Adjustable Aircraft Engine Wash Water Collection System

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Solution Overview

Problem

Existing systems for collecting and treating waste water from aircraft engine washing operations are not effective for engines with exhausts located in difficult-to-reach positions, such as non-perpendicular or centrally positioned exhausts, leading to inefficient waste liquid collection and potential environmental hazards due to hazardous contaminants like cadmium.

Innovation Solution

A mobile cart-based system with a versatile liquid separation device and drip pan arrangement, featuring adjustable and tiltable droplet separator frames, and extendable arms to position the collection system accurately around various engine types, including helicopters and turboprop aircraft, allowing for effective collection and treatment of waste water from aircraft turbine engines with non-standard exhaust orientations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a fixed collection system is used for waste water from engine washing, then the system structure is simple, but it cannot adapt to engines with non-standard exhaust orientations

Engineering Contradiction:
Improveadaptability to different exhaust positionsVSAvoidsystem structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The collection system employs movable and adjustable components including an extendable arm with telescopic sections, a pivotable support arm, and a tiltable separator frame. These dynamic elements allow the system to adapt its geometry to match various exhaust positions (perpendicular, angled, central) while maintaining a relatively simple base structure that can be configured as needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The collection system is designed as a universal apparatus capable of serving multiple engine types and exhaust configurations. The combination of extendable arms, pivotable support structures, and tiltable separator frames enables a single system design to handle perpendicular exhausts, angled exhausts, and centrally positioned exhausts, eliminating the need for multiple specialized collection systems.

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

2Object-affected harmful factors

If the liquid separation device is positioned far from the exhaust, then the system has easier access, but waste liquid spreads over larger area

Engineering Contradiction:
Improvewaste liquid spreadVSAvoidsystem positioning ease
Core Design Contradiction:
Object-affected harmful factorsVSEase of operation

Solution Approach 1:

The system uses an extendable arm with telescopic sections that can be adjusted to achieve the optimal distance between the liquid separation device and the exhaust outlet. This dynamic positioning capability allows the operator to minimize waste liquid spread by placing the separator as close as necessary while maintaining ease of operation through simple extension and retraction mechanisms.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The support arm is designed to be pivotable, allowing the liquid separation device to be positioned not only at varying distances from the exhaust but also at different angular orientations. This adds a rotational dimension to the positioning capability, enabling the system to adapt to exhausts at various angles while maintaining close proximity for effective waste liquid collection.

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

3Volume of moving object

If the collection system is made compact, then the device size is reduced, but the range of adjustable positions is limited

Engineering Contradiction:
Improvesystem sizeVSAvoidposition adjustment range
Core Design Contradiction:
Volume of moving objectVSAdaptability or versatility

Solution Approach 1:

The extendable arm is divided into multiple telescopic sections that can be independently extended or retracted. This segmentation allows the system to maintain a compact storage size when not in use, while providing a large adjustment range when deployed. Each section can be adjusted to achieve the required length and position without requiring the entire system to be oversized.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The telescopic arm sections are nested within each other in a concentric arrangement, allowing the compact storage configuration where the extended portions are retracted into the inner sections. This nesting principle enables the system to achieve both compact size for transport and storage, and extended reach for positioning the liquid separation device at various distances from different exhaust configurations.

Inventive Principle:
Principle #7Nested doll (Nesting)

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 enables efficient collection and treatment of waste water from aircraft engines with challenging exhaust positions, reducing environmental impact by containing hazardous materials and improving operational efficiency by minimizing waste liquid spread and facilitating flexible treatment based on varying wash liquid compositions.

Implementation Method 1

the liquid separation device causes the liquid to condense in the drip pan

Methodology Applied
Scientific EffectInertial impaction:

Implementation Method 2

the liquid separation device causes the liquid to condense in the drip pan

Methodology Applied
Scientific EffectGravity: Gravitation

Data Source

PatentEP2236221B1Device and method for collecting waste water from turbine engine washing
Publication Date: 2011.09.07 GTE TURBINE EFFICIENCY SWEDEN AB
  • EP2236221B1 patent drawingFigure 1
  • EP2236221B1 patent drawingFigure 2
  • EP2236221B1 patent drawingFigure 3a

AI summary

The invention relates to an apparatus for collecting waste water from cleaning operations performed on aircraft turbine engines. It comprises a frame structure (41). On the frame a support arm (44) is pivotally mounted. An actuator arm (46) is arranged to raise and lower the support arm between an essentially horizontal transport position to an operative position forming an angle in the range of more than 0° to 90° or less with respect to the horizontal. There is further a liquid separation device (47) pivotally attached to the support arm so as to be movable around both a horizontal and a vertical axis.