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Civil Aerospace

Introduction

Description

Technical data



The Trent 800 powers the Boeing 777

Trent 800

Technical data

  • The Trent 800 is a three-shaft high bypass ratio engine.
  • Fan diameter: 110 inches (2.79 metres)
  • Eight-stage IP compressor
  • Six-stage HP compressor
  • Single annular combustor with 24 fuel injectors (Trent 700 and 800)
  • Single-stage HP turbine
  • Single-stage IP turbine
  • Five-stage LP turbine (Trent 800, 500, 900 and 600)
Engine EIS Power Applications Seats* Range (nm)*
Trent 875 1996 75,000lb
334kN
Boeing 777-200
(506,000 lb)
305 4100
Trent 877 1996 77,000lb
343kN
Boeing 777-200
(545,000 lb)
305 5210
Trent 884 1997 84,000lb
374kN
Boeing 777-200
(590,000 lb)
305 5870
Trent 892 1997 92,000lb
409kN
Boeing 777-200
(656,000lb)
Boeing 777-300
(660,000lb)
301

368
7665

5955
Trent 895 2000 95,000lb
423kN
Boeing 777-200
(656,000lb)
Boeing 777-300
(660,000lb)
301

368
7665

5955
*Aircraft Manufacturer's Data

 


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