DS3800NTCF1C1C Product datasheet
Model number: |
DS3800NTCF1C1C |
|
Module Type: |
Thermocouple Condition Card |
Manufacture: |
GE |
|
Condition: |
Brand New |
Range of Product: |
Multilin |
|
Lead time: |
In Stock |
Weight: |
0.3 kg |
|
HS CODE: |
8537101190 |
Dimension: |
19.2x1.7x23.4cm |
|
MOQ: |
1 |
Product Origin: |
USA |
|
System: |
DCS |
Discontinued on: |
Active |
|
Communication Service: |
Ethernet router |
DS3800NTCF1C1C Functional Description
The DS3800NTCF1C1C is a printed circuit board (PCB) developed by GE for the Mark IV Turbine Control System, a key component of the Speedtronic series designed for gas and steam turbine management. As part of the Mark IV system, this board plays a crucial role in maintaining operational efficiency. The Mark IV series represents one of the later advancements in GE's Speedtronic control technology, which was first introduced with the Mark I system in the 1960s. While the Mark IV system, including the DS3800NTCF1C1C, was a significant step forward in turbine control, it did not yet support wind turbine compatibility—an enhancement that was later introduced with the Mark VI series.
The DS3800NTCF1C1C functions as a thermocouple condition card, with the Mark IV system utilizing thirteen of these cards to regulate turbine exhaust temperatures. This card measures real-time exhaust temperature and compares it to a pre-set reference point, generating a command signal to maintain optimal performance. If any of the thirteen cards provide corrupt data, it may lead to inaccurate temperature readings, potentially causing combustion or engine issues. Regular maintenance of the DS3800NTCF1C1C is essential for the long-term health of the turbine system.
This board includes five jumper switches, one resistor network, and four potentiometers, which are used to manage voltage distribution. Although the DS3800NTCF1C1C Thermocouple Condition Card is an essential revision of the thermocouple condition board, it is not the original version; that title belongs to the DS3800NTCF1. The board features alignment markings, factory drill points, and nylon extractor/inserter clips for easy installation and removal. Additionally, the DS3800NTCF1C1C GE Speedtronic MKIV gas turbine control is equipped with two PCB connectors—218A4637-P4 and 218A4553-1 Amp 533002-1—along with various metal film and carbon composite resistors. It also includes polyester film and ceramic capacitors, ensuring stability and durability.
As part of a discontinued legacy series, GE originally provided all technical support for the DS3800NTCF1C1C, including datasheets and manuals. While the board is no longer in active production, its unique functional code structure still serves as a reference for identifying its hardware components and specifications. For those maintaining or replacing Mark IV system components, understanding the General Electric DS3800NTCF1C1C and its specifications is critical for ensuring continued operational efficiency.
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GE Gas Turbine Control System
The GE Mark VI system is a comprehensive control solution used primarily in power generation and other industrial applications. It controls, protects, and monitors gas and steam turbines, generators, and auxiliary systems.
The SPEEDTRONIC™ Mark VI turbine control is the current state-of-the-art control for GE turbines that have a heritage of more than 30 years of successful operation. It is designed as a complete integrated control, protection, and monitoring system for generator and mechanical drive applications of gas and steam turbines. It is also an ideal platform for integrating all power island and balance-of-plant controls. Hardware and software are designed with close coordination between GE’s turbine design engineering and controls engineering to insure that your control system provides the optimum turbine performance and you receive a true “system” solution. With Mark VI, you receive the benefits of GE’s unmatched experience with an advanced turbine control platform.
The heart of the control system is the Control Module, which is available in either a 13- or 21- slot standard VME card rack. Inputs are received by the Control Module through termination boards with either barrier or box-type terminal blocks and passive signal conditioning. Each I/O card contains a TMS320C32 DSP processor to digitally filter the data before conversion to 32 bit IEEE-854 floating point format. The data is then placed in dual port memory that is accessible by the on-board C32 DSP on one side and the VME bus on the other. In addition to the I/O cards, the Control Module contains an “internal” communication card, a main processor card, and sometimes a flash disk card. Each card takes one slot except for the main processor that takes two slots. Cards are manufactured with surface-mounted technology and conformal coated per IPC-CC830. I/O data is transmitted on the VME backplane between the I/O cards and the VCMI card located in slot 1. The VCMI is used for “internal” communications between:
■ I/O cards that are contained within its card rack
■ I/O cards that may be contained in expansion I/O racks called Interface Modules
■ I/O in backup <P> Protection Modules
■ I/O in other Control Modules used in triple redundant control configurations
■ The main processor card
Triple Redundancy
Mark VI control systems are available in Simplex and Triple Redundant forms for small applications and large integrated systems with control ranging from a single module to many distributed modules. The name Triple Module Redundant (TMR) is derived from the basic architecture with three completely separate and independent Control Modules, power supplies, and IONets. Mark VI is the third generation of triple redundant control systems that were pioneered by GE in 1983. System throughput enables operation of up to nine, 21-slot VME racks of I/O cards at 40 ms including voting the data. Inputs are voted in software in a scheme called Software Implemented Fault Tolerance (SIFT). The VCMI card in each Control Module receives inputs from the Control Module back-plane and other modules via “its own” IONet. Data from the VCMI cards in each of the three Control Modules is then exchanged and voted prior to transmitting the data to the main processor cards for execution of the application software. Output voting is extended to the turbine with three coil servos for control valves and 2 out of 3 relays for critical outputs such as hydraulic trip solenoids. Other forms of output voting are available, including a median select of 4-20ma outputs for process control and 0- 200ma outputs for positioners. Sensor interface for TMR controls can be either single, dual, triple redundant, or combinations of redundancy levels. The TMR architecture supports riding through a single point failure in the electronics and repair of the defective card or module while the process is running. Adding sensor redundancy increases the fault tolerance of the overall “system.” Another TMR feature is the ability to distinguish between field sensor faults and internal electronics faults. Diagnostics continuously monitor the 3 sets of input electronics and alarms any discrepancies between them as an internal fault versus a sensor fault. In addition, all three main processors
continue to execute the correct “voted” input data,More info pls check GEH-6005 datasheet