Intake Manifold Air Bypass Control for Low-Load Temperature Stability

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Solution Overview

Problem

Internal combustion engines designed for alternative fuels face challenges with low intake manifold temperatures at sub-maximum loads, leading to reduced emissions performance and limited alternative fuel substitution, which existing systems like the '858 patent fail to adequately address.

Innovation Solution

An intake manifold temperature system with a compressor bypass valve and controller that adjusts air flow through an air cooler based on ambient and manifold conditions to maintain optimal intake manifold temperature, using sensors and an electronic control module to actuate the bypass valve.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If air flow through the air cooler is increased to cool the intake air, then the intake air temperature decreases, but the intake manifold temperature becomes too low at sub-maximum loads, reducing emissions performance and alternative fuel combustion efficiency

Engineering Contradiction:
Improveintake air temperatureVSAvoidemissions performance
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The air flow path is segmented into two separate paths: one through the air cooler for heat dissipation, and another through the bypass passage for temperature maintenance. The bypass valve controls the distribution of air between these two paths, allowing independent optimization of cooling efficiency and temperature maintenance.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bypass valve dynamically adjusts the proportion of air flow through the bypass passage versus the air cooler based on real-time operating conditions. This dynamic control enables the system to adapt to varying load conditions, maintaining optimal intake manifold temperature across different operating regimes.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If a bypass passage is added to allow air to bypass the air cooler, then the system gains temperature control flexibility, but the device complexity increases

Engineering Contradiction:
Improvetemperature control flexibilityVSAvoidsystem structure
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The bypass valve serves multiple functions: it controls the proportion of air bypassing the cooler, regulates intake manifold temperature, and adapts to different operating conditions. This multi-functionality is achieved through a single integrated component rather than multiple separate systems.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The bypass valve acts as an intermediary component that mediates between the compressor outlet and the intake manifold, controlling the mixing of cooled and bypassed air. This intermediary element enables precise temperature control without requiring complex multi-component systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 system maintains optimal intake manifold temperature, enhancing engine performance, efficiency, and emissions control by adapting air flow to compensate for low ambient or engine loads, preventing overheating and ensuring stable combustion.

Implementation Method 1

an air cooler connected downstream of the compressor

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

an electronically-controlled bypass valve connected downstream of the compressor, the bypass valve configured to control a proportion of air flow through the bypass passage and through the air cooler

Methodology Applied
Scientific EffectFluid flow control: Valve

Implementation Method 3

a compressor, an air cooler connected downstream of the compressor

Methodology Applied
Scientific EffectCompression: Compression

Data Source

PatentUS12516622B1Coolant system bypass for engine
Publication Date: 2026.01.06 CATERPILLAR INC
  • US12516622B1 patent drawing
  • US12516622B1 patent drawing
  • US12516622B1 patent drawing

AI summary

An intake manifold temperature system including an internal combustion engine, an intake manifold connected to the internal combustion engine, an air supply system configured to supply compressed air to the internal combustion engine, an ambient condition sensor, an air system sensor, a manifold condition sensor, and a controller. The air supply system may include a compressor, an air cooler connected downstream of the compressor, a bypass passage connected downstream of the compressor to provide compressed air to the intake manifold, the air having bypassed the air cooler, and an electronically-controlled bypass valve connected downstream of the compressor, the bypass valve configured to control a proportion of air flow through the bypass passage and through the air cooler. The controller may be configured to actuate the bypass valve based on signals and a desired intake manifold temperature.