Variable Area Nozzle With Inclined Rotation Axis

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Solution Overview

Problem

Current throat area control systems in supersonic vehicles with afterburners face challenges in maintaining angular trailing edges while varying the nozzle throat area, leading to undesirable gaps and complex sealing requirements, making them infeasible for advanced aircraft designs.

Innovation Solution

A variable area mechanism with a movable flow area control surface that rotates about an off-body axis-of-rotation, utilizing a contoured interface surface to expand and retract without opening asymmetric gaps, and a forward flow panel with a slide interface to seal the angular trailing edges.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a mechanism rotates around an axis perpendicular to the flow to change throat area, then the flow area can be varied, but asymmetric gaps are opened requiring complicated sealing techniques

Engineering Contradiction:
Improvethroat area variation capabilityVSAvoidsealing complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent changes the rotation axis from a conventional perpendicular-to-flow orientation to an inclined orientation relative to the flow direction. This dimensional change in the rotation axis orientation allows the mechanism to vary throat area while maintaining continuous contact between the movable surface and nozzle walls, eliminating asymmetric gaps and the need for complicated sealing techniques.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The patent employs asymmetric geometry in the movable flow area control surface and nozzle configuration. The movable surface is designed with specific angular orientations and contoured interface surfaces that asymmetrically match the nozzle geometry, enabling the mechanism to rotate and seal against the nozzle walls without creating gaps, thus simplifying the sealing requirement.

Inventive Principle:
Principle #4Asymmetry

2Reliability

If edges are oriented perpendicular to the airflow, then sealing is simplified, but radar cross section increases reducing survivability

Engineering Contradiction:
Improvesealing reliabilityVSAvoidradar cross section
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent employs asymmetric geometry in the movable flow area control surface and nozzle configuration. The movable surface is designed with specific angular orientations and contoured interface surfaces that asymmetrically match the nozzle geometry, enabling the mechanism to rotate and seal against the nozzle walls without creating gaps, thus simplifying the sealing requirement.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent changes the orientation parameter of the rotation axis from perpendicular to inclined relative to the flow direction. This parameter change allows the trailing edges to be oriented at angles to the airflow, reducing radar cross section and improving survivability while the contoured interface surfaces ensure continuous sealing contact.

Inventive Principle:
Principle #35Parameter changes

3Object-affected harmful factors

If edges are oriented at an angle to the airflow to reduce radar cross section, then survivability improves, but gaps open requiring very complicated sealing techniques

Engineering Contradiction:
Improveradar cross sectionVSAvoidsealing complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The patent changes the rotation axis from a conventional perpendicular-to-flow orientation to an inclined orientation relative to the flow direction. This dimensional change in the rotation axis orientation allows the mechanism to vary throat area while maintaining continuous contact between the movable surface and nozzle walls, eliminating asymmetric gaps and the need for complicated sealing techniques.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The contoured interface surface acts as an intermediary element between the movable flow area control surface and the nozzle walls. This specially contoured surface ensures continuous contact and sealing during rotation, mediating the interaction between the angled edges and the nozzle structure, thereby eliminating gaps without requiring additional sealing mechanisms.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP2626541B1Variable area mechanism with angular trailing edges
Publication Date: 2019.10.02 THE BOEING CO
  • EP2626541B1 patent drawingFigure 1~2
  • EP2626541B1 patent drawingFigure 3
  • EP2626541B1 patent drawingFigure 4

AI summary

A variable area mechanism and methods are disclosed. A movable surface (608) comprising a contoured interface surface (618) is operable to rotate about an off-body axis-of-rotation (616) such that the movable surface (608) expands from and retracts into an angle notched surface (606).