N61-0841-000-000:Layout 1 09/05/2008 2:19 PM Page 1 TPE331 ... · † Beta-Pressure Sensing Switch...

2
TPE331-10 Turboprop Engine Advanced Engine Performance and Power Generation Capability HIGH PERFORMANCE. INCREASED PERFORMANCE. LOWER COST OF OWNERSHIP. Photo Courtesy of General Atomics Aeronautical Systems, Inc. All Rights Reserved.

Transcript of N61-0841-000-000:Layout 1 09/05/2008 2:19 PM Page 1 TPE331 ... · † Beta-Pressure Sensing Switch...

Page 1: N61-0841-000-000:Layout 1 09/05/2008 2:19 PM Page 1 TPE331 ... · † Beta-Pressure Sensing Switch † Fire-Shield Adapter † Propeller Flange † Torque and Temperature Limiting

TPE331-10 Turboprop Engine

Advanced Engine Performance and Power Generation Capability

HIGH PERFORMANCE. INCREASED PERFORMANCE. LOWER COST OF OWNERSHIP.

Photo Courtesy of General Atomics Aeronautical Systems, Inc. All Rights Reserved.

N61-0841-000-000:Layout 1 09/05/2008 2:19 PM Page 1

Page 2: N61-0841-000-000:Layout 1 09/05/2008 2:19 PM Page 1 TPE331 ... · † Beta-Pressure Sensing Switch † Fire-Shield Adapter † Propeller Flange † Torque and Temperature Limiting

N61-0841-000-000September 2008© 2008 Honeywell International Inc.

Honeywell

P.O. Box 29003

Phoenix, AZ 85038-9003

Domestic: 1.800.601.3099 or

International: 602.395.3099

www.honeywell.com

Specifications - (Sea Level – Standard day – Uninstalled)

Power output: shp 940shp (thermo) 1,000eshp 944eshp (thermo) 1,045

ESFC: 0.534RPM: gas gen 41,730

shaft output 2,000 (cw from rear)

1,591(ccw from rear)

Weight: 375 lbPressure ratio: 10.37Airflow: 7.7 lb/secFuel: Jet A, Jet B, Jet A-1,

JP-8, JP8+10, JP-1, JP-4, JP-5

Oil: Mil-L-23699BMil-L-7808Type I/Type II

Electrical: 24 vdc,16.2 amp (max)

(Demonstrated)Start capability: SL–30,000 ft

No minimum O.A.T. to + 55ºC

(Demonstrated)Operational limits: SL–45,000 ft

No minimum O.A.T to + 55ºC

Compressor bleed: high pressure10% (max)

*Available in cw and ccw

Optional Accessories/Features• Digital Control System

- Digital Electronic Engine Computer(DEEC)

- Built In Test (BIT)

- Electronic Fuel Control(Hydromechanical Back-Up System)

- Electronic Propeller Governor

- Optional Extended RPM Operation

- Strain Gage Auto Bridge Switching

• Water Methanol Augmentation Manifold

Basic Engine Includes• Control System

- Single Red Line /Auto-Start Controller

- Hydromechanical Fuel Control

• Propeller Governor

• Dual Bridge Strain Gage TorqueSensing System (redundant system)

• Fuel Pump

• Fuel Shutoff Valve,

• Fuel Anti-ice Heating System

• Dual Continuous Ignition System

• Lubrication System

• Propeller-Pitch Control

• Oil Temperature-Sensing Bulb

• Negative-Torque-Sensing (NTS) System

• Beta-Pressure Sensing Switch

• Fire-Shield Adapter

• Propeller Flange

• Torque and Temperature Limiting

• Fuel Purge System

• Air Speed and Ambient Pressure RatioTransducer

• Aluminum Gearbox

TPE331-10 TURBOPROPENGINE

Aircraft AccessoriesStarteror StarterGenerator

TachometerGenerator

Prop PitchControlPropeller

Governor

N61-0841-000-000:Layout 1 09/05/2008 2:20 PM Page 2