Nacelle Inlet Acoustic Panel Layout for Compact Ice Protection

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Solution Overview

Problem

Existing nacelle designs face challenges with volume constraints and inefficiencies due to the integration of pneumatic anti-ice systems, which limit acoustic panel length and increase complexity and cost, while pneumatic anti-ice systems require thermal insulation elements, further reducing available space and efficiency.

Innovation Solution

A compact nacelle inlet assembly integrates a liquid-based fluid ice protection system (FIPS) that positions the plenum back wall forward, allowing the acoustic panel to extend closer to the leading edge, eliminating bulkheads and thermal insulation, and enhancing laminar flow by using a seamless metallic coating.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a pneumatic anti-ice system is integrated into the inlet section, then ice protection is provided, but device complexity and power demand increase

Engineering Contradiction:
Improveice protectionVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces the pneumatic anti-ice system (mechanical/gas-based) with a fluid ice protection system that uses liquid or gel状 anti-ice fluid applied through a coating or film on the inlet surface. This substitution reduces system complexity by eliminating the need for heated air ducts, bulkheads, and thermal insulation elements while maintaining ice protection functionality.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent transitions from a pneumatic system (using pressurized gas) to a hydraulic or liquid-based system where anti-ice fluid is delivered through a fluid delivery system. This allows for a more compact design without requiring the thermal insulation infrastructure of pneumatic systems, thereby reducing overall device complexity.

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Reliability

If a pneumatic anti-ice system with thermal insulation elements is integrated into the inlet section, then ice protection is provided, but available volume and surface area are reduced

Engineering Contradiction:
Improveice protectionVSAvoidavailable volume
Core Design Contradiction:
ReliabilityVSVolume of stationary object

Solution Approach 1:

The patent extracts and removes the thermal insulation elements (bulkheads, insulation layers) from the inlet section design. By eliminating these components, the available volume and surface area for other systems (such as acoustic panels) are maximized while the fluid ice protection system maintains ice protection through a thinner, more space-efficient configuration.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent employs a thin film or coating-based fluid delivery system instead of bulky thermal insulation structures. This thin-film approach provides the necessary ice protection functionality while occupying minimal space, thereby preserving available volume for acoustic treatment and other inlet systems.

Inventive Principle:
Principle #30Flexible shells and thin films

3Loss of energy

If the inlet section is shortened to improve fuel efficiency, then fuel burn is reduced, but acoustic panel length and available space are reduced

Engineering Contradiction:
Improvefuel burnVSAvoidacoustic panel length
Core Design Contradiction:
Loss of energyVSLength of stationary object

Solution Approach 1:

The patent changes the state or configuration of the anti-ice system from a space-consuming pneumatic system to a compact fluid-based system. This parameter change in the anti-ice system configuration allows the acoustic panel to extend further along the shortened inlet section, compensating for the reduced overall length while maintaining noise reduction effectiveness.

Inventive Principle:
Principle #35Parameter changes

4Reliability

If a pneumatic anti-ice system is used, then ice protection is provided, but manufacturing cost and complexity increase

Engineering Contradiction:
Improveice protectionVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent replaces the complex pneumatic anti-ice system with a simpler fluid-based system that uses liquid or gel状 anti-ice fluid applied through a coating or film. This substitution reduces manufacturing complexity and cost by eliminating the need for heated air ducts, bulkheads, and thermal insulation elements, while maintaining reliable ice protection.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS12539976B2Nacelle inlet assembly with acoustic panel
Publication Date: 2026.02.03 THE BOEING CO
  • US12539976B2 patent drawing
  • US12539976B2 patent drawing
  • US12539976B2 patent drawing

AI summary

An inlet assembly for a nacelle includes an inlet cowl and a plenum back wall of a fluid ice protection system (FIPS). The inlet cowl extends a length from a front end of the inlet cowl to a rear end of the inlet cowl. The inlet cowl includes a lipskin that defines a leading edge of the inlet cowl at the front end, and an acoustic panel coupled to the lipskin at an interface along an inner side of the inlet cowl. A seam is defined between the acoustic panel and the lipskin. The plenum back wall is affixed to an interior surface of the lipskin to define a plenum between the interior surface and a front surface of the plenum back wall. The plenum receives an anti-ice liquid. The plenum back wall is disposed in front of the seam along the length of the inlet cowl.