CN110435896A - A kind of general-purpose aircraft loudspeaker with sound amplification function - Google Patents

A kind of general-purpose aircraft loudspeaker with sound amplification function Download PDF

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Publication number
CN110435896A
CN110435896A CN201910529728.6A CN201910529728A CN110435896A CN 110435896 A CN110435896 A CN 110435896A CN 201910529728 A CN201910529728 A CN 201910529728A CN 110435896 A CN110435896 A CN 110435896A
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CN
China
Prior art keywords
loudspeaker
shell
sound
loudspeaker shell
general
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
CN201910529728.6A
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Chinese (zh)
Other versions
CN110435896B (en
Inventor
李宁康
梁飞
曾辉
刘韬
熊超林
韩晋平
李峰
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.)
Jiangxi Guanyi Aviation Co ltd
Shanghai Guanyi General Aircraft Co ltd
Original Assignee
Jiangxi Crown General Aviation Co Ltd
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Application filed by Jiangxi Crown General Aviation Co Ltd filed Critical Jiangxi Crown General Aviation Co Ltd
Priority to CN201910529728.6A priority Critical patent/CN110435896B/en
Publication of CN110435896A publication Critical patent/CN110435896A/en
Application granted granted Critical
Publication of CN110435896B publication Critical patent/CN110435896B/en
Active legal-status Critical Current
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04RLOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
    • H04R27/00Public address systems
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04RLOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
    • H04R9/00Transducers of moving-coil, moving-strip, or moving-wire type
    • H04R9/06Loudspeakers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Signal Processing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Details Of Audible-Bandwidth Transducers (AREA)

Abstract

A kind of general-purpose aircraft loudspeaker with sound amplification function disclosed by the invention, including loudspeaker shell, the loudspeaker shell is movably arranged in the installation cavity of the interior shell body of aircraft, the front end of the loudspeaker shell is fixedly installed with one piece of panel, the front end face center of the panel is fixedly installed with one layer of protective net, the two sides of the panel are movably set with a limit clamp respectively up and down, the upper end of the loudspeaker shell is fixedly installed with one of mobile rack, and the upper end of the mobile rack is intermeshed by the gear teeth and a No.1 transmission gear.A kind of general-purpose aircraft loudspeaker with sound amplification function of the present invention, the loudspeaker shell stretched by design activity, inside it by outer sound loudspeaker installation, realization amplifies, and design rack and pinion is driven to control the flexible of loudspeaker shell in the upper end of loudspeaker shell, setting limits clamp to fix loudspeaker shell on loudspeaker shell front console simultaneously, and the vibration of aircraft during take-off and landing is facilitated not interfere with loudspeaker shell.

