Hoop Ejector Airflow Induction for TAT Probe Radiation Error Reduction

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Solution Overview

Problem

Total air temperature (TAT) probes on aircraft are susceptible to radiation errors when stationary and exposed to direct sunlight, leading to inaccurate temperature readings due to increased temperature within the probe.

Innovation Solution

A hoop ejector with angled holes is integrated into the TAT probe, creating a pressure differential to induce airflow through the probe, reducing solar radiation effects and maintaining accurate readings by aspirating air and reducing pressure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If the TAT probe is stationary and exposed to direct sunlight, then the temperature of the probe and air inside increases, but this causes radiation error and inaccurate temperature readings

Engineering Contradiction:
Improvetemperature reading accuracyVSAvoidsolar radiation error
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The system performs preliminary action by using the hoop ejector to induce airflow through the TAT probe before radiation error significantly affects measurements. The compressed air supply activates the hoop ejector proactively to maintain accurate readings during sunlight exposure, preventing temperature distortion rather than correcting it afterward.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention applies pneumatic principles by using compressed air supplied to the hoop ejector to create airflow induction. The hoop ejector utilizes pneumatic pressure differential to draw air through the probe, replacing natural convection that causes radiation error with controlled pneumatic flow that maintains measurement accuracy.

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Weight of stationary object

If the TAT probe is designed to be smaller and lighter, then the device complexity is reduced, but it may compromise the ability to maintain accurate readings under radiation exposure

Engineering Contradiction:
Improveprobe weightVSAvoidreading accuracy under radiation
Core Design Contradiction:
Weight of stationary objectVSReliability

Solution Approach 1:

The hoop ejector serves multiple functions: it induces airflow through the probe for accurate temperature measurement, and simultaneously cools the probe structure to prevent radiation-induced heating. This multi-functionality allows the probe to maintain reliability and accuracy under radiation exposure without requiring additional separate cooling systems that would increase weight.

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

3Measurement precision

If airflow is induced through the probe using a hoop ejector, then solar radiation effects are reduced, but this requires additional components and compressed air supply

Engineering Contradiction:
Improvetemperature measurement accuracyVSAvoidprobe structure complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The hoop ejector acts as an intermediary device between the compressed air supply and the TAT probe. It translates compressed air pressure into controlled airflow induction through the probe, mediating the interaction between the external air supply system and the sensitive temperature measurement components, thereby improving measurement precision without directly complicating the probe's internal structure.

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

The hoop ejector effectively reduces solar radiation errors by up to 95%, ensuring more accurate temperature readings without altering the internal geometry of the TAT probe, allowing it to be smaller and lighter.

Implementation Method 1

A hoop ejector with angled holes is integrated into the TAT probe, creating a pressure differential to induce airflow through the probe

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Implementation Method 2

aspirating air and reducing pressure

Methodology Applied
Scientific EffectAir aspiration: Suction

Implementation Method 3

The plurality of holes extend from an outer diameter of the inner wall of the hoop to an inner diameter of the inner wall of the hoop at an angle... The holes are configured to speed up the velocity of air as air passes through the holes and lower the pressure of air as air passes through the holes

Methodology Applied
Scientific EffectVenturi effect: Venturi Effect

Data Source

PatentEP3462154B1Sensor aspiration utilizing hoop airflow induction
Publication Date: 2020.11.04 ROSEMOUNT AEROSPACE INC
  • EP3462154B1 patent drawingFigure 1A
  • EP3462154B1 patent drawingFigure 1B
  • EP3462154B1 patent drawingFigure 2A

AI summary

A probe (10) includes a housing (14) defining a flow passage (24) for a first fluid and having an entrance port (20) and an exit port (30), a sensor configured to sense a parameter of the first fluid and positioned within the flow passage (24), and a hoop ejector (12) connected externally to the housing (14) such that a channel (54) of the hoop ejector (12) surrounds the exit port (30). The hoop ejector (12) has a plurality of holes (58) configured to port a second fluid from the channel (54) such that the first fluid is aspirated from the flow passage (24) and out through the exit port (30).