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- Projects Developed
SHIFTING AND LOADING SPM
- SHIFTING AND LOADING SPM Maximum lift height – 2 meters. - Adjustable Pushing force – 400 to 500 Newton. Dia of Job – 325 mm All systems controlled by PLC with dedicated VES software developed by us. Vertical and horizontal movement by Precise controlled Hydraulic system.
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- Projects Developed
Cable Harness
- Wiring Harness & Cable Highlights: • Applications for Engine, Fuselage, Nacelle, Landing Gear, UAV, Space, Ground Support, and a host of System Wiring Harnesses • Repairable Designs • Environmentally Engineered • Durable, Lightweight Materials • Potted, Closed, or Strain-Relief Style Backshells (MIL-Spec or Custom) • Multi-branched Open Bundle and Closed Bundle designs • Cylindrical connector designs as well as D-sub…
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DESIGN AND DEVELOPMENT OF LOAD BANK
- AC RESISTIVE LOAD BANK 115V AC 3 PH /150A / 50HZ 1. Load input Voltage 115 V AC 3 ph 50Hz CURRENT : 150A 2. Specification. CAPACITY 30 KW 3. Load selections TP MCB'S 4. No.of steps : Total : 7 steps ,5A* 1 NO,10A* 2 Nos 25A* 3 NOs, 50A* 1NO. AC RESISTIVE LOAD BANK 115V AC 3 PH…
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- Projects Developed
DESIGN AND DEVELOPMENT AC TO DC CONVERTOR
- Input Voltage:- 95 V AC to 198.75 V AC, Phase to Neutral. Nominal: 162.5V AC Frequency:- 500 Hz Input power compliance: MIL-STD 704-D Output Power:- 350 Watts Output Voltage:- 28 Vdc + 0.5 V / -1.5 V Efficiency :- > 85 % Over Voltage Protection:- MIL-STD 704-D Under Voltage Protection:- MIL-STD 704-D BIT:- Health OK Overload capacity:- 150% for 5…
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- Projects Developed
Flight Data Recorder (FDR)
- Flight Data Recorder (FDR) - a device used to record specific aircraft performance parameters. The purpose of an FDR is to collect and record data from a variety of aircraft sensors onto a medium designed to survive an accident. An FDR has historically been one of two types of "flight recorder" carried on aircraft, the other being a cockpit voice recorder…
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- Projects Developed
Frangible Switch
- PIN Signal Name Destination Type Specification Definition Direction A Operate AIRCRAFT Discrete Single wire Normally Low, Active High. 16-32Vdc, <3.5Amps OUT B +28Vdc Aircraft Power Supply AIRCRAFT DC Single wire 16-32Vdc, <3.5Amps IN C 0V Aircraft Return AIRCRAFT DC Single wire 0V Aircraft Return Common
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- Projects Developed
Test Bench
- A test bench or testing workbench is an environment used to verify the correctness or soundness of a design or model. The term has its roots in the testing of electronic devices, where an engineer would sit at a lab bench with tools for measurement and manipulation, such as oscilloscopes, multimeters, soldering irons, wire cutters, and so on, and manually verify the correctness of the device under…
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- Projects Developed
Hydrostatic Switch
- Specifications - • Setpoint range from 5 to 105 psi • Deadband range from 3.5 psi or 15%, whichever is greater, to 45% of the setpoint • Proof pressure up to 300 psi • Pressure capsule all stainless steel, heliarc welded and leak proof to 1 X 10-9 SCC/SEC • SPDT snap action switch element • Electrical rating 1 amp…
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- Projects Developed
Display Head Assembly (DHA)
- The major technology gap involved in the development of MFD is in Optics i.e the Display Head Assembly. The present-day display panels are generally the ruggedized Active Matrix Liquid Crystal Display (AMLCD) panels are inbuilt with higher-end capabilities of temperature, light sensors, and touch screen capabilities. Building Blocks of a Ruggedized DHA A Ruggedized DHA consists of the Following Basic…
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- Projects Developed
PCB Assembly
- With a reputation for unparalleled quality and advanced traceability, Saline Lectronics has become a preferred supplier for PCB assembly within the military and aerospace industries. We thoroughly understand the critical nature of these industries, and intentionally design our mixed technology manufacturing plans to support mission-critical products that need to withstand extreme conditions within harsh environments. Due to our continued growth…
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