GENERIC DESIGN OF AN EMERGENCY RECOVERY AND ESCAPE PATH CLEARANCE SUBSYSTEM FOR ROTARY WING VEHICLES

Award Information
Agency:
Department of Defense
Branch:
Navy
Amount:
$381,000.00
Award Year:
1988
Program:
SBIR
Phase:
Phase II
Contract:
N/A
Agency Tracking Number:
6074
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Lme (delta Technology Systems)
605 Louis Dr - Ste 503b, Warminster, PA, 18974
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
N/A
Principal Investigator
 W Barry Shope
 (215) 675-9656
Business Contact
Phone: () -
Research Institution
N/A
Abstract
INFLIGHT RECOVERY OR ESCAPE FROM A DISABLE HELICOPTER REQUIRES THAT THE ROTOR BLADES NOT INTERFERE WITH THE ORDERLY OPERATION OF THE EMERGENCY SYSTEM THAT WILL RETURN THE OCCUPANTS SAFELY TO EARTH. THE OBJECTIVE IS TO PRESENT A METHODOLOGY FOR REMOVAL OF THE ROTOR BLADES IN A CONTROLLED MANNER TO ELIMINATE THEIR BECOMING A FLYING HAZARD TO OTHER AIRCRAFT IN CLOSE PROXIMITY. THIS REPORT PRESENTS A GENERIC DESIGN FOR BOTH BLADE REMOVAL AND DECELERATION TO DELETHALIZE THEIR DANGER AS FREE FLYING MISSILES. STARTING FROM A TRADE-OFF STUDY OF CANDIDATE CONCEPTS WHICH TAKES INTO ACCOUNT COMPLEXITY, COST, RELIABILITY, MAINTENANCE, AND SYSTEM SAFETY FACTORS, A GENERIC DESIGN IS PROPOSED FOR ACCOMPLISHING THE OBJECTIVE.

* information listed above is at the time of submission.

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