (en) Sound-isolating sponge
CN201874479U (en) Construction frame for horizontal drilling in bridge section sound barrier
CN206328699U (en) A kind of traffic safety protection solar energy reflector
CN204644923U (en) Novel municipal greening wire mesh grating

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
GR01 Patent grant
GR01 Patent grant