DS-11B
selsyn sensor
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






