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

Slides:



Advertisements
Similar presentations
International Coordinating Council of Aerospace Industries Associations Preventing Runway Excursions Technical solutions From the Design and Manufacturing.
Advertisements

September 2005 The Implications of Handling Qualities in Civil Helicopter Accidents Involving Hover and Low Speed Flight Daniel C. Dugan, NASA CDR Kevin.
EECE499 Computers and Nuclear Energy Electrical and Computer Eng Howard University Dr. Charles Kim Fall 2013 Webpage:
HEMS Vision & Mission Our Program, LLC. Vision Vision Mission Mission Principles Principles Collaboration Collaboration Authenticity Authenticity Mission.
Kirkland Energy Services Your Logo Here Larry Kirkland President Larry Kirkland President KES.
Night Helicopter EMS (HEMS) Operations Safety
1-212 th AVIATION REGIMENT COMBAT MANEUVERING FLIGHT AND POWER MANAGEMENT.
Your Fleet Management Solution OSHA Logbooks Your vehicle sends information automatically to your password protected Internet Site. From your computer,
Weather and General Aviation Accidents: A Statistical Perspective Jody James National Weather Service, Lubbock, TX Warning Coordination Meteorologist FAA.
PANH Helicopters. Challenges of Russian-Made Helicopters Operation in Adverse Climatic Conditions.
1 Golden Rules Known and Not Known Every fixed-wing pilot knows that it takes more power to go slower (safely) when flying “behind the power curve”, i.e.,
Know the principles of flight and control for rotary wing aircraft
MAINTENANCE ERROR ACCIDENTS
1 Software Testing and Quality Assurance Lecture 37 – Software Quality Assurance.
REAL-TIME SOFTWARE SYSTEMS DEVELOPMENT Instructor: Dr. Hany H. Ammar Dept. of Computer Science and Electrical Engineering, WVU.
Electrical Safety Training
What’s behind the amazing light show and the booming wall of sound? Energy. Energy is all around us but have you ever considered a career in energy?
Rohrback Cosasco Systems, Inc.
T. Bajd, M. Mihelj, J. Lenarčič, A. Stanovnik, M. Munih, Robotics, Springer, 2010 SAFETY IN INDUSTRIAL ROBOTICS R. Kamnik, T. Bajd and M. Mihelj.
Data Processing Equipment
Takeoff Performance Jet Aircraft Performance
Uncontrolled copy not subject to amendment Principles of Flight Learning Outcome 2 Understand how the stability and manoeuvrability of an aeroplane are.
Data Driven Safety. X-15 Simulator X-15 Simulator Use Time honored criteria to predict aircraft behavior failed to uncover serious threats Pilot.
Risk Assessment – An Essential Standard
National Transportation Safety Board- NTSB
Fueling System Safety Solutions Presented by SEMPER Program LLC “Increase Safety of Operations Through HMI”
Quality Assurance Human Factors Proactive Safety Management: Emirates Airline Maintenance Human Factors Tim J. Garrett Human Factors Manager OFC
Maintenance Malfunction Information Report (MMIR) & Event Reporting Ed DiCampli Helicopter Association International.
Modern Software Engineering for Distributed Embedded Systems Joseph Voelmle, Carlos Daboin, Joanne Sirois, Josh Gallegos Mentor: Dr. Janusz Zalewski.
Levels of safety Priorities for eliminating hazards in the workplace Eliminate the hazard through the machine design stage Apply safeguarding technology.
Centre for Petroleum Production Facilities CPPF SINTEF / MARINTEK / IFE / IRIS / UiS / NTNU In co-operation with the petroleum industry Copyright CPPF.
Annual Reports Direct Mail Business Cards Brochures Posters Letterhead Flyers Note Pads Stationery Labels Digital Printing Large Format Variable Imaging.
Conditions and Terms of Use
Honeywell Helicopter RMUs
2.2 Software Myths 2.2 Software Myths Myth 1. The cost of computers is lower than that of analog or electromechanical devices. –Hardware is cheap compared.
AvSport of Lock Haven What’s the Spin on Stalls? Presentation Copyright © 2015 Mastering the most dreaded maneuver in flight training Prof. H. Paul Shuch,
Presented to: By: Date: Federal Aviation Administration Minimum Safe Altitude Warning November 19, 2008 Glenn W. Michael Air Traffic Manager, Boston ARTCC.
Federal Aviation Administration 0 Certification Standards for New Technologies June 9, 2005 Certification Standards for New Technologies Presentation to:
