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{{DISPLAYTITLE:Pitot Tube}}
[[File:Pitot_tube_airplane.svg|thumb|right|Pitot tube mounted on aircraft]]


A '''pitot tube''' (/ˈpiːtoʊ/ PEE-toh) measures fluid flow velocity. It was invented by French engineer Henri Pitot during work with aqueducts in 1732 and later adapted for modern aviation and industry. It is widely used in aircraft, boats, and industrial applications.
'''Pitot Tube'''


== Theory of Operation ==
[[File:Pitot_Tube.jpg|thumb|right|Aircraft use pitot tubes to measure airspeed. This example, from an Airbus A380, combines a pitot tube (right) with a static port and an angle-of-attack vane (left). Air-flow is right to left.]]
[[File:Pitot_Tube2.jpg|thumb|right|A pitot-static tube connected to a manometer]]


The pitot tube is a device for measuring fluid velocity by converting the kinetic energy in a fluid flow into potential energy. It measures the difference between stagnation pressure (measured in the pitot opening facing the flow) and static pressure.
The Pitot tube, a device for measuring fluid flow velocity, was invented by French engineer Henri Pitot in the early 18th century and refined by Henry Darcy in the mid-19th century. It works by measuring the difference between stagnation (total) and static pressure within a fluid, allowing for the calculation of flow velocity.


'''Basic principle:'''
==Here's a more detailed historical account:==
: Stagnation pressure = Static pressure + Dynamic pressure


In aviation, the difference between the stagnation and static pressure is used to compute the dynamic pressure, which in turn is used to determine airspeed.
===Early Development (1732):===
Henri Pitot, a French engineer, developed the original Pitot tube in 1732 to measure the speed of water flow in rivers and canals.


== Use in Aircraft ==
===Purpose of the Invention:===
Pitot's invention aimed to determine the velocity of fluids by measuring the pressure exerted by the fluid's kinetic energy.


Aircraft use pitot tubes to measure airspeed. These are typically mounted on the wings or nose, oriented directly into the airflow. The measured pressure difference is translated into airspeed through mechanical or electronic systems.
===Mechanism:===
The Pitot tube works by converting the kinetic energy of the fluid flow into potential energy, which is then measured as a pressure difference.


== Aircraft and Accidents ==
===Modern Form (1858):===
In 1858, French scientist Henry Darcy modified Pitot's design, creating the modern form of the Pitot tube, enhancing its accuracy and applicability.


The pitot-static system (which includes the pitot tube) is vital to flight safety. Blockages or failures can lead to erroneous airspeed readings.
===Key Principle:===
The Pitot tube measures the stagnation pressure (total pressure) at the front of the tube and the static pressure at the sides, with the difference between these two pressures representing the dynamic pressure, which can be used to calculate the fluid velocity.


'''Notable incidents:'''
==Applications:==
* Austral Líneas Aéreas Flight 2553
Pitot tubes are widely used in various fields, including:
* Northwest Airlines Flight 6231
* '''Aviation''': Determining the airspeed of aircraft.
* Birgenair Flight 301
* '''Hydraulics''': Measuring the water speed of boats.
* Air France Flight 447
* '''Industry''': Measuring the flow velocity of liquids, air, and gases.
* In 2008, Air Caraïbes reported pitot tube icing issues on its A330s.
 
For more information, see: [[Pitot-static system]]
 
== References ==
* [https://en.wikipedia.org/wiki/Pitot_tube Wikipedia – Pitot Tube]
* [https://skybrary.aero/articles/pitot-static-system SKYbrary – Pitot-Static System]


==Pitot-static tube:==
A variation of the Pitot tube, called a Pitot-static tube, measures both stagnation and static pressures, allowing for more accurate velocity calculations.
   

Latest revision as of 10:02, 5 April 2025

Pitot Tube

Aircraft use pitot tubes to measure airspeed. This example, from an Airbus A380, combines a pitot tube (right) with a static port and an angle-of-attack vane (left). Air-flow is right to left.
A pitot-static tube connected to a manometer

The Pitot tube, a device for measuring fluid flow velocity, was invented by French engineer Henri Pitot in the early 18th century and refined by Henry Darcy in the mid-19th century. It works by measuring the difference between stagnation (total) and static pressure within a fluid, allowing for the calculation of flow velocity.

Here's a more detailed historical account:

Early Development (1732):

Henri Pitot, a French engineer, developed the original Pitot tube in 1732 to measure the speed of water flow in rivers and canals.

Purpose of the Invention:

Pitot's invention aimed to determine the velocity of fluids by measuring the pressure exerted by the fluid's kinetic energy.

Mechanism:

The Pitot tube works by converting the kinetic energy of the fluid flow into potential energy, which is then measured as a pressure difference.

Modern Form (1858):

In 1858, French scientist Henry Darcy modified Pitot's design, creating the modern form of the Pitot tube, enhancing its accuracy and applicability.

Key Principle:

The Pitot tube measures the stagnation pressure (total pressure) at the front of the tube and the static pressure at the sides, with the difference between these two pressures representing the dynamic pressure, which can be used to calculate the fluid velocity.

Applications:

Pitot tubes are widely used in various fields, including:

  • Aviation: Determining the airspeed of aircraft.
  • Hydraulics: Measuring the water speed of boats.
  • Industry: Measuring the flow velocity of liquids, air, and gases.

Pitot-static tube:

A variation of the Pitot tube, called a Pitot-static tube, measures both stagnation and static pressures, allowing for more accurate velocity calculations.