Description

A kind of general-purpose aircraft loudspeaker with sound amplification function
Technical field
The present invention relates to loudspeaker field, in particular to a kind of general-purpose aircraft loudspeaker with sound amplification function.
Background technique
Loudspeaker is a kind of energy transducer for electric signal being changed into acoustical signal, mainly by magnet, frame, centring disk, Mould ring tapered cone composition, is sound equipment, building block important in broadcast system, and loudspeaker can divide according to principle and structure It for many types, is widely applied in all trades and professions, in the broadcast system and sound system in aircraft, it is also desirable to use Loudspeaker, for issuing broadcast and while playing Video Music uses, but for beauty, the broadcast system of interior of aircraft and Sound system is all embedded in the shell of internal decorative layer, and concordant with the holding of interior facing, under such circumstances loudspeaker at work, Most sound wave is passed in internal decorative layer, and is empathized in internal decorative layer, the sound played so as to cause loudspeaker It is dull and ambiguous, the content that people do not hear loudspeaker broadcasting accurately is influenced, to influence broadcast system and sound equipment system The normal work of system.
Summary of the invention
The main purpose of the present invention is to provide a kind of general-purpose aircraft loudspeaker with sound amplification function, can effectively solve Certainly problem in background technique.
To achieve the above object, the technical scheme adopted by the invention is as follows:
A kind of general-purpose aircraft loudspeaker with sound amplification function, including loudspeaker shell, the loudspeaker shell are movably arranged on winged In the installation cavity of the interior shell body of machine, the front end of the loudspeaker shell is fixedly installed with one piece of panel, in the front end face of the panel Heart position is fixedly installed with one layer of protective net, and the two sides of the panel are movably set with a limit clamp respectively up and down, described The upper end of loudspeaker shell is fixedly installed with one of mobile rack, and the upper end of the mobile rack passes through the gear teeth and a No.1 driving cog Wheel intermeshing, the same gear teeth excessively in the upper end of the No.1 transmission gear and No. two transmission gear are intermeshed, and described two The side of number transmission gear, which is separately connected with outside one, adjusts ring, and the rear end sides of the loudspeaker shell are respectively equipped with a sound-muffling box, The Internal back end of the loudspeaker shell is equipped with an outer sound loudspeaker, and the bottom of the outer sound loudspeaker is fixedly installed to peace by mounting rack The bottom behaveing affectedly.
Preferably, the width of the panel is equal to three times of loudspeaker shell tail width, and the both sides of the head of loudspeaker shell is logical Curved surface is crossed to seamlessly transit to wide with panel, the height of the panel be equal to the height of loudspeaker shell and the height of mobile rack it With.
Preferably, the two sides side upper and lower position of the panel offers a flexible card slot respectively inwards, described flexible Card slot is internally provided with a limit spring, and one end of the limit spring is fixedly mounted on the bottom of flexible card slot, described As soon as the other end of limit spring is then connected with a piece postive stop baffle, the limit clamp is fixedly mounted on the another side of postive stop baffle On, the postive stop baffle is located at the inside of flexible card slot, and limits clamp then protruding flexible card slot, and snap onto installation cavity On the inner wall of two sides in the corresponding limit card slot opened up.
Preferably, the mobile rack is fixedly mounted on the upper end of loudspeaker shell, the No.1 driving cog by welding manner Wheel is located at the surface of mobile rack, and No.1 transmission gear is movably arranged on peace by a No.1 installation axle in the center point On the inner wall behaveing affectedly, No. two transmission gears are then located at the surface of No.1 transmission gear, and No. two transmission gears are same On the inner wall that the center point is movably arranged on installation cavity by No. two installation axles, the side of No. two transmission gears is fixed It is coaxially connected with outside one and adjusts ring, the outer edge for adjusting ring passes through the regulating tank on interior shell body surface, and is exposed at interior Adorn the outside of shell.
Preferably, the outer sound loudspeaker is mainly by T iron, magnet, Hua Si, voice coil, bullet wave, frame, cone and dustproof cover group At the magnet is covered in T iron and this can be compressed by China, and the head of the voice coil is fixedly connected with wave is played, and voice coil Tail portion pass through Hua Si and magnet and cover in T iron, the another side for playing wave is close to the bottom surface of frame, the cone and dustproof cover All it is mounted on the inside of frame.
Preferably, the component that the sound-muffling box and loudspeaker shell are integrally formed, the inner hollow of the sound-muffling box, and Inside is filled with silencing cotton.
Compared with prior art, the invention has the following beneficial effects:
