GAS TURBINE ENGINE SHROUD RING MOUNTING
Assignee
ROLLS-ROYCE LIMITED
Filed
Nov 30, 1982
Granted
Jan 26, 1993
Location
WATFORD GB
Abstract
A turbine suitable for a gas turbine engine is provided with a stage of rotary aerofoil blades which is surrounded by a shroud ring made of silicon nitride. In order to minimize load transfer between the shroud ring and the turbine casing the shroud ring is radially supported by and radially spaced apart from the turbine casing by a woven wire mesh array.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 11, 1983
Rescinded
Jul 10, 1992
Duration
9 years, 3 months
Inventor
- 1TERENCE R. PELLOW
Record Details
- Patent number
- US 5181827
- Application
- 00645044
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
ROLLS-ROYCE LIMITEDMore from this assignee
DIVERTER VALVE WITH BYPASS DUCT OBTURATOR
ROLLS-ROYCE LIMITED
FUEL CONTROL SYSTEM
ROLLS-ROYCE LIMITED
AXIAL FLOW GAS TURBINES
ROLLS-ROYCE LIMITED
GAS TURBINE ENGINE
ROLLS-ROYCE LIMITED
COOLED TURBINE BLADE
ROLLS-ROYCE LIMITED
JET PROPULSION NOZZLE
ROLLS-ROYCE LIMITED
Related by domain
GAS TURBINE ENGINE COMBUSTOR HAVING TRAPPED DUAL VORTEX CAVITY
General Electric
SOLID ROCKET PROPELLANT
GAS TURBINE ENGINE FAN (U)
General Electric
TURNING VANE ARRANGEMENT FOR IR SUPPRESSORS
SIKORSKY AIRCRAFT CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION