Reed Valve Lubricant Delivery for Emergency Gearbox Backup Flow

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Solution Overview

Problem

Rotorcraft gearboxes face premature failure and safety risks due to excessive heat generation and inadequate lubrication, particularly when primary lubrication systems fail, leading to increased weight and complexity with dual lubrication systems.

Innovation Solution

A fluid delivery device that can seamlessly switch between primary and secondary lubricant sources, utilizing a reed valve mechanism to redirect lubricant flow from a secondary source during emergencies, thereby reducing friction and extending operational time without increasing weight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a secondary emergency lubrication system is added to operate when the primary lubrication system fails, then the reliability of lubrication is improved, but the weight of the rotorcraft increases

Engineering Contradiction:
Improvelubrication system reliabilityVSAvoidrotorcraft weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent combines the primary and secondary lubrication systems into a single integrated fluid delivery device. The body contains both a primary inflow passage and a secondary inflow passage, with a common outflow passage that serves both systems. This merging eliminates the need for separate delivery mechanisms, reducing overall weight while maintaining dual-system reliability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fluid delivery device is designed with multi-functionality, where a single device can deliver lubricant from either the primary source or secondary source (or both simultaneously) through a common outflow passage. The reed valve mechanism enables the device to automatically switch between functions based on operating conditions, providing universal lubrication delivery capability without requiring separate dedicated systems.

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

2Duration of action of moving object

If a secondary emergency lubrication system is added to operate when the primary lubrication system fails, then the operational duration is improved, but the device complexity increases

Engineering Contradiction:
Improveoperational durationVSAvoidlubrication system complexity
Core Design Contradiction:
Duration of action of moving objectVSDevice complexity

Solution Approach 1:

The patent merges the control mechanisms for primary and secondary lubrication into a single reed valve-based automatic switching system. The reed valve responds to pressure differential changes to automatically route lubricant flow between primary and secondary sources, eliminating the need for complex electronic sensors, controllers, or manual switching mechanisms that would increase device complexity.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fluid delivery device employs a self-regulating mechanism where the reed valve automatically switches between primary and secondary lubrication sources based on pressure differential conditions without external control. The system monitors its own state through the pressure differential across the reed valve and autonomously adjusts the flow path, extending operational duration while maintaining simple device architecture.

Inventive Principle:
Principle #25Self-service

3Reliability

If separate primary and secondary jets are used for dual lubrication sources, then the lubrication reliability is improved, but the weight increases

Engineering Contradiction:
Improvedual lubrication reliabilityVSAvoidjet system weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent merges the primary and secondary jet functions into a single common outflow passage that serves both lubrication sources. Instead of having separate delivery passages and control mechanisms for primary and secondary jets, the invention uses one shared passage with a reed valve that directs flow from either source, significantly reducing the weight of the jet system while maintaining the ability to deliver lubricant from both sources reliably.

Inventive Principle:
Principle #5Merging (Combining)

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 device effectively delivers supplemental lubricant during reduced pressure conditions, reducing friction and extending rotorcraft operational time while minimizing weight and complexity.

Implementation Method 1

A fluid delivery device that can seamlessly switch between primary and secondary lubricant sources, utilizing a reed valve mechanism to redirect lubricant flow from a secondary source during emergencies

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentUS11077936B2Fluid delivery device
Publication Date: 2021.08.03 BELL HELICOPTER TEXTRON INC
  • US11077936B2 patent drawing
  • US11077936B2 patent drawing
  • US11077936B2 patent drawing

AI summary

A fluid delivery device includes a body and a reed. The body has a primary inflow passage, a secondary inflow passage, and an outflow passage. The reed is disposed at least partially within the body. The reed is configured to move to a first position when a fluid flows from the primary inflow passage and move to a second position when the fluid flows from the secondary inflow passage.