Holographic Sound Field Inspection Instrument Compressor Condition Monitoring SolutionIssuing time:2026-09-26 22:48 Holographic Sound Field Inspection Instrument |
| Dimension | Conventional Contact Monitoring | Holographic Sound Field Inspection Instrument |
|---|---|---|
| Monitoring method | Point-wise contact measurement of vibration / temperature / pressure | Non-contact panoramic acoustic monitoring |
| Coverage | Limited mounting positions; blind zones exist | 360° global field of view; full-machine coverage |
| Deployment conditions | Shutdown for retrofit; difficult explosion-proof wiring | Inspection mode requiring neither shutdown nor retrofit |
| Diagnostic depth | Threshold alarming; empirical judgment | Spatial source inversion; intelligent diagnosis |
Technical route: spherical-array panoramic acquisition → spherical harmonic sound field reconstruction → acoustic–optical fusion visualization → global physical quantity acquisition → state inversion and intelligent diagnosis.

By virtue of its high degree of three-dimensional spatial symmetry, the spherical microphone array synchronously maps all radiated noise arriving from every direction within a single measurement cycle. Within the mathematical framework, the spatial sound pressure field can be expanded by the Spherical Harmonic Transform (SHT): in the received sound pressure model p(k)=A(k)S(k)+z(k), the directional steering matrix A(k) can be decomposed as A(k)=Y(Ω)B(kr)YH(Γ), where the frequency term is concentrated in the diagonal matrix B(kr) and the source-direction matrix YH(Γ) no longer contains a frequency component. This achieves complete frequency–direction decoupling, so that the cross-spectral matrix can be computed directly in the frequency domain with spatial spectrum smoothing—laying the foundation for localization and reconstruction of broadband sound sources.
When processing the characteristic noise of a compressor (such as low-frequency fundamental-frequency pulsation below 500 Hz), conventional spherical harmonic beamforming encounters severe physical limitations: as kr→0 in the low-frequency band, the modal strength bn(kr) plunges rapidly toward zero, so that solving the inverse matrix becomes severely ill-posed and the condition number tends to infinity—tiny ambient noise or array mismatch is then infinitely amplified. In addition, the limited aperture of a portable device’s array (radius approximately 0.15–0.3 m) results in an abnormally broad low-frequency main lobe and high side lobes, making it difficult to clearly separate closely packed gas storage tanks, cylinders, and valves.
To address this, the solution introduces a hierarchical multi-task Transformer (HMT-SH-Transformer) sound field reconstruction model. Taking the normalized spherical harmonic feature matrices of each frequency band as input, it employs a multi-head self-attention mechanism to adaptively weight different spherical harmonic orders, precisely excluding the interference of ill-conditioned orders caused by low-frequency spherical Bessel functions; it then layers grid labels by frequency band (low frequency → low resolution, high frequency → high resolution) and fuses the outputs of the branches, simultaneously improving the convergence of low-frequency ill-posed signals and the imaging resolution of high-frequency transient impulses.
Based on the Green’s function matrix, the inverse boundary value problem of the acoustic wave equation (Helmholtz equation) is solved, precisely back-propagating the captured sound field data to the equipment surface and computing the absolute sound pressure distribution, the normal vibration velocity, and the sound intensity spatial vector. Here, normal vibration velocity is the core bridge connecting the external sound field to the internal mechanical dynamics: combined with the compressor’s multi-rigid-body dynamics and thermodynamic coupling model, the external normal vibration velocity can be deeply mapped to the internal unsteady gas forces (indicator-diagram P–V cycle parameters), inversely deriving internal thermodynamic state deterioration or disruption of hydrodynamic pressure balance (e.g., concealed gas blow-by, piston ring fracture).
The system fuses panoramic visual images with spatial acoustic energy distribution images at the pixel level to generate an intuitive panoramic acoustic mapping image. It further converts the three-dimensional radiated sound field into two-dimensional pseudo-color slices, extracts gray-level co-occurrence matrix (GLCM) texture parameters, and combines them with refined composite multiscale dispersion entropy (RCMDE) to form a hybrid feature vector. This vector is input into a deep belief network (DBN) / bidirectional gated recurrent unit (BiGRU), which automatically mines high-dimensional nonlinear feature correlations and precisely clusters healthy boundaries and mixed fault states without any manually specified physical threshold.

The acoustic signal of a reciprocating compressor is a complex mixture in which multiple physical fields interweave—aerodynamics, fluid–structure interaction, rotor dynamics, and others. Panoramic acoustic imaging technology provides in-depth analysis of the sound generation mechanisms of the three core components:
| Core component | Sound generation mechanism | Monitoring scheme |
|---|---|---|
| Intake main valve | High-frequency hydrodynamic flutter induced by high-speed gas vortex shedding, superimposed on the transient mechanical impact of valve plate collision | Panoramic acoustic imaging combined with high-order spherical harmonic features to construct a three-dimensional “time–space–frequency” health fingerprint |
| First-stage intake/exhaust tank | High-pressure airflow pulsation induced by intermittent intake and exhaust, coupled and resonating with the acoustic modes of the cavity | Spherical array observation of anomalous low-frequency radiation bright spots and energy backflow on the tank surface |
| Crankcase and cylinder block | Three broadband impact sources: piston slap, crosshead/connecting-rod clearance impact, and unbalanced inertial force resonance | Surface sound intensity vector contour map pinpoints radiated “hot spots” and traces internal mechanical fault sources in reverse |
CAUSE — Severe fouling and blockage of the oil-removal filter, mechanical seizure of the multi-stage back-pressure valve, or hydrate icing of the pipeline in extremely cold weather, all of which impose a severe physical restriction on the discharge flow cross-section.
ACOUSTIC INVERSION LOGIC — An abnormally elevated back pressure directly alters the instantaneous differential pressure before and after the discharge valve opens; the fluid impact force at the instant the valve plate is forced open is amplified exponentially, and the center frequency of the fluid–structure interaction flutter during the valve-plate open-hold period drifts noticeably upward. The absolute sound pressure in the intake/exhaust tank region rises in a nonlinear, stepwise manner, and in the holographic sound image the red high-intensity acoustic center exhibits abnormal “accumulation” and “stagnation” along the downstream direction of the discharge pipe.

