Overview of Resistive Type Fuel Qty. Measuring Systems

Overview of Resistive Type Fuel Qty. Measuring System

 

The Resistive Type Fuel Quantity measuring system utilizes a variable resistive element in order to vary a precise electrical DC voltage based on the quantity of fuel in the fuel tank. The varying electrical signal, in turn, is used to drive the pointer on a fuel quantity indicator in a manner which is proportional to the amount of fuel in the tank, thereby visibly indicating remaining fuel quantity to the pilot.

The typical components in this type of system include the following:

a) Regulated DC Power Source
b) Tank Unit (Fuel Qty Sender, Fuel Probe)
c)  Indicator

Stay tuned to the TGH Aviation for additional information pertaining to these components

 

 

Stay tuned for upcoming Blogs

General Overview Fuel Measuring Systems

General Overview Fuel Flow Systems

 

The purpose of the Fuel Quantity Measuring System is to provide the pilot with a visual representation of the amount of useable fuel which is currently being held within the aircrafts fuel tanks.

There are two basic methods of providing this measurement:

Resistive Type Measuring Systems

Capacitive Type Measuring Systems

Both of these systems provide fuel quantity information by varying a precisely controlled electrical signal. However the method of varying that signal is considerably different between the two. In general, while resistive type systems are reasonably accurate and reliable they do not provide the high level precision and extended long term reliability that is provided by the capacitive type system. As a result, in modern aircraft, resistive systems are typically relegated to lower cost, lower performance aircraft while higher cost, and higher performance aircraft will almost always utilize the capacitive systems.

This training document will provide a general knowledge about both of these systems without going too deeply into the engineering and technical aspects of either system. This document is not intended to provide technical training at a level that would permit the student to perform repairs or maintenance on this system but rather is intended to provide a general knowledge of those systems at a level required by a Sales or Marketing person. Therefore only following subjects will be addressed:

a) A General Theory of System Operation
b)Components of the system
c) System pros and cons
d) Typical failure modes
e) Typical end users
f) Common manufacturers

 

Stay tuned for upcoming Blogs

Airspeeds- Selecting a Replacement Indicator

Airspeeds – Selecting a Replacement Indicator

 

Typically, you can replace any airspeed indicator with another manufacturer’s indicator of the same type and range. However, there are some considerations, which should be taken into account.

Aerosonic and Kollsman indicators often have a longer case than other manufacturers, this could cause an installation problem in some aircraft.

On typical indicators the Pitot input will be in the center of the back of the indicator, with the Static input to the right, when viewed from the rear. Occasionally you will find some older indicators where this was reversed. This may cause installation difficulties on some aircraft.

TGH Aviation offers custom range markings for all blank-dial instruments (most commonly, factory new units) and re-screening services on used instruments in need of refreshed or adjusted range markings. Call or email one of our sales rep’s today for assistance and quotes on all of your Airspeed or other instrument requirements.

Airspeeds- Frequently Asked Questions

Airspeeds – Frequently Asked Questions

 

What would cause my airspeed indicator to be stuck at zero all the time?

A common cause of this is a problem with the Pitot source. If the line from the Pitot tube has disconnected, then pressure will not be applied to the instrument.

If the Pitot tube is clogged, then pressure will not be applied to the instrument.
It is common for Leaf Bugs to build nests in Pitot tubes and effectively clog them.

 

What would cause my indicator to be stuck at a high speed all the time?

A common cause of this is over pressure being applied to the Pitot tube. Aircraft are often washed using a high-pressure water hose. A careless mechanic may spray the hose across the Pitot tube applying high pressure to the air speed indicator. This will usually destroy the diaphragm. Units damaged in this way normally cannot be repaired and must be replaced.

 

Can you re-screen and/or range mark my dial?

Yes, we can. The repair department will advise you of the fee for this process. Screening dials is not done in house, this function is done at an outside vendor. The repair shop will advise the lead time. In order to ensure that the proper range marks are applied we require a copy of the airspeed specifications that are in the Pilot’s Operating Handbook.

 

The temperature bulb on my true airspeed indicator is broken can you fix it

No, we cannot. The bulb on a true air speed indicator is filled with gas. All of the gas escaped when the bulb broke. The bulb must be replaced. However, these bulbs are extremely expensive and extremely difficult to find.
Is the indicator you are selling me, Tso’d ?

United Instruments, Edo-Aire, Kollsman, Garwin, Aerosonic – Yes

UMA – No

If an instrument is certified to a TSO, it must state such on the ID plate. If it does not state the TSO on the name plate then you must assume that it is not approved to the TSO.

