ROTOR IN A TURBINE ENGINE COUPLED TO PROVIDE INDIVIDUAL AND SEPARATE ACCESS TO RESPECTIVE ASSEMBLIES OF COMPRESSOR AND TURBINE DISKS
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Mar 24, 2016
app pub date -
May 5, 2014
filing date -
May 14, 2013
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A rotor for a turbine engine. The rotor may include an assembly of axially-bolted compressor disks (14). A compressor torque tube (30) is connected to the assembly of compressor disks (14). The rotor may further include an assembly of axially-bolted turbine disks (22). A turbine torque tube (32) is axially connected to the assembly of turbine disks (22). A marriage coupling (34) is arranged to interconnect the respective torque tubes (30, 32). The marriage coupling includes a flange joint arranged to decouple the compressor torque tube or the turbine torque tube so that individual and separate access can be provided to the respective assemblies of compressor disks and turbine disks.
First Claim
Family
International Classification(s)
Cited Art Landscape
Patent Citation Ranking
Advertisement
Advertisement
Advertisement
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully