Transcript UH-60M Evolution

UH-60M Evolution
UH-60A/L
Baseline
UH-60M
Block I
UH-60M
Upgrade
UH-60M
Block II
FUTURE
FORCE
 Analog Cockpit
 STD Transmission
 700 Series Engine
 Digital Cockpit
 Dual Digital Flight Controls
 Fully-Coupled Flt Director
 Wide Chord Blades
 Rotor Brake Provisions
 Folding Composite
Stabilator
 Improved Durability
Gearbox
 701D Engine
 IVHMS / HUMS
 Fly-by-Wire (FBW)
Advanced Flight Controls
 Common Cockpit Common Avionics
Architecture Sys (CAAS)
 Full-Authority Digital Engine
Control (FADEC)
 Composite
Tailcone/Driveshaft
 JTRS – (Alt Comms)
 CMWS / ICMD
 Improved Turbine Engine
Program (ITEP)
 Improved Transmission
 FLIR/MMR
 Large Fuel Cell
 Improved ASE
 Composite Airframe
Performance Attributes (4K/95):
External Lift (4500 lbs)
Net Ready
Today
2007
External Lift (4500 lbs)
Net Ready
2009
External Lift (9000 lbs)
Net ready
2013
UNCLASSIFIED
UH-60M BLOCK 1 BLACK HAWK
New Cabin
Section
Logistics
Initiatives
 On- Board Diagnostics
(HUMS)
 Conditioned Based
Maintenance (CBM)
 Performance Based
Logistics
Propulsion
 Monolithic
Machined Parts
 Transmission
Beams
 Corrosion
Protection
 Wide Chord Blades
 T700-GE-701D Engine
 Rotor Brake
Enhanced Survivability
 Enhanced Laser Warning System
 Improved IR Suppression
 Crashworthy Fuel System (CEFS)
Integrated Digital Cockpit
 4 Multifunction Displays
 Improved Data Modem
 Enhanced GPS / INS System
 BFT
 Dual Digital Flight Controls
 Digital Map
 Integrated Storm Scope
UNCLASSIFIED
UH-60M Upgrade Black Hawk
Active Controls w/
Tactile Feedback for
Improved Situational Awareness
Regime based CLAWS with
“Always On” Level 1 DVE Capability
Fully integrated Triple
Redundant Flight Director
New MRS/TRS with
12.7 mm Ballistic Tolerance
Hydraulic and Electrical
Improvements
T700-GE-701D Engine
Wide Chord Blades
with FADEC
Permanent Magnetic Generators
Transmission Driven Backup Pump
Removed Quick Disconnect Fittings
Extended Emergency DC Electrical Power
Improved Ballistic Tolerance
Dual Channel, Triplex
Fly-by-Wire FCS
FADEC
Common CAAS Cockpit
Embedded Flight Model
Improved Hover, EICAS, WCA Displays
Integrated FD Panel
Integrated with FBW FCS
Integrated ASE
Displays
Improved
PVI
Integrated
JACS and CMWS
Airframe Improvements
New Cabin, Upper Deck,
Transmission Beams and Servo Rails
Composite Tail Cone
and Driveshafts
Improved Stabilator Actuator,
triplex position sensor with
Digital Interface to FBW