 

What is a TSO ?

TSO stands for Technical Standard Order. This is an FAA document, which, defines how a specific type of instrument should work in order to be considered airworthy.

 

What is the tolerance (accuracy) on an airspeed indicator?

Typically +/-2 (Knots or Miles per hour) up to 200 after which it is typically +/-3.

 

Why does it cost so much to overhaul my airspeed indicator?

Overhauling an airspeed indicator is not as simple as you would think. A typical overhaul includes all of the following steps:

Total dis-assembly and inspection.
Determine and correct the cause of failure.
Ultrasonic cleaning of all jewels, pivots, and gears.
Reassemble internal components.
Silk-screen dial and/or range mark
Calibrate the unit to manufacturers and/or FAA specifications
Assemble unit into case.
Seal Case.
Verify calibration of final assembly.
Accomplish cosmetic touch-up.
Complete all FAA mandated paperwork and certifications.

The typical time required to overhaul an airspeed indicator can range from 1 hour for a simple unit to over 3 hours for complex units.

Calibration of an airspeed indicator is a complex process. Airspeed is a non-linear function, which must be displayed on a linear dial. There are at minimum seven calibration points that are all interactive with each other.

Airspeeds – Get to Know the Operation and Manufactures

Airspeeds – Get to Know the Operation and Manufactures

 

How it works

Pitot pressure is forced into the diaphragm causing it to expand like a balloon. Static pressure is contained within the indicator case and surrounding the diaphragm. As the static pressure changes it, will either cause the diaphragm to compress, as the aircraft loses altitude or allow it to expand as the aircraft gains altitude. This expansion and contraction of the diaphragm is mechanically linked to the pointer causing it to move around the dial thereby displaying the speed of the aircraft as a function of the difference between the Pitot and static pressures.

 

Range Marks

Range marks are a reminder to the pilot of the aircrafts basic operating envelope as it pertains to airspeed. Typical range marks found on an air speed dial are:

White Arc – VFE This is the maximum speed at which the aircraft can operate safely with the flaps extended.

Green Arc –  This is the normal operating range

Yellow (Orange) Arc – Caution

Red Radial – VNE Never exceed speed

Blue Radial – This is the minimum operating speed using one engine on a two engine aircraft.

Note: Maneuvering speed is not marked on the dial, it is normally on a placard, which is located on the instrument panel.

 

Manufactures

The following companies all have manufactured air speed indicators and are the most common that you will see:
United Instruments

Kollsman
Aerosonic
Aeromarine
McCleod
UMA
Garwin
Edo-Aire

 

Airspeeds- Basic Principle of Operation

Airspeeds- Basic Principle of Operation

 

Main Components

The major components of an air speed indicator are:

  1. Case
  2. Diaphragm
  3. Dial
  4. Pointer
  5. Mechanical Linkage
  6. Hair Spring
  7. Jewels and Pivots


Case
A standard air speed indicator for general aviation comes in a 31/8  inch diameter case. This is a standard size for most general aviation indicators. It is important that an air speed case be air tight as the case contains the static pressure input.

A leaky air speed case will cause the indicator to give erroneous readings. There are two input ports on the back of the case. These ports are the Pitot port and the Static port. These ports are connected to aircraft Pitot tube and Static port respectively.

 

Diaphragm
A diaphragm is essentially a balloon made of very thin metal. Typical metals used for this purpose are copper or brass. The diaphragm is sealed at all points except for one very thin pressure input tube. This tube is located directly in the center of the back face of the diaphragm. The pressure tube is connected directly to the Pitot port. The thickness of the metal used in manufacturing the diaphragm will determine the range of the air speed indicator (thin = low speed, thick = high speed). It is important to note that this diaphragm is extremely delicate. Picking up a unit a blowing air into the input port will damage the diaphragm.

 

Dial
The dial will contain the speed information and any pertinent range marks.

 

Pointer
The pointer points to the current speed of the aircraft as indicated on the dial.

 

Mechanical Linkage
The mechanical linkage connects the pointer to the diaphragm.

 

Hair Spring
The hair spring returns the pointer to zero when pressure is removed from the indicator.

 

Jewels and Pivots
The pivot is the spindle or axle for the pointer. Jewels are glass bearings on which the pivot rotates.

 

 

Understanding Your Airspeed

Understanding Your Airspeed

 

General Information

In its purest form, an air speed indicator is simply a differential pressure gauge. This means that it is displaying the difference between two different pressure sources that are being simultaneously applied. In the case of airspeed, the two pressures are Pitot Pressure and Static Pressure.

