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4results about How to "Guaranteed Performance Requirements" patented technology

A membrane wall structure of a waste incinerator

The utility model belongs to garbage incinerator membrane type wall screen structure in the technical field of garbage incinerator. Membrane type wall pipe screen includes many pipe fittings (6), adjacent pipe fittings (6) welding connection, every pipe fitting (6) includes first pipe fitting subassembly (1), second pipe fitting subassembly (2), third pipe fitting subassembly (3), first tee (4), second tee (5), first tee (4) is connected between first pipe fitting subassembly (1) and second pipe fitting subassembly (2), second tee (5) is connected between second pipe fitting subassembly (2) and third pipe fitting subassembly (3). The garbage incinerator membrane type wall screen structure of the utility model, simple structure can reduce the labor intensity, improve the assembly efficiency.
Owner:ANHUI CONCH KAWASAKI ENERGY CONSERVATION EQUIPMENT MANUFACTURING CO LTD

A tidal computing power scheduling system and method for a heterogeneous computing power resource pool

This application relates to the technical field of artificial intelligence computing power, and in particular to a tidal computing power scheduling system and method for heterogeneous computing power resource pools. It includes: a computing power request parsing module, used to receive and parse computing power service requests to determine the computing power requirements corresponding to the tasks; a resource pool management module, used to manage the computing power resource pool; a priority scheduling module, used to obtain request information corresponding to the computing power service requests to determine task priorities, and configure corresponding resource allocation strategies based on task priorities; a node filtering module, used to filter computing nodes in the computing power resource pool according to computing power requirements; and a tidal dynamic scaling scheduling module, used to calculate the tidal period determination results and the load data of the computing power resource pool, and dynamically generate tidal dynamic actions in conjunction with a preset multi-level load threshold pipeline for tidal decision adjustment. This application achieves efficient utilization and intelligent elastic scaling of computing power resources.
Owner:WASU DIGITAL TV MEDIA GRP CO LTD +1

Compressor two-stage expansion muffler

ActiveCN224339137UGuaranteed Performance RequirementsGuaranteed Noise Cancellation PerformancePositive displacement pump componentsPositive-displacement liquid enginesInterior spaceRefrigerant
This utility model discloses a two-stage expansion muffler for a compressor, belonging to the field of compressor technology. It includes a muffler cavity with an inlet pipe outside the cavity. A flow-dividing cavity is located inside the cavity, corresponding to the output end of the inlet pipe. A flow-dividing hole is provided on the cavity wall of the flow-dividing cavity, which connects to the inlet pipe. The diameters of both the flow-dividing hole and the inlet pipe are smaller than the internal space dimensions of the flow-dividing cavity. The flow-dividing cavity, connected to the inlet pipe, provides semi-directional flow guidance for the refrigerant entering the muffler. The internal space dimensions of the flow-dividing cavity are larger than the cross-sectional area of ​​the inlet pipe's hole but smaller than the internal volume of the muffler cavity. The refrigerant enters from the inlet pipe into the flow-dividing cavity and then from the flow-dividing cavity into the muffler cavity, forming a two-stage expansion impedance muffler structure that filters noise.
Owner:JIAXIPERA COMPRESSOR

Engine rotor blade tip multi-parameter design method and system, and related device

PendingCN122113288AEnsure safe operationGuaranteed Performance RequirementsGeometric CADSustainable transportationMachineSafe operation
The application provides an engine rotor blade tip multi-parameter design method, system and related device, relates to the rotor blade tip design technical field, and the design method comprises the following steps: S1, calculating a blade tip deformation amount, and drawing a blade tip thermal profile; S2, according to the blade tip thermal profile and the blade tip deformation amount, a blade tip final shape is drawn; S3, the deformation amount of a machine case is calculated, and a machine case cold profile is drawn; and S4, according to the machine case cold profile and the blade tip final shape, the cold installation gap of the blade tip and the machine case is determined. The application can ensure the safe operation of the engine under the condition of ensuring the performance requirements of the engine, and greatly improves the rationality of the gap design.
Owner:AECC COMML AIRCRAFT ENGINE CO LTD