CN219068324U - DSP aerial sound wave synthesizer - Google Patents

DSP aerial sound wave synthesizer Download PDF

Info

Publication number
CN219068324U
CN219068324U CN202320137506.1U CN202320137506U CN219068324U CN 219068324 U CN219068324 U CN 219068324U CN 202320137506 U CN202320137506 U CN 202320137506U CN 219068324 U CN219068324 U CN 219068324U
Authority
CN
China
Prior art keywords
knob
fuselage
sound wave
dsp
observation panel
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.)
Active
Application number
CN202320137506.1U
Other languages
Chinese (zh)
Inventor
兰兴文
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.)
Zhongshan Jinye Electronic Technology Co ltd
Original Assignee
Zhongshan Jinye Electronic 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 Zhongshan Jinye Electronic Technology Co ltd filed Critical Zhongshan Jinye Electronic Technology Co ltd
Priority to CN202320137506.1U priority Critical patent/CN219068324U/en
Application granted granted Critical
Publication of CN219068324U publication Critical patent/CN219068324U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Details Of Audible-Bandwidth Transducers (AREA)

Abstract

The utility model relates to the technical field of sound wave synthesis and discloses a DSP (digital Signal processor) aerial sound wave synthesis device, which comprises a machine body, wherein an observation panel is arranged on the side wall of the machine body, a left channel UV (ultraviolet) meter and a right channel UV meter are respectively arranged on the side wall of the observation panel, a display screen is arranged on the side wall of the observation panel, which is positioned at the interval of the left channel UV meter and the right channel UV meter, an audio effect rotating button is arranged on the side wall of the machine body, which is positioned below the observation panel, a low-frequency rotating button is arranged on the right side of the audio effect rotating button, a high-frequency rotating button is arranged on the right side of the low-frequency rotating button, a dynamic balance rotating button is arranged on the right side of the high-frequency rotating button, and adjusting rotating buttons are respectively arranged on the two sides of the machine body, which is positioned on the observation panel. The utility model is convenient for adjusting tone color, can quickly achieve ideal hearing effect and improves using effect.