CAUSE — The lubricating oil film becomes locally thinner and ultimately ruptures, causing direct dry metal-on-metal friction between the crosshead and the slideway and between the bearing and the journal, while the clearance widens sharply due to wear.
ACOUSTIC INVERSION LOGIC — The inertial impact of the heavy piston’s direction reversal causes periodic metallic knocking between the crosshead pin and the connecting rod big end, whose frequency is strongly phase-locked to the motor speed. After the knocking sound penetrates the thick housing, the low- and mid-frequency sound intensity distribution on the outer panel of the crankcase shifts from a geometrically symmetric healthy state to a marked spatial tilt and displacement toward the dry-friction side panel, forming an eccentric acoustic heat map. This provides a non-contact verification basis for precisely locating the internal mechanical looseness.
CAUSE — Insufficient lubrication, localized high temperature caused by scaling in the cooling water jacket, or carbon deposits from inhaled particulates induce dry friction between the piston and the cylinder wall, which then evolves into seizure.
ACOUSTIC INVERSION LOGIC — In a normal sound field, radiated energy is uniformly and symmetrically distributed, with high-frequency energy spots regularly concentrated in the valve opening and closing regions. Once seizure occurs, however, extremely high sound pressure level, isolated, and irregular strong radiation bright spots abruptly emerge in the faulty cylinder and along the piston trajectory in the abnormal sound field holographic slice. Based on the sound field image comparison of “uniform background → localized high-intensity bright spot,” the seizure location can be locked on rapidly, buying valuable intervention time to prevent cylinder scoring and connecting rod fracture.
Field measurement was carried out using a non-stop, no-retrofit inspection approach, completed in complex reverberant background noise above 90 dB at a gas gathering station. The measured sound pressure levels at typical locations are as follows:
| Monitoring location | Measured sound pressure level |
|---|---|
| Piston position | 111.0 dB |
| First-stage intake/exhaust tank | 108.3 dB |
| Piston pulsation compression discharge neck | 107.9 dB |
| Crankcase | 98.8 dB |
Core product specifications:
| Item | Specification |
|---|---|
| Microphone array | 64-element omnidirectional (80 dB SNR) |
| Imaging field of view | H360° × V180° |
| Sound field reconstruction resolution | 4° |
| Frequency range | 20 Hz – 20 kHz |
| Value dimension | Core capability |
|---|---|
| Coverage capability | With a 360° global field of view and strong spatial resolution, the spherical acoustic array breaks through the physical limitations of contact-type point sensors in spatial coverage and adaptability to harsh operating conditions. |
| Separation capability | Drawing on Transformer multi-label classification and a hierarchical multi-task architecture, it achieves three-dimensional “time–space–frequency” separation of high-frequency valve flutter, low-frequency tank pulsation, and broadband crankcase impact at extremely low signal-to-noise ratios. |
| Inversion capability | Through dynamic modeling and inverse solution, concealed anomalous sources are translated into in-depth state diagnostic indicators such as excessive discharge back pressure, valve plate leakage, and crosshead dry-friction wear. |
| Paradigm shift | By fusing deep neural networks, it constructs fully automatic dynamic health decision thresholds within a multi-dimensional feature space, achieving the leap from qualitative “abnormal sound perception” to quantitative “spatial source inversion.” |
Taking “spherical harmonic transform + Transformer sound field reconstruction + acoustic holographic reconstruction + state inversion” as its core technical route, the holographic sound field inspection instrument provides reciprocating compressors with a non-contact, panoramic-coverage, quantitatively inverting intelligent condition monitoring solution, fundamentally overcoming the coverage blind zones, explosion-proof wiring difficulties, and operation and maintenance costs of conventional contact-type monitoring.
Industrial deployment roadmap:
Lightweight on-device algorithm deployment—the diagnostic model is made lightweight to enable real-time on-site edge inference.
Edge computing and global monitoring network—multiple units are networked to build a station-level global acoustic monitoring network.
Digital twin integration and iteration of the O&M paradigm—acoustic data is connected to a global digital twin hub, driving the leap from “reactive post-failure repair” to “intelligent predictive condition-based maintenance.”
GroupCore Acoustic
Hear the subtle, perceive the profound.
Beijing GroupCore Acoustic Technology Co., Ltd.
For a detailed technical whitepaper or to schedule a prototype demonstration, please contact us: Mr. Zhang, +86 186 0053 8599