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Safe Flight Instrument Corporation Pioneering Safety and Performance Products Since 1946 Proprietary Notice This document contains proprietary information.

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Presentation on theme: "Safe Flight Instrument Corporation Pioneering Safety and Performance Products Since 1946 Proprietary Notice This document contains proprietary information."— Presentation transcript:

1 Safe Flight Instrument Corporation Pioneering Safety and Performance Products Since 1946 Proprietary Notice This document contains proprietary information and covers equipment in which Safe Flight Instrument Corporation has proprietary rights. No data contained herein may be duplicated, used or disclosed, in whole or in part, for any purpose, without the express written permission of Safe Flight Instrument Corporation. Safe Flight Instrument Corporation expressly reserves all rights, including all rights of patent and copyright protection.  Safe Flight Instrument Corporation 2004

2 Presented By:  Adrian Rosenberg Helicopter Program Manager  Al Warg Government Program Manager

3 Company History  Founded in 1946  Supplier to Commercial, Business, General and Government Aviation Markets  Product Installed Base Includes 2/3 rd ’s of the World’s Aircraft  Pioneered  Stall Warning  Automatic Throttle Systems  Wind Shear Warning  Over 100 Aviation Patents  Facility – 40,000 sq ft in White Plains, NY  120 Employees

4 Safe Flight Areas of Core Competencies   Detection   Lift Detector/Transducer   AOA Vane   Flap Transmitter   Ice   Pressure   Powerline Detector   Performance   AutoPower®   SCAT   Speed Command   N1 Computer   Warning   Stall Warning   Exceedance Warning   Wind Shear Warning   Stick Shakers   Horns   Voice Alert   Certification   DER Engineering   DER Flight Test   DMIR Quality   Flight Test   Fixed Wing   Rotary Wing

5  Computer Aided Design  Aerodynamic Design  Systems Integration  Environmental Testing  Fixed and Rotary-Wing Aircraft Flight Test Facility Engineering Competencies  Staff Includes  FAA DER Test pilot  FAA DER Systems  FAA DMIR  Conceptual and Analytical Design  Analog and Digital Electrical Design  Software Design and Verification  Electro-Mechanical Design  System Design and Integration

6 Powerline Warning PROTECTION YOU CAN HEAR

7 Powerline Detection  Challenge  Protect Rotary Wing pilots from the “invisible hazard” of power lines  Safe Flight Solution  We developed a powerline detection system that aids pilots in reducing risk of power line strikes during low level operations  Features  Provides an audio alert, which clicks like a Geiger counter, is heard through the audio system and increased in frequency as the power line gets closer.

8 Powerline Strike Risk Reduction On Average:  60% of wire strike victims failed to see the wire  75% of all wire strikes destroy the aircraft  Average reaction time between seeing the wire and meaningful action to avoid is 4.6/5.0 seconds (The Powerline Detection system increases the reaction time to 10 seconds)  Two wire strike accidents occur in the United States each week  One fatality occurs every seventeen days  Only about 10% of the wire strikes that occur are recorded  There are 4.6 Million Miles of Powerline in the U.S. Powerline Strikes are one of the greatest hazards to both civil and military helicopter operations.

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10 Powerline Detection Installation Drawing

11 Powerline Detection System  Offers a Simple, Inexpensive Solution to Major Safety Concern  Significantly Reduces the Potential for Wire Strikes  Passively Detects Obstacles in a Head-Up Attitude  Double Pilot’s Time to React  Can Save Lives As Well As Dollars

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13 The Issue  INADVERTENT OPERATING LIMIT EXCEEDANCE:  Excessive Transmission Torque  Excessive Exhaust Gas Temperature  Excessive Gas Producer Speed  Low Rotor Speed  Others  MOST EXCEEDANCES ARE INADVERTENT  COSTS:  Disaster – Accidents / Lives  Dollars – Equipment / Maintenance  Down Time - MMH/FH  Degraded Aircraft Availability Rate

14 Exceedance Warning  Challenge  Provide rotary wing pilots with a tactile warning when operating limits are approached  Safe Flight Solution  We designed and produce collective and pedal stick shaker systems warning pilots when they are approaching various operating limits  Features  Provides Tactile Warning of when Operating Limits are being approached or exceeded  Such as: Transmission Over Torque, EGT, Rotor Speed

15 The Requirement  Significantly Reduce Inadvertent Operating Limit Exceedances  Reduce Accidents / Unscheduled Maintenance  Expand Pilot’s Situational Awareness  Improve Operator Safety Margins  Solution Must Be Practical and Cost Effective

16 Exceedance System Diagram

17 SFIC Exceedance Warning System  Provides Tactile Feedback Cues to the Pilot  Dual Speed Collective Shaker  Limit Exceedance Computer  Prevents Inadvertent Exceedances from Occurring  Pilot-In-The-Loop Decision Making  No Hard or Soft Stops  Complete Freedom of Collective Movement

18 How It Works – Human Factors  Pilot’s Response - Instinctive  Lower Collective (Reduce Power) if Appropriate  Result  Pilot Has the Information Needed to Make the Best Decision in a Timely Manner  The Pilot Knows When a Limit Is Being Exceeded  The PILOT DECIDES What To Do

19 Collective Shaker  Dual Speed Shaker Controlled by the Limit Exceedance Computer  Low Speed Shaker - Warning of an Impending Limit  High Speed Shaker - Alert That a Limit Has Been Reached or Exceeded

20 How It Works – Collective Shaker

21 Shaker Installation in Bell206B3

22 How It Works – Exceedance Computer  Continuous Real Time Monitoring  Transmission Torque  Engine Exhaust Gas Temperature  Engine Gas Producer Speed  Main Rotor Speed  Others  Dual, Programmable Trigger Points

23 Exceedance Computer- Diagram

24 System Characteristics  Shaker  1.1 to 1.4 lbs  2.5” x 4” Approximate Envelope  <28 VDC @ 0.5 Amp (1 Amp Surge)  Exceedance Computer  8”L x 5”H x 2.5”W  2.5 lbs  Waterproof  Dustproof  28 VDC @ < 1 Amp  Reliability / Maintainability  Reliability > 22,000 hours @ 40 Degrees C  Extensive BIT  Maintenance Diagnostics via Laptop  R / R Time < 10 Minutes  Qualified to DO-160D

25 Exceedance Avoidance OPERATING LIMITS YOU CAN FEEL  Significantly Reduces the Potential for Operating Limit Exceedances  Prevents Exceedances Rather Than Recording Them “After the Fact”  Reduces Unscheduled Maintenance  Improves Situational Awareness- “Eyes Out Of Cockpit”  Increases Operator Safety Margins  Is Effective and Simple to Install

26 Safe Flight Instrument Corporation  Powerline Detection -Doubles Pilots Reaction Times -Saves Money and Lives -Significantly Reduces the Potential for Wire Strikes  Exceedance Warning -Is Inexpensive -Is Easily Installed -Will Increase Aircraft Availability Rates -Will Drastically Reduce Maintenance Costs


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