Helicopter Air Intake Deflector for Yaw-Dependent Cooling

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Solution Overview

Problem

Helicopter airflow variations due to yaw angle affect thermodynamic efficiency and transmission cooling, leading to inconsistent airflow and increased turbulence, which impairs engine performance and cooling efficiency over a wide attitude range.

Innovation Solution

The design incorporates a dual airflow system with deflecting and guide means to separate first and second airflows, ensuring constant airflow to the engine and transmission cooling system, reducing turbulence and maintaining efficiency across varying yaw angles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the helicopter operates over a wide yaw angle range, then the helicopter's maneuverability and operational flexibility are improved, but the airflow to the engine and transmission becomes inconsistent and turbulent, degrading thermodynamic efficiency and cooling performance

Engineering Contradiction:
Improveyaw angle rangeVSAvoidairflow consistency
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The air intake system incorporates movable deflecting means that dynamically adjust their position in response to varying yaw angles. This dynamic adaptation allows the intake to maintain optimal airflow alignment with the fuselage centerline across different flight attitudes, ensuring consistent airflow to the engine and transmission while preserving wide maneuverability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system employs feedback mechanisms where sensors detect the actual yaw angle and feed this information to control the deflecting means. This closed-loop control ensures that the air intake automatically compensates for yaw angle variations, maintaining stable airflow conditions regardless of the helicopter's attitude changes

Inventive Principle:
Principle #23Feedback

2Productivity

If separate inlets are provided for engine air intake and transmission cooling air intake, then the airflow requirements of both systems can be independently optimized, but the device complexity and manufacturing cost increase

Engineering Contradiction:
Improveairflow optimizationVSAvoidinlet structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The air intake system is segmented into distinct flow paths within a unified structure. The deflecting means separates the incoming airflow into different streams that can be directed to the engine and transmission independently, allowing each system to receive optimized airflow while maintaining a relatively simple integrated inlet structure

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The air intake system is designed as a multi-functional unit that serves both the engine and transmission simultaneously. The deflecting means provides universal functionality by being able to direct airflow to either system or both systems concurrently, reducing the need for separate dedicated inlets while maintaining independent optimization capability

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

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

This solution maintains consistent airflow and reduces turbulence, enhancing engine thermodynamic efficiency and transmission cooling, thereby improving overall helicopter performance and reducing the risk of overheating across a wide range of yaw angles.

Implementation Method 1

deflecting means interacting, in use, with an airflow F outside helicopter (1) to divide the airflow into a first and second airflow

Methodology Applied
Scientific EffectFlow division:

Implementation Method 2

guide means for guiding the first airflow along a first path P extending from the deflecting means to inlet (21)

Methodology Applied
Scientific EffectFlow guidance:

Implementation Method 3

guiding the second airflow along two second paths Q separate from path P and extending from the deflecting means to inlets (22)

Methodology Applied
Scientific EffectFlow guidance:

Data Source

PatentUS8113461B2Helicopter
Publication Date: 2012.02.14 LEONARDO FINMECCANICA SPA
  • US8113461B2 patent drawing
  • US8113461B2 patent drawing
  • US8113461B2 patent drawing

AI summary

A helicopter comprising a drive having an air intake conduit, a main rotor connected functionally to the drive and a transmission interposed functionally between the main rotor and the drive and housed in a housing. The helicopter further comprises at least one air intake having a first inlet fluidly connected to the intake conduit, at least one second inlet fluidly connected to the housing and deflecting means interacting, in use, with an airflow to divide the airflow into a first and a second airflow. The air intake also has guide means for guiding the first airflow along a first path extending from the deflecting means to the first inlet, and for guiding the second airflow along a second path separate from the first path and extending from the deflecting means to the second inlet.