For the loudspeaker on existing aircraft there are the drawbacks of, amplify first at the exterior design of loudspeaker horn one Shell, the big tail portion in the head of loudspeaker shell is small, plays the role of poly- sound and amplifies, and furthermore installs a toothed rack in the upper end of loudspeaker shell, and Two transmission gears are engaged in the upper end of rack gear, ring, the outer edge for adjusting ring are adjusted outside coaxially connected one of the gear of the top Expose internal decorative layer, facilitates the outer stretching retraction for adjusting the i.e. controllable loudspeaker shell of ring of people's rotation, under the premise of not influencing appearance Loudspeaker is set to reach good amplifying effect;Secondly, by installing a sound-muffling box in the tail end two sides of loudspeaker shell, using in box The silencing cotton of filling blocks the transmitting between sound and internal decorative layer, reduces the generation of sympathetic response, guarantees that the sound after amplifying is clear It is clear;Finally, four limit clamps are arranged by the panel two sides in loudspeaker shell front end, can block after facilitating entire loudspeaker shell to be retracted Firmly, it prevents from causing loudspeaker shell surprisingly to be stretched out because airframe vibrates, causes unnecessary using trouble.
Detailed description of the invention
Fig. 1 is a kind of overall structure diagram of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 2 is a kind of internal structure cross-sectional view of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 3 is a kind of transmission connection plan view of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 4 is a kind of transmission connection top view of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 5 is a kind of outer sound loudspeaker structural schematic diagram of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 6 is a kind of limiting card header structure schematic diagram of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 7 is a kind of scheme of installation of the general-purpose aircraft loudspeaker with sound amplification function of the present invention;
Fig. 8 is a kind of sound-muffling box schematic diagram of internal structure of the general-purpose aircraft loudspeaker with sound amplification function of the present invention.
In figure: 1, loudspeaker shell;2, panel;3, protective net;4, clamp is limited;5, mobile rack;6, outer sound loudspeaker;7, it installs Frame;8, No.1 transmission gear;9, No.1 installation axle;10, No. two transmission gears;11, No. two installation axles;12, outer adjusting ring;13, Regulating tank;14, interior shell body;15, T iron;16, magnet;17, Hua Si;18, voice coil;19, wave is played;20, frame;21, cone;22, Dustproof cover;23, stretch card slot;24, limit spring;25, postive stop baffle;26, limit card slot;27, installation cavity;28, sound-muffling box; 29, silencing cotton.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to Specific embodiment, the present invention is further explained.
In the description of the present invention, it should be noted that term " on ", "lower", "inner", "outside" " front end ", " rear end ", The orientation or positional relationship of the instructions such as " both ends ", " one end ", " other end " is to be based on the orientation or positional relationship shown in the drawings, only It is that for the convenience of describing the present invention and simplifying the description, rather than the device or element of indication or suggestion meaning must have specifically Orientation is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, term " first ", " the Two " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation " " is set Be equipped with ", " connection " etc., shall be understood in a broad sense, such as " connection ", may be a fixed connection, may be a detachable connection or one Connect to body;It can be mechanical connection, be also possible to be electrically connected;It can be directly connected, it can also be indirect by intermediary It is connected, can be the connection inside two elements.For the ordinary skill in the art, on being understood with concrete condition State the concrete meaning of term in the present invention.
As shown in figures 1-8, a kind of general-purpose aircraft loudspeaker with sound amplification function, including loudspeaker shell 1, loudspeaker shell 1 are living In the installation cavity 27 of the dynamic interior shell body 14 for being mounted on aircraft, the front end of loudspeaker shell 1 is fixedly installed with one piece of panel 2, panel 2 Front end face center is fixedly installed with one layer of protective net 3, and the two sides of panel 2 are movably set with a limit clamp respectively up and down 4, the upper end of loudspeaker shell 1 is fixedly installed with one of mobile rack 5, and the upper end of mobile rack 5 is driven by the gear teeth and a No.1 Gear 8 is intermeshed, and the same gear teeth excessively in the upper end of No.1 transmission gear 8 and No. two transmission gear 10 are intermeshed, and No. two The side of transmission gear 10, which is separately connected with outside one, adjusts ring 12, and the rear end sides of loudspeaker shell 1 are respectively equipped with a sound-muffling box 28, The Internal back end of loudspeaker shell 1 is equipped with an outer sound loudspeaker 6, and the bottom of outer sound loudspeaker 6 is fixedly installed to installation cavity by mounting rack 7 27 bottom;
