Angled Feeder Conduit Discharge Manifold to Reduce Vibration

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Solution Overview

Problem

In commercial HVAC systems with multiple compressors in parallel configuration, existing discharge gas manifolds experience significant vibration due to refrigerant gas flow, necessitating additional bracketing to stabilize them, which increases system costs.

Innovation Solution

A discharge gas manifold design featuring a main conduit with angled end and intermediate feeder conduits that reduce turbulent gas flow by aligning refrigerant gas entry with the main conduit axis, minimizing the need for extra bracketing through optimized conduit geometry.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a common discharge line and discharge gas manifold are used to connect multiple compressors, then the HVAC system can efficiently circulate refrigerant gas, but significant vibration occurs due to turbulent gas flow requiring extra bracketing

Engineering Contradiction:
Improverefrigerant circulation efficiencyVSAvoidvibration
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The feeder conduits are designed with curved portions that form angles between 0°-60° with the main conduit axis, creating smooth transitions that guide refrigerant gas flow. This curvature eliminates sharp 90° angles, reducing turbulence and vibration while maintaining efficient refrigerant circulation through the discharge manifold

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The invention changes the flow direction parameters by angling the feeder conduits at 0°-60° relative to the main conduit axis instead of using perpendicular connections. This parameter modification optimizes gas flow characteristics, reducing turbulent flow and associated vibration in the discharge manifold

Inventive Principle:
Principle #35Parameter changes

2Object-affected harmful factors

If extra bracketing is added to stabilize the discharge gas manifold against vibration, then vibration is reduced, but system cost increases

Engineering Contradiction:
ImprovevibrationVSAvoidsystem cost
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The invention converts the potentially harmful turbulent flow into beneficial laminar flow by designing feeder conduits with smooth curved transitions at 0°-60° angles. This design transformation eliminates the need for additional vibration-reducing bracketing, reducing system complexity and cost while maintaining vibration control

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The discharge manifold design is self-stabilizing through its geometric configuration. The angled feeder conduits inherently reduce turbulence and vibration, making the system self-regulating without requiring external bracketing support, thereby reducing overall system complexity and installation cost

Inventive Principle:
Principle #25Self-service

3Ease of operation

If feeder conduits are connected at 90° angles to the main conduit, then installation is simplified, but turbulent flow and vibration increase

Engineering Contradiction:
Improveinstallation simplicityVSAvoidturbulent flow
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The feeder conduits incorporate curved portions that transition smoothly into the main conduit at angles between 0°-60°, replacing sharp 90° connections. This curvature simplifies the flow path while reducing turbulence, maintaining ease of installation through standardized angular configurations

Inventive Principle:
Principle #14Spheroidality (Curvature)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The design reduces vibration and eliminates the need for extra bracketing, thereby lowering system costs and enhancing operational stability by minimizing turbulent flow and associated vibrations.

Implementation Method 1

The intermediate feeder conduit includes an intermediate first straight portion that forms an angle with the longitudinal axis of the main conduit... reduces the vibration levels of the refrigerant gas entering the main conduit

Methodology Applied
Scientific EffectTurbulent flow: Turbulence

Data Source

PatentUS9869497B2Discharge manifold for use with multiple compressors
Publication Date: 2018.01.16 CARRIER CORP
  • US9869497B2 patent drawing
  • US9869497B2 patent drawing
  • US9869497B2 patent drawing

AI summary

A discharge gas manifold having a main conduit, an end feeder conduit, and at least one intermediate feeder conduit, wherein the at least one intermediate feeder conduit contains a portion, adjacent to the main conduit, that forms an angle between 0°-60° with the axis of the main conduit.