Rotor Blade Spar End Cap Drainage via Pressure Differential

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Solution Overview

Problem

Water accumulation within the rotor blade spar of rotary wing aircrafts poses a challenge due to manufacturing processes, temperature changes, and storage conditions, leading to potential damage when attempting to remove trapped water.

Innovation Solution

A rotor blade spar design featuring an end cap with fluidly coupled ports and a port sealing system that utilizes a pressure differential, either through air or vacuum, to remove water without damaging the spar, incorporating one-way valves and removable plugs for efficient water removal.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the end cap is sealed to prevent water entry, then water protection is improved, but water removal becomes difficult and may require end cap replacement

Engineering Contradiction:
Improvewater protectionVSAvoidwater removal
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The end cap is segmented into a sealed portion and a drain portion with separate functions. The sealed portion maintains water protection while the drain portion provides water removal capability through drain holes and channels, resolving the contradiction between sealing and drainage

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A removable plug acts as an intermediary element that blocks drain holes during normal operation to maintain sealing, but can be removed to enable water removal. This mediator allows the system to switch between sealed and draining states without compromising either function

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If the end cap is removed to remove water, then water removal is enabled, but damage to the blade spar may occur

Engineering Contradiction:
Improvewater removalVSAvoidspar integrity
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

The water removal function is extracted from the main end cap structure and placed in a separate drain portion. This allows water to be removed through the drain holes and channels without requiring removal of the main end cap, thus protecting the blade spar from potential damage

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The removable plug serves as an intermediary that enables water removal through the drain portion without compromising the sealed portion's attachment to the blade spar, avoiding the need to remove or damage the main end cap structure

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If fastener holes are created during fabrication, then assembly is enabled, but water entry pathways are created

Engineering Contradiction:
Improveassembly capabilityVSAvoidwater entry
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The fastener holes that create water entry pathways are converted into beneficial drainage pathways. The drain holes are positioned to utilize the same hole locations for water removal, transforming the harmful effect into a useful drainage function

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The removable plug acts as a mediator that blocks water entry through fastener holes during normal operation, while still allowing the holes to serve their structural assembly function. When removed, the same holes facilitate water drainage

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

Minimizes water accumulation within the rotor blade, reduces manufacturing costs, and prevents damage to the spar by allowing for safe and efficient removal of water without replacing the end cap.

Implementation Method 1

The first port is connectable to an external device configured to generate a pressure differential between the interior and the exterior sufficient to create an airflow through the first and second ports which removes a liquid disposed in the housing

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Implementation Method 2

the sealing system includes a one way valve configured to allow fluid to flow through the first port in a first direction

Methodology Applied
Scientific EffectOne-way flow control: Valve

Data Source

PatentUS10293930B2Spar end cap with drain hole provisions
Publication Date: 2019.05.21 SIKORSKY AIRCRAFT CORP
  • US10293930B2 patent drawing
  • US10293930B2 patent drawing
  • US10293930B2 patent drawing

AI summary

A rotor blade spar for use in a rotor blade is provided comprising a housing defining an interior and having an open end. An end cap is affixed to and sealed on the open end to seal the interior from an exterior outside of the housing. The end cap includes a first port and a second port fluidly coupling the interior to the exterior. A port sealing system closes the first and second ports. The first port is connectable to an external device configured to generate a pressure differential between the interior and the exterior sufficient to create an airflow through the first and second ports which removes a liquid disposed in the housing through one of the first and second ports.