The width of panel 2 is equal to three times of 1 tail width of loudspeaker shell, and the both sides of the head of loudspeaker shell 1 is flat by curved surface Sliding to transit to wide with panel 2, the sum of the height of panel 2 is equal to the height of loudspeaker shell 1 and the height of mobile rack 5;Panel 2 Two sides side upper and lower position offer a flexible card slot 23 respectively inwards, flexible card slot 23 is internally provided with a limit Spring 24, one end of limit spring 24 are fixedly mounted on the bottom of flexible card slot 23, and the other end of limit spring 24 is then connected with As soon as piece postive stop baffle 25, limit clamp 4 is fixedly mounted on the another side of postive stop baffle 25, and postive stop baffle 25 is located at flexible card The inside of slot 23, and the then protruding flexible card slot 23 of clamp 4 is limited, and snap onto correspondence on 27 two sides inner wall of installation cavity and open up Limit card slot 26 in;Mobile rack 5 is fixedly mounted on the upper end of loudspeaker shell 1 by welding manner, and No.1 transmission gear 8 is located at The surface of mobile rack 5, and No.1 transmission gear 8 is movably arranged on installation by a No.1 installation axle 9 in the center point On the inner wall of chamber 27, No. two transmission gears 10 are then located at the surface of No.1 transmission gear 8, and No. two transmission gears 10 are same It is movably arranged on the inner wall of installation cavity 27 in the center point by No. two installation axles 11, the side of No. two transmission gears 10 is solid Surely it being coaxially connected with outside one and adjusts ring 12, the outer edge for adjusting ring 12 passes through the regulating tank 13 on 14 surface of interior shell body, and It is exposed at the outside of interior shell body 14;Outer sound loudspeaker 6 mainly by T iron 15, magnet 16, Hua Si 17, voice coil 18, play wave 19, frame 20, Cone 21 and dustproof cover 22 form, and 16 sets of magnet in T iron 15 and 17 can be compressed, the head of voice coil 18 and bullet by magnificent this Wave 19 is fixedly connected, and the tail portion of voice coil 18 pass through China this 17 with 16 sets of magnet in T iron 15, play wave 19 another side be close to basin The bottom surface of frame 20, cone 21 and dustproof cover 22 are all mounted on the inside of frame 20;What sound-muffling box 28 and loudspeaker shell 1 were integrally formed Component, the inner hollow of sound-muffling box 28, and it is filled with silencing cotton 29.
It should be noted that the present invention is a kind of general-purpose aircraft loudspeaker with sound amplification function, by outer sound loudspeaker 6 exterior design installs a loudspeaker shell 1, and the wide tail portion in the head of loudspeaker shell 1 is narrow, can play good poly- sound and amplify effect Fruit, and it is arranged one one by the way that a mobile rack 5 is fixedly mounted in the upper end of loudspeaker shell 1, while in the upper end of mobile rack 5 Number transmission gear 8 and mobile rack 5 are intermeshed, and are equally passed through the gear teeth in the upper end of No.1 transmission gear 8 and are passed with one No. two Moving gear 10 is intermeshed, and is connected in the side of No. two transmission gears 10 and is adjusted ring 12 outside one, and the outer edge for adjusting ring 12 is logical It crosses the regulating tank 13 that 14 surface of interior shell body opens up to stretch out, people is facilitated to be rotated with hand;In actual use, it is first depending on left hand Law, when being broadcasted, sound is converted to electric signal before this, the diatom of belt current it is vertical with the magnetic line of force put magnet south into Between the arctic, conducting wire will by the magnetic line of force and both electric currents interaction and move, then a piece of vibrating diaphragm is attached to this root diatom On, as curent change vibrating diaphragm just generates the movement of front and back, so that sound sending is converted electrical signals into, at this point, passenger passes through Outer adjusting ring 12 is rotated down, so that No. two coaxial transmission gears 10 is driven to rotate clockwise along No. two installation axles 11, and The No.1 transmission gear 8 engaged with No. two transmission gears 10 is rotated counterclockwise along No.1 installation axle 9 therewith, to drive movement Rack gear 5 is protruding, i.e., drive loudspeaker shell 1 move out, at this point, the limit clamp 4 of 1 front console of loudspeaker shell, 2 two sides by The extruding of limit card slot 26 retracts in flexible card slot 23, continues to rotate outer adjusting ring 12, until loudspeaker shell 1 is completely from installation cavity 27 Interior stretching, at this point, the sound-muffling box 28 of 1 tail portion of loudspeaker shell is tightly attached on the inner wall of installation cavity 27, the sound portion that outer sound loudspeaker 6 issues Divide and is transmitted through sound-muffling box 28 to interior shell body 14 by the shell of 1 tail portion of loudspeaker shell, and during transmitting, sound, which enters, to disappear In silencing cotton 29 inside sound box 28, via the fine and close pore on 29 surface of silencing cotton and inside, by air molecule friction and glue Resistance hysteresis, and fiber fines is made to make mechanical oscillation, to enable sound to be changed into thermal energy, to obstruct sound to interior shell body 14 transmitting avoids sound and empathizes in interior shell body 14 phenomenon, and people is caused not hear the sound of loudspeaker sending, And most sound is after loudspeaker shell 1 amplifies, form the sound beam more concentrated transmits forwards, facilitates people and listens Chhnang The particular content for the sound that sound device issues, plays good amplifying effect, when without using loudspeaker, need to only be rotated up Outer adjusting ring 12 retracts loudspeaker shell 1 after the transmitting of No. two transmission gears 10, No.1 transmission gear 8 and mobile rack 5 In installation cavity 27, when the panel 2 of 1 front end of loudspeaker shell is flushed with 14 surface of interior shell body, the limit clamp 4 of 2 two sides of panel exists It is sticked into limit card slot 26 under the action of limit spring 24 again after extruding, so that loudspeaker shell 1 is fixed in installation cavity 27, Guarantee in takeoff and landing, slight vibration will not make 1 auto-extending of loudspeaker shell.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention.The technology of the industry Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this The principle of invention, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its Equivalent thereof.

