Request a Quote 0
Back to catalog

DS-11B

selsyn sensor

AvailabilityPartner stock
Availability
Partner stock
Condition
New
Warranty
6 Months
Price on request

Price and lead time are confirmed before payment.

Description

DS-11B contactless selsyn sensor for aircraft equipment

DS-11B is a contactless aircraft selsyn sensor used as an AC rotary transformer for measuring angular mismatch between two axes or gyro precession angle. The sensor belongs to the DS-11 family and is used in aviation and specialized industrial control systems. In aircraft applications, DS-11B is associated with gyroscopic systems, attitude and heading equipment, servo systems and onboard automatic control circuits.

Full descriptionCollapse description

Function of the DS-11B angle sensor

The main function of DS-11B is to convert mechanical angular displacement into an electrical signal. The sensor operates in transformer mode: when AC excitation is applied to the excitation winding, output voltages are induced in the synchronization windings. Their amplitude and phase depend on rotor position. This allows the connected system to detect angular mismatch, gyro frame movement or precession angle and transmit the data to a control, indication or follow-up circuit.

Contactless construction of DS-11B

DS-11B is a contactless selsyn, so it has no brushes, slip rings or sliding electrical contacts. This design reduces wear, eliminates sparking at the current-collection point and improves stability in vibration conditions. The absence of friction elements is especially important in aircraft gyroscopic equipment, where additional mechanical resistance can affect measurement accuracy. The sensor is intended for continuous operation as part of onboard or ground-based control and measuring systems.

Operating principle of the DS-11B sensor

In the basic DS-11 winding scheme, the unit has a single-phase rotor excitation winding and three stator synchronization windings arranged 120 degrees apart and connected in a star circuit. Depending on the specific installation, the winding arrangement and connection scheme may vary. As the rotor turns relative to the stator, the inductive coupling between the windings changes. The resulting output EMF on the stator windings is proportional to the angular mismatch and is used by the receiving equipment to determine the measured angle.

DS-11B use on Mi-8 / Mi-171 systems

DS-11B is used in aircraft equipment where small angular movements must be measured with stable electrical transmission. The source context indicates use on Mi-8 / Mi-171 family helicopters, including gyroscopic systems and flight-navigation equipment. Typical application areas include gyro-verticals, attitude and heading systems, control aggregates, servo mechanisms and test equipment. Since actual installation depends on the specific avionics set and aircraft modification, compatibility should be checked against the relevant equipment documentation.

Ordering and replacement of DS-11B

When ordering DS-11B, the exact designation, modification and technical conditions should be confirmed. DS-11B belongs to the wider DS-11 series, which also includes DS-11A, DS-11V and DS-11G. These versions may differ by electrical data, mechanical execution or installation method. For supply or maintenance, the buyer should specify whether a product passport, verification certificate, storage records or wiring diagram is required. It is also useful to confirm the receiving unit, indicator or gyro system where the sensor will be installed.

Technical details

Product Type
Contactless selsyn sensor / AC rotary transformer
Designation
DS-11B
Alternative Designations
DS11B, DS-11Б, ДС-11Б, ДС11Б
Series
DS-11 selsyn sensor family
Function
Measurement of angular mismatch between two axes or gyro precession angle
All specificationsCollapse specifications
Signal Role
Conversion of mechanical angular displacement into an electrical output signal
Operating Principle
Transformer mode with AC excitation and induced stator output EMF
Contact System
Contactless, without brushes and slip rings
Technical Conditions
6Zh2.329.014TU / 6Ж2.329.014 ТУ
OKP Code
754524002607, according to source context
Excitation Voltage
12 V or 36 V AC depending on aircraft circuit and equipment configuration
Excitation Frequency
400 Hz
Rotor Winding
Single-phase excitation winding, according to source context
Stator Winding
Three synchronization windings shifted by 120° and connected in star circuit, according to source context
Operating Mode
Transformer mode / angular mismatch sensor mode
Output Signal
AC EMF with amplitude and phase proportional to angular mismatch
Accuracy Requirement
High output voltage slope for detection of small angular deviations
Application / Where Used
Aircraft gyro-verticals, attitude and heading systems, control aggregates, servo systems and test equipment
Compatible Aircraft / Equipment
Mi-8 / Mi-171 family helicopters and other equipment depending on documentation
Related Modifications
DS-11A, DS-11V, DS-11G
Environmental Context
Aircraft vibration, temperature variation and onboard operating conditions
Technical Documentation
Product passport, verification certificate, test report, storage records, wiring diagram and equipment documentation if available

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.

Availability, lead time, delivery cost and payment terms are confirmed for your order before payment.

Payment & delivery terms

Questions about this part?

Send your requirements — we’ll clarify the details for your order.

Share this part

DS-11B