+ All Categories
Home > Documents > UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I 2007 2009 2013 Analog...

UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I 2007 2009 2013 Analog...

Date post: 19-Dec-2015
Category:
Upload: edith-mcgee
View: 255 times
Download: 14 times
Share this document with a friend
3
UH-60A/L Baseline Today UH-60M Block I 2007 2009 2013 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 Improved Turbine Engine Program (ITEP) Improved Transmission FLIR/MMR Large Fuel Cell Improved ASE Composite Airframe 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 External Lift (4500 lbs) Net Ready External Lift (4500 lbs) Net Ready External Lift (9000 lbs) Net ready UH-60M Block II UH-60M Evolution FUTURE FORCE UH-60M Upgrade Performance Attributes (4K/95):
Transcript
Page 1: UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I 2007 2009 2013  Analog Cockpit  STD Transmission  700 Series Engine  Digital.

UH-60A/LBaselineUH-60A/LBaseline

TodayToday

UH-60MBlock I

UH-60MBlock I

20072007 20092009 20132013

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

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

Improved Turbine Engine Program (ITEP)

Improved Transmission FLIR/MMR Large Fuel Cell Improved ASE Composite Airframe

Improved Turbine Engine Program (ITEP)

Improved Transmission FLIR/MMR Large Fuel Cell Improved ASE Composite Airframe

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

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

External Lift (4500 lbs) Net Ready

External Lift (4500 lbs)Net Ready

External Lift (9000 lbs)Net ready

UH-60MBlock IIUH-60MBlock II

UH-60M Evolution

FUTUREFORCE

FUTUREFORCE

UH-60MUpgradeUH-60MUpgrade

Performance Attributes (4K/95):

Page 2: UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I 2007 2009 2013  Analog Cockpit  STD Transmission  700 Series Engine  Digital.

UNCLASSIFIED

UH-60M BLOCK 1 BLACK HAWK

On- Board Diagnostics (HUMS)

Conditioned Based Maintenance (CBM)

Performance Based Logistics

Monolithic Machined Parts

Transmission Beams

Corrosion Protection

Wide Chord Blades T700-GE-701D Engine Rotor Brake

Enhanced Laser Warning System Improved IR Suppression Crashworthy Fuel System (CEFS)

4 Multifunction Displays Improved Data Modem Enhanced GPS / INS System

BFT Dual Digital Flight Controls Digital Map Integrated Storm Scope

Enhanced Survivability

New Cabin Section

Propulsion

Logistics Initiatives

Integrated Digital Cockpit

UNCLASSIFIEDUNCLASSIFIED

Page 3: UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I 2007 2009 2013  Analog Cockpit  STD Transmission  700 Series Engine  Digital.

UH-60M Upgrade Black HawkUH-60M Upgrade Black Hawk

Composite Tail Cone and Driveshafts

New Cabin, Upper Deck,Transmission Beams and Servo Rails

Wide Chord Blades

ImprovedPVI

Integrated JACS and CMWS

Integrated ASEDisplays

FADECFADEC

Dual Channel, Triplex Fly-by-Wire FCS

Dual Channel, Triplex Fly-by-Wire FCS

Hydraulic and ElectricalImprovements

T700-GE-701D Enginewith FADEC

Permanent Magnetic GeneratorsTransmission Driven Backup PumpRemoved Quick Disconnect FittingsExtended Emergency DC Electrical PowerImproved Ballistic Tolerance

Common CAAS Cockpit Common CAAS Cockpit

Improved Stabilator Actuator, triplex position sensor with

Digital Interface to FBW

Airframe ImprovementsAirframe Improvements

Regime based CLAWS with “Always On” Level 1 DVE Capability

Fully integrated TripleRedundant Flight Director

Embedded Flight ModelImproved Hover, EICAS, WCA DisplaysIntegrated FD PanelIntegrated with FBW FCS

Active Controls w/ Tactile Feedback for

Improved Situational Awareness

New MRS/TRS with 12.7 mm Ballistic Tolerance


Recommended