Claims (6)

1. a kind of general-purpose aircraft loudspeaker with sound amplification function, it is characterised in that: including loudspeaker shell (1), the loudspeaker shell (1) it is movably arranged in the installation cavity (27) of the interior shell body (14) of aircraft, the front end of the loudspeaker shell (1) is fixedly installed with one Block panel (2), the front end face center of the panel (2) are fixedly installed with one layer of protective net (3), and the two of the panel (2) Side is movably set with a limit clamp (4) respectively up and down, and the upper end of the loudspeaker shell (1) is fixedly installed with one of mobile rack (5), the upper end of the mobile rack (5) is intermeshed by the gear teeth and a No.1 transmission gear (8), the No.1 driving cog The same gear teeth excessively in upper end and No. two transmission gear (10) for taking turns (8) are intermeshed, and the one of No. two transmission gears (10) Side is separately connected with outside one and adjusts ring (12), and the rear end sides of the loudspeaker shell (1) are respectively equipped with a sound-muffling box (28), described The Internal back end of loudspeaker shell (1) is equipped with an outer sound loudspeaker (6), and the bottom of the outer sound loudspeaker (6) is fixed by mounting rack (7) It is installed to the bottom of installation cavity (27).
2. a kind of general-purpose aircraft loudspeaker with sound amplification function according to claim 1, it is characterised in that: the face The width of plate (2) is equal to three times of loudspeaker shell (1) tail width, and the both sides of the head of loudspeaker shell (1) is smoothed by curved surface Cross to wide with panel (2), the height of the panel (2) be equal to the height of loudspeaker shell (1) and the height of mobile rack (5) it With.
3. a kind of general-purpose aircraft loudspeaker with sound amplification function according to claim 1, it is characterised in that: the face The two sides side upper and lower position of plate (2) offers a flexible card slot (23), the inside of the flexible card slot (23) respectively inwards It is provided with a limit spring (24), one end of the limit spring (24) is fixedly mounted on the bottom of flexible card slot (23), institute State limit spring (24) as soon as the other end be then connected with a piece postive stop baffle (25), the limit clamp (4) is fixedly mounted on limit On the another side of position baffle (25), the postive stop baffle (25) is located at the inside of flexible card slot (23), and limit clamp (4) then to It is outer to stretch out flexible card slot (23), and snap on the inner wall of installation cavity (27) two sides in the corresponding limit card slot (26) opened up.
4. a kind of general-purpose aircraft loudspeaker with sound amplification function according to claim 1, it is characterised in that: the shifting Carry-over bar (5) is fixedly mounted on the upper end of loudspeaker shell (1) by welding manner, and the No.1 transmission gear (8) is located at mobile tooth The surface of item (5), and No.1 transmission gear (8) is movably arranged on installation by a No.1 installation axle (9) in the center point On the inner wall of chamber (27), No. two transmission gears (10) are then located at the surface of No.1 transmission gear (8), and No. two transmissions Gear (10) is equally movably arranged on the inner wall of installation cavity (27) in the center point by No. two installation axles (11), and described two The side fixing coaxial of number transmission gear (10) is connected with outside one and adjusts ring (12), and the outer edge for adjusting ring (12) passes through Regulating tank (13) on interior shell body (14) surface, and it is exposed at the outside of interior shell body (14).
5. a kind of general-purpose aircraft loudspeaker with sound amplification function according to claim 1, it is characterised in that: described outer Sound loudspeaker (6) are mainly by T iron (15), magnet (16), Hua Si (17), voice coil (18), bullet wave (19), frame (20), cone (21) It is formed with dustproof cover (22), the magnet (16) covers on T iron (15) and can be compressed by Hua Si (17), the voice coil (18) head is fixedly connected with wave (19) are played, and the tail portion of voice coil (18) passes through Hua Si (17) and magnet (16) and covers in T iron (15) on, the another side for playing wave (19) is close to the bottom surface of frame (20), and the cone (21) is all installed with dustproof cover (22) In the inside of frame (20).
6. a kind of general-purpose aircraft loudspeaker with sound amplification function according to claim 1, it is characterised in that: described to disappear The component that sound box (28) and loudspeaker shell (1) are integrally formed, the inner hollow of the sound-muffling box (28), and be filled with Silencing cotton (29).
CN201910529728.6A 2019-06-19 2019-06-19 General aircraft loudspeaker with sound amplifying function Active CN110435896B (en)