848T High Density Temperature Measurement Validation Diagnostic.
SUPERAWOS AWOS AUTOMATED UNICOM. YOUR PILOTS NEED AWOS For flight requirements UNICOM For flight safety & service.
HELICOPTER SAFETY - ACHIEVING THE NEXT LEVEL 4-6 June 2007 Sao Paulo, Brazil Roy Fox Chief, Flight Safety.
Overcoming The Challenges Together Fred Brisbois Director, Aviation & Product Safety Sikorsky Aircraft REDUCING THE ACCIDENT RATE.
Affordable Computerized Maintenance Management Solutions (CMMS) Gabi Miles Hach Company May 22, 2009.
1-212 th Aviation Regiment th AVIATION REGIMENT COMBAT MANEUVERING FLIGHT And POWER MANAGEMENT.
12 Myths about Stalls & Spins Checked out from the Members Only Library Society of Aviation and Flight Educators The following presentation.
Managing Rotorcraft Safety During Frequently Performed Unique Missions September 28, 2005 AHS International Helicopter Safety Symposium 2005 Philip G.
Office of Aviation Safety Airspeed Selection and Stall Training Procedures Operations presentation.
Lecture 9: Ecological Factors & Aircraft Performance AIRCRAFT WEIGHT & PERFORMANCE.
AIR & SPACE TRAVEL CONTINENTAL US FLIGHT OPERATIONS PROVIDE GENERAL AVIATION SERVICES PROVIDE FLIGHT PLANNING SUPPORT Request Flight Plan Request User.
1 Industrial Process Offerings and Capabilities May 8, 2003 Atmosphere Recovery, Inc nd Avenue North, Suite 110 Plymouth, MN Ph: (763)
Isolation Lock-Out Room Johns River Quarry Site Contact: Blake Ardrey, Quarry Manager, BCM, Johns River Quarry Phone:
Lecture 9 Ground Proximity Warning System (GPWS) Radio Aids & Navigational System.
Uncontrolled copy not subject to amendment Principles of Flight Learning Outcome 4 Know the principles of flight and control for rotary wing aircraft Identify.
Uncontrolled copy not subject to amendment Principles of Flight Learning Outcome 2 Understand how the stability and manoeuvrability of an aeroplane are.
CFIT Controlled Flight into Terrain Video - ron flat light.
Staying Ahead of the Curve IFM Outsourcing pushes the envelope on energy savings Chris Pesek, Managing Director Integrated Facilities Management, JLL.
LECTURE 7 AVIATION SAFETY & SECURITY
Process Safety Management Soft Skills Programme Nexus Alliance Ltd.
Health and Safety Legislation E5: Human Factors Design IB Technology.
FUNDAMENTALS OF COMPUTER SYSTEMS Lesson 1. Starter What is the difference between hardware and software?
2016 Maintenance Innovation Challenge
FBW – Introduction The FBW architecture was developed in 1970’s
Engine Control Systems
Why did you choose us? To address and provide a solution to the many problems associated with your current manual filing system -Problems include: -Lack.
Warm-Up – 1/6 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the categories of aircraft for which a pilot.
Preventing Runway Excursions Technical solutions
Air Carrier Continuing Analysis and Surveillance System (CASS)
Air Carrier Continuing Analysis and Surveillance System (CASS)
Mastering the most dreaded maneuver in flight training
Presentation transcript:

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

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

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

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

 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

Powerline Warning PROTECTION YOU CAN HEAR

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.

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.

Powerline Detection Installation Drawing

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

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

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

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

Exceedance System Diagram

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

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

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

How It Works – Collective Shaker

Shaker Installation in Bell206B3

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

Exceedance Computer- Diagram

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

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

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