TDK Capsule Gas Temperature Sensor | Aviamisto
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TDK

Capsule Gas Temp Sensor

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Availability
Out of stock
Condition
New
Warranty
6 Months
Price on request

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Description

TDK capsule gas temperature sensor

TDK is an aviation capsule gas temperature sensor used in the automatic control equipment of gas-turbine engines. Published engine documentation lists the unit as standard equipment for the RD-33 Series 2, while additional aviation records identify installations with the RD-33 and AL-31F engine families. The sensor responds to the total temperature of the airflow at the engine inlet and converts that temperature into a control pressure signal. It is therefore a hydromechanical sensing unit rather than a conventional electrical temperature probe.

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Temperature-to-pressure operating principle

The capsule sensing assembly reacts to the temperature surrounding its receiver. The internal mechanism forms a pressure differential whose value changes with inlet-air temperature. This pressure signal is used by compatible engine fuel-control equipment to introduce temperature correction into the governing schedule. The exact port assignment, calibration curve and test limits are determined by the TDK passport and the engine maintenance documentation. The yellow protective caps, sealed fittings, safety wires and hydraulic connections visible in the photographs are important identification and preservation features and must not be treated as electrical connectors.

Role in the RD-33 control system

In the RD-33 control system, the TDK signal participates in correcting the high-pressure rotor speed regulator and the compressor control schedule for inlet temperature. Published descriptions place TDK in the main engine fuel-control circuit together with the NR-59A pump-regulator and the BPR-88 Series 4 limiting-regulator unit. These links describe interaction inside the system; they do not mean that any of the units can replace another. A modified TDK-M execution is documented for later engine configurations, but substitution for TDK must be approved by the applicable engine documentation.

Aircraft and engine application

Public technical records associate TDK with the RD-33 installed on the MiG-29 and with the AL-31F installed on the Su-27. The exact engine series, aircraft modification and installation position must be checked before supply because control-system configurations changed during production and modernization. The published designation 2706.000 is associated with the TDK family, but the complete marking, serial number and drawing reference on the offered unit remain the controlling identifiers.

Identification, inspection and ordering

Before ordering, compare the designation TDK / ТДК, nameplate, pressure-port layout, mounting base, safety locking and any engraved manufacturing reference with the engine illustrated parts catalogue. The supplied photographs show the complete unit from the front, three-quarter, side and port-side views. For a quotation, state the required quantity, engine type, acceptable condition and required documentation. Installation and bench testing must follow the approved passport limits; open-source dimensions and operating data below are useful for identification but do not replace the individual product passport.

Technical details

Product Type
Capsule gas temperature sensor
Primary Designation
TDK
Original Cyrillic Designation
ТДК
Alternative Designations
TDK; ТДК; 2706.000
Measured Variable
Total air temperature at the engine inlet
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Operating Principle
Capsule sensing element with pressure-differential output
Output
Hydraulic / pneumatic control pressure differential dependent on temperature
Documented Engines
RD-33 Series 2; RD-33 family; AL-31F
Documented Aircraft
MiG-29 with RD-33; Su-27 with AL-31F
System Function
Inlet-temperature correction for engine fuel and compressor control schedules
Associated Equipment
NR-59A pump-regulator; BPR-88 limiting-regulator unit; compatible engine fuel-control circuit
Published Working Fuels
RT, T-1, TS-1, T-8V and T-6 aviation fuels under the listed standards
Published Fuel Temperature at Inlet
−50 to +120 °C
Published Ambient Temperature
−60 to +220 °C
Published Pressure Values
0.04 and 0.35 MPa for the inlet / drain circuit; confirm exact port assignment from the passport
Dimensions
112 × 127.5 × 122.5 mm
Mass
Not more than 1.2 kg
Installation Check
Verify engine series, mounting base, ports, marking and calibration against approved documentation
Interchangeability
TDK-M replacement is not assumed without engine-specific approval
Documentation
Exact product passport, engine illustrated parts catalogue and maintenance instructions

Payment & delivery

Orders ship from our hub in Dubai. Partner stock is first transferred to Dubai, then shipped to you.

Dubai stock: 100% before dispatch. Partner stock (Remote stock) and Pre-order: 50% advance payment to start the order and 50% before shipment from Dubai to you.

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