Pitot Pressure is the pressure that is generated when air is forced into the aircraft Pitot tube because of the forward motion of the aircraft. The Pitot tube is a slender tube that is typically mounted near the front of the aircraft. The opening of the tube is facing forward so that air is forced into it. This tube is connected directly to the input of the air speed indicator.

Static pressure is the standard air pressure at the current altitude. Static pressure will vary due to altitude changes and due to changes in weather.

Standard Static pressure at sea level altitude on a “standard” day is typically 29.92 In Hg (inches of mercury) as measured on a class “A” barometer. Static pressure on an aircraft is measured at the static port. The static port is a small hole usually located on the side of the aircraft. This pressure is applied to all instruments in the aircraft static system, of which the air speed indicator is one.

 

Airspeed Indicators – Product Familiarization

Airspeed Indicators – Product Familiarization

 

General Information

The Air Speed indicator provides the basic function of indicating to the pilot the current speed of his aircraft. The indicator is normally a 31/8” size dial face with a single pointer. Location of this indicator is typically in the top row of instruments on the left side of the panel. In a standard “T”, configuration instrument panel the airspeed indicator would be located just to the left of the attitude gyroscope.

 

Types of Air Speed Indicators

  1. Indicated Air Speed Indicator
  2. True Air Speed Indicator (Manually Operated)
  3. True Air Speed Indicator (Automatically Operated)
  4. Maximum Allowable Air Speed Indicator
  5. Mach Air Speed Indicator
  6. F1 Air Speed Indicator
  7. Helicopter Air Speed Indicator
  8. Dual Scale Indicators

 

Indicated Air Speed Indicators
The Indicated Air Speed (IAS) Indicator provides the pilot with a speed-reading, which is based only on Pitot and Static pressure inputs. This type of indicator does not take into account other variable inputs such as temperature or altitude.

 

True Air Speed Indicator (Manually Operated)
The manually operated True Air Speed Indicator provides the pilot with a method of inputting pressure altitude and outside air temperature via a knob on the instrument face. This knob controls a sub-dial which will provide the pilot with “True Airspeed’ data

 

True Air Speed Indicator (Automatically Operated)
An automatically operated True Air Speed Indicator has both a temperature bulb and altitude aneroid built into the instrument. This type of indicator will always display the true speed of the aircraft without user input.

 

Maximum Allowable Air Speed Indicator
A Maximum Allowable Air Speed Indicator has a second pointer that is set to indicate the maximum permitted speed of the aircraft at the current altitude. This pointer is usually a red barber pole.

 

Mach Air Speed Indicator
A Mach Air Speed Indicator indicates the speed of the aircraft as a percent of the speed of sound. When an object is traveling at the speed of sound it is traveling at Mach 1, twice the speed of sound would be Mach 2, etc…

 

F1 Air Speed Indicator
An F1 Air Speed Indicator is a high-speed indicator, typically 600 Kts. or higher and typically is a drum type indicator.

 

Helicopter Air Speed Indicator
A Helicopter Air Speed Indicator is typically an Indicated Air Speed Indicator that has very low speed-readings.

 

Dual Scale Indicator
One Knot, one Nautical Mile, is equal to 1.15077945 Statute Miles.
One Statute Mile is equal to 0.86897624 Knots. A dual scale air speed indicator will indicate both Knots (KPH or Kts.) and Statute Miles (MPH). Always verify if the customer wants the Kts. or MPH on the outer or inner scale of the dial.

TGH Aviation Awarded Military Contract

TGH Aviation Awarded Military Contract for Support of the United States Air Force

Auburn, CA, December, 8th, 2015

T-38Talon

TGH Aviation, based out of the Auburn Airport in Auburn CA, is proud to announce it has been awarded a multi-million dollar five year contract by the U.S. Air Force for the purpose of overhauling all Fuel Flow Transmitters, 8TJ61 Series, for the T-38 Supersonic Jet Trainers. The T-38 is the primary training aircraft for the Air Force. More than 60,000 USAF pilots have trained in the T-38 since it entered service in 1961, when it was the world’s first supersonic trainer. USAF T-38 trainers are primarily used by the Air Education and Training Command for joint specialized undergraduate pilot training (JSUPT), but the aircraft are also used by the Air Combat Command for its companion training program and by the Air Force Materiel Command to test experimental equipment.

“The award of this contract extension is an affirmation by the Air Force of the extraordinary service and quality of workmanship provided by the employees of TGH Aviation,” said TGH President Richard Anderson regarding the recent contract award. For more than 56 years TGH Aviation, formerly The Gyro House, has been an industry leader in flight system support. The company exudes confidence in its ability to provide best-in-class repair, overhaul and new products for a wide range of aviation needs, with the fuel flow support being at the heart of them. TGH operates four full time Fuel Flow Transmitter calibration laboratories. All tools and test equipment utilized by TGH, for the “Return to Service” of Fuel Flow Transmitters, are calibrated, certified and traceable to the National Institute of Standards and Technology (NIST). TGH uses only quality parts that are OEM or FAA approved in the completion of repair work on Fuel Flow Transmitters. The flowmeter operates on the principle that the rotation the fuel by the constant-speed inlet impeller tends to rotate the stationary outlet turbine in an amount which is proportional to the rate of fluid flow through the device measured in pounds per hour. A constant speed motor turns at 8,000 RPM, driving the inlet impeller at 206 RPM through a reduction gear. The inlet struts and inlet impeller combine to impart a clockwise rotation to the incoming fluid, which tends to turn the outlet turbine. The outlet turbine does not rotate through a complete revolution, but as the fuel passes from the inlet impeller with a clockwise spin, it causes the outlet turbine to deflect from its neutral position against the action of a spring. The angular deflection is directly proportional to the mass rate of fuel flow. The outlet turbine deflection is sensed by a synchro transmitter which is directly coupled to it, and provides a signal proportional to the rate of flow to an indicator.

TGH Aviation has a well-known reputation for their precision and innovation within the aviation industry. In addition to military aircraft repair, TGH also overhauls fuel flow transmitters for high performance aviation aircraft, corporate/commuter aircraft and large commercial aircraft. For more information on TGH aviation and their capabilities please check out their website at www.tghaviation.com.

Frequently Asked Altimeter Questions

Frequently Asked Altimeter Questions

 

The pointers on my altimeter are very jumpy and stick sometimes.
What is wrong?

The altimeter is exposed to the outside atmosphere. This includes all of the dirt and dust present in that atmosphere. Dirt and dust will get into the gears and cause them to stick and bind, the vibration from the aircraft will help the gears to overcome this problem but they will be very jumpy and become worse as the unit gets older. This unit needs an overhaul.

 

Can I convert my milli-bar altimeter to InHg or vice versa?

Yes, altimeter dials can be converted, provided that the manufacturer has published a procedure for doing so. If there are no published, FAA Approved, procedures then, no, this modification cannot be accomplished.

 

How often does my altimeter need to be calibrated?

The FAA requires that the aircraft static system be tested and certified biannually. The altimeter is a part of that system.

 

The altimeter ID plate says that it is a 35,000 Ft. altimeter, but the repair shop that overhauled my altimeter marked the unit as being certified to 30,000 Ft. Why the difference?

As altimeters get older and the parts wear the unit will become inaccurate at the higher end of its range. This does not mean that the altimeter can no longer be used; it just has to be used at the lower altitude. Therefore, it will be sold only to customers who request a lower altitude unit, typically general aviation.

 

What is a “car” altimeter?

Sometimes, if a unit is so old and worn that it can no longer be used in an aircraft then these units are sold at a discounted price for use in other than aircraft, typically people will use them in motor homes, cars, and boats.

 

Along with my altimeter, I received a correction card. What is that?

Altitude is a non-linear function.  It is impossible to calibrate an altimeter to be absolutely accurate at all altitudes. Therefore, a certain amount of error is allowable. The correction card advises the users of the amount of error in a particular altimeter. As each altimeter will have its own characteristics, the error card is identified with the unit’s serial number.

 

What is a TSO?

TSO stands for Technical Standard Order. This is an FAA document, which defines how a specific type of instrument should work in order to be considered airworthy. Altimeters manufactured by the following companies typically are manufactured to TSO standards: United Instruments, Kollsman, Garwin, and Aerosonic. Altimeters manufactured by the following companies typically are not qualified to TSO specifications:UMA & Falcon. If an instrument is certified to a TSO, it must state such on the ID plate. If it does not state the TSO on the nameplate then you must assume that it is not qualified to the TSO.

 

What are the typical failure modes of an altimeter?

  1. Sticky/jumpy pointers
  2. Inability to properly adjust the Kollsman window
  3. Out of calibration
  4. Worn pivots and/or jewels
  5. “Oil-canning” of the aneroid

 

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