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CN110435896B CN110435896B (en) 2022-08-09

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113784246A (en) * 2021-11-11 2021-12-10 江西科技学院 Make things convenient for public address equipment of dismouting

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Publication number Priority date Publication date Assignee Title
CN201549091U (en) * 2009-10-21 2010-08-11 王昊 Multifunctional ferule
CN102833663A (en) * 2011-06-16 2012-12-19 飞跃科技股份有限公司 Retractable microphone
CN104902380A (en) * 2015-04-08 2015-09-09 苏州三星电子电脑有限公司 Electronic equipment provided with variable-volume sound box structure
CN106945837A (en) * 2017-04-14 2017-07-14 上海博历机械科技有限公司 A kind of bird repellent unmanned plane of utilization high efficiency dye sensitization solar battery
CN108477135A (en) * 2018-04-28 2018-09-04 陈钦旺 One kind being used for garden fruit tree birds device for driving away

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201549091U (en) * 2009-10-21 2010-08-11 王昊 Multifunctional ferule
CN102833663A (en) * 2011-06-16 2012-12-19 飞跃科技股份有限公司 Retractable microphone
CN104902380A (en) * 2015-04-08 2015-09-09 苏州三星电子电脑有限公司 Electronic equipment provided with variable-volume sound box structure
CN106945837A (en) * 2017-04-14 2017-07-14 上海博历机械科技有限公司 A kind of bird repellent unmanned plane of utilization high efficiency dye sensitization solar battery
CN108477135A (en) * 2018-04-28 2018-09-04 陈钦旺 One kind being used for garden fruit tree birds device for driving away

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113784246A (en) * 2021-11-11 2021-12-10 江西科技学院 Make things convenient for public address equipment of dismouting

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