Description

DSP aerial sound wave synthesizer
Technical Field
The utility model relates to the technical field of sound wave synthesis, in particular to a DSP air sound wave synthesis device.
Background
DSP, digital signal processing, is the use of digital processing, such as by a computer or more specialized digital signal processor, to perform a wide variety of signal processing operations in which the signal processed in this way is a series of numbers representing continuously variable samples in the time, space or frequency domain, applications of digital signal processors including audio and speech processing, sonar, radar and other sensor array processing, spectral density estimation, statistical signal processing, digital image processing, telecommunication signal processing.
In the prior art, in the EQ adjusting process in the sound wave synthesizing process, tone color is single, and the sound wave synthesizing process has certain locality and influences the using effect. Therefore, the application designs a DSP air sound wave synthesizing device.
Disclosure of Invention
The utility model aims to solve the problems that in the prior art, in the EQ adjusting process in the sound wave synthesizing process, tone color is single, certain locality is achieved, and the using effect is affected.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides an aerial sound wave synthesizer of DSP, includes the fuselage, be provided with the observation panel on the lateral wall of fuselage, be provided with left channel UV table and right channel UV table on the lateral wall of observation panel respectively, be provided with the display screen on the lateral wall that observation panel is located left channel UV table and right channel UV table interval department, be equipped with the audio switch on the lateral wall that the fuselage is located the observation panel below, the right side of audio switch is equipped with the low frequency switch, the right side of low frequency switch is equipped with the high frequency switch, the right side of high frequency switch is equipped with dynamic balance switch, the both sides that the fuselage is located the observation panel are provided with the regulation switch respectively, the both sides of fuselage are provided with loudspeaker respectively, one side that the fuselage deviates from observation panel is provided with the mounting panel, be provided with audio jack on the lateral wall of mounting panel.
Preferably, a USB socket is provided below the adjusting knob, and the side walls of the sound effect knob, the low-frequency knob, the high-frequency knob, the dynamic balance knob and the adjusting knob are respectively provided with anti-skid lines.
Preferably, the fuselage is equipped with the apron on being located the lateral wall of loudspeaker, be provided with the fixture block on the lateral wall of apron, fixture block joint sets up in the clearance department of fuselage and loudspeaker.
Preferably, a plurality of supports are arranged at the bottom of the machine body, and anti-slip pads are respectively arranged at one ends of the supports, deviating from the machine body.
Preferably, the fuselage is provided with the antenna on the lateral wall of mounting panel, be provided with the buckle on the lateral wall of mounting panel, the antenna joint sets up the inner wall at the buckle.
Preferably, a plurality of strip-shaped heat dissipation openings are formed in the side wall of the mounting plate.
Compared with the prior art, the utility model provides a DSP air sound wave synthesizing device, which has the following beneficial effects:
1. according to the DSP aerial sound wave synthesizing device, the sound wave coverage range is increased by arranging the loudspeakers left and right, the tone color in the space range is uniform, the listening consistency is improved, the sound effect, low-frequency, high-frequency and dynamic balance buttons can be controlled by rotating the sound effect buttons, the low-frequency, high-frequency and dynamic balance buttons, and the personal hearing effects of different sounds in different environments can be met.
2. The DSP aerial sound wave synthesizing device can display the output power of each channel in real time through the left channel UV table and the right channel UV table, can intuitively adjust the output state of each channel, and has quicker and more accurate sound effect adjustment.
The device has the advantages that the device has no part which is the same as or can be realized by adopting the prior art, the tone color can be conveniently adjusted, the ideal hearing effect can be quickly achieved, and the using effect is improved.
Drawings
FIG. 1 is a front view of a DSP air sound wave synthesizer according to the present utility model;
fig. 2 is a rear view of the structure of a DSP air-borne sound wave synthesizing device according to the present utility model.
In the figure: 1 fuselage, 2 observation panel, 3 left channel UV table, 4 right channel UV table, 5 display screen, 6 audio switch, 7 low frequency switch, 8 high frequency switch, 9 dynamic balance switch, 10 adjustment switch, 11USB socket, 12 loudspeaker, 13 apron, 14 fixture block, 15 anti-skidding lines, 16 support, 17 mounting panel, 18 antenna, 19 bar thermovent, 20 audio socket, 21 buckle.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
In the description of the present utility model, it should be understood that the terms "upper," "lower," "front," "rear," "left," "right," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the present utility model and to simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
Referring to fig. 1-2, a DSP aerial sound wave synthesizing device, including fuselage 1, be provided with observation panel 2 on the lateral wall of fuselage 1, be provided with left channel UV table 3 and right channel UV table 4 on the lateral wall of observation panel 2 respectively, be provided with display screen 5 on the lateral wall that observation panel 2 is located left channel UV table 3 and right channel UV table 4 interval department, be equipped with audio knob 6 on the lateral wall that fuselage 1 is located observation panel 2 below, the right side of audio knob 6 is equipped with low frequency knob 7, the right side of low frequency knob 7 is equipped with high frequency knob 8, the right side of high frequency knob 8 is equipped with dynamic balance knob 9, fuselage 1 is located the both sides of observation panel 2 and is provided with adjusting knob 10 respectively, fuselage 1's both sides are provided with loudspeaker 12 respectively, fuselage 1 deviates from the lateral wall of observation panel 2 and is provided with mounting panel 17, be provided with audio jack 20 on the lateral wall of mounting panel 17.
The below of adjusting the button 10 is provided with USB socket 11, sound effect button 6, low frequency button 7, high frequency button 8, dynamic balance button 9 and adjusting the button 10 set up respectively in anti-skidding line 15 on the lateral wall, fuselage 1 is located the lateral wall of loudspeaker 12 and is equipped with apron 13, be provided with fixture block 14 on the lateral wall of apron 13, fixture block 14 joint sets up in fuselage 1 and loudspeaker 12's clearance department, fuselage 1's bottom is provided with a plurality of supports 16, a plurality of supports 16 deviate from fuselage 1's one end and are provided with the slipmat respectively, fuselage 1 is provided with antenna 18 on the lateral wall of mounting panel 17, be provided with buckle 21 on the lateral wall of mounting panel 17, antenna 18 joint sets up the inner wall at buckle 21, a plurality of bar thermovent 19 have been seted up on the lateral wall of mounting panel 17.
In the utility model, when in use, the sound wave coverage area is increased by arranging the loudspeakers 12 left and right, the tone color in the space range is uniform, the hearing consistency is improved, the hardware in the machine body 1 can be controlled to adjust the sound effect, the low frequency, the high frequency and the dynamic balance by rotating the sound effect rotary button 6, the low frequency rotary button 7, the high frequency rotary button 8 and the dynamic balance rotary button 9, the personal hearing effect of different sounds in different environments can be satisfied, the output power of each sound channel can be displayed in real time by the left sound channel UV table 3 and the right sound channel UV table 4, the output state of each channel can be intuitively adjusted, and the sound effect is adjusted more quickly and accurately. The cover plate 13 can play certain protective effect to loudspeaker 12, can improve the stability of fuselage 1 through support 16, can improve the radiating effect of fuselage 1 through bar thermovent 19, and buckle 21 is convenient for fix antenna 20, and antenna 20 can strengthen the signal of fuselage 1.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.

Claims (6)

1. The utility model provides an aerial sound wave synthesizer of DSP, includes fuselage (1), its characterized in that: be provided with on the lateral wall of fuselage (1) and observe panel (2), be provided with left channel UV table (3) and right channel UV table (4) on the lateral wall of observing panel (2) respectively, be provided with display screen (5) on the lateral wall of observing panel (2) and right channel UV table (4) interval department in observation panel (2) position, be equipped with audio knob (6) on the lateral wall of fuselage (1) below observation panel (2), the right side of audio knob (6) is equipped with low frequency knob (7), the right side of low frequency knob (7) is equipped with high frequency knob (8), the right side of high frequency knob (8) is equipped with dynamic balance knob (9), the both sides that fuselage (1) are located observation panel (2) are provided with regulation knob (10) respectively, the both sides of fuselage (1) are provided with loudspeaker (12) respectively, one side that fuselage (1) were located observation panel (2) side is provided with mounting panel (17), the lateral wall (20) that are provided with on mounting panel (17) are deviate from to audio.
2. The DSP air-borne sound wave synthesizing device according to claim 1, wherein: the anti-slip device is characterized in that a USB socket (11) is arranged below the adjusting knob (10), and anti-slip lines (15) are respectively arranged on the side walls of the sound effect knob (6), the low-frequency knob (7), the high-frequency knob (8), the dynamic balance knob (9) and the adjusting knob (10).
3. The DSP air-borne sound wave synthesizing device according to claim 1, wherein: the loudspeaker is characterized in that the side wall of the loudspeaker body (1) located at the loudspeaker (12) is provided with a cover plate (13), the side wall of the cover plate (13) is provided with a clamping block (14), and the clamping block (14) is clamped and arranged at the gap between the loudspeaker body (12) and the loudspeaker body (1).
4. The DSP air-borne sound wave synthesizing device according to claim 1, wherein: the bottom of fuselage (1) is provided with a plurality of supports (16), a plurality of support (16) deviate from the one end of fuselage (1) and are provided with slipmat respectively.
5. The DSP air-borne sound wave synthesizing device according to claim 1, wherein: the antenna is characterized in that an antenna (18) is arranged on the side wall of the mounting plate (17) of the machine body (1), a buckle (21) is arranged on the side wall of the mounting plate (17), and the antenna (18) is clamped on the inner wall of the buckle (21).
6. The DSP air-borne sound wave synthesizing device according to claim 1, wherein: a plurality of strip-shaped heat dissipation openings (19) are formed in the side wall of the mounting plate (17).
CN202320137506.1U 2023-02-07 2023-02-07 DSP aerial sound wave synthesizer Active CN219068324U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320137506.1U CN219068324U (en) 2023-02-07 2023-02-07 DSP aerial sound wave synthesizer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320137506.1U CN219068324U (en) 2023-02-07 2023-02-07 DSP aerial sound wave synthesizer

Publications (1)

Publication Number Publication Date
CN219068324U true CN219068324U (en) 2023-05-23

Family

ID=86375684

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320137506.1U Active CN219068324U (en) 2023-02-07 2023-02-07 DSP aerial sound wave synthesizer

Country Status (1)

Country Link
CN (1) CN219068324U (en)

Similar Documents

Publication Publication Date Title
JP3703528B2 (en) Electroacoustic conversion system and sound field forming apparatus
JP2945983B2 (en) Speaker device
EP0165733B1 (en) Method and apparatus for measuring and correcting acoustic characteristic in sound field
Shaw Acoustical features of the human external ear
US3824343A (en) Multiple driver dynamic loud speaker
TW200603651A (en) Speaker system, and speaker cluster system
US3483945A (en) Omnidirectional sound system
US20060291669A1 (en) Audio Signal Processing
CN112788480B (en) Sound production structure and wearable equipment
CN219068324U (en) DSP aerial sound wave synthesizer
CN201138867Y (en) Active acoustics in linear array
EP1864548B1 (en) A multiple loudspeaker device
Suzuki et al. New design method of a binaural microphone array using multiple constraints
Baumfield et al. Performance of assistive listening devices using insertion gain measures
CN210007872U (en) audio output device
US20180041832A1 (en) Blended passive microphone
US2926740A (en) Acoustic control device for loudspeakers
CA2456298A1 (en) A method of and apparatus for producing apparent multidimensional sound
CN210927955U (en) Angle-adjustable combined sound box
CN103269477A (en) Air voice sound field control method and system for implementing same
US3243525A (en) Hearing intensifying and directing apparatus
JP2002291086A (en) Loud speaker system
CN213280078U (en) Single loudspeaker device
CN219938515U (en) Double-channel directional sounding device
CN216437466U (en) Intelligent musical instrument sound box

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant