About 23 results
https://drivepatents.com/patents/984693 · 3 Jul 2013
A gas turbine engine (10) includes a spool (14) along an engine centerline axis (A) which drives a gear train (25), said spool (14) includes a low pressure compressor (16) with four to eight (4-8) stages.
https://drivepatents.com/patents/989549 · 19 Jun 2013
A fan rotor (16) includes a fan blade (18) for use in a gas turbine engine includes a sheath (37) formed of a material that is more conductive than a main fan blade body. A grounding element (63) provides a grounding path from the sheath (37) into a rotor ...
https://drivepatents.com/patents/998117 · 19 Sep 2012
A tool (200) includes an annular frame portion (202) including a mount portion (204) extending radially from the frame portion, a hook portion (210) arranged on the mount portion, the hook portion sized and shaped to engage a member of a tubular component ...
https://drivepatents.com/patents/1001042 · 27 Jun 2012
Provided is a machine unit layout system that simplifies the layout of a compressor unit and an expander unit and is extremely effective in terms of not only the reliability of the entire machine but also maintainability. Two separate compressors, a low-pr...
https://drivepatents.com/patents/1004128 · 21 Mar 2012
A turbocharger unit for an internal combustion engine includes an auxiliary component (2) adjacent to the turbocharger unit (1) is provided with means for fixing thereof to the structure of the engine. The auxiliary component (2) has a fluid outlet arrange...
https://drivepatents.com/patents/1005039 · 22 Feb 2012
A manifold mounting arrangement comprising: a discrete manifold module; a clevis arrangement having a clevis straddling a flange and pivotally secured to the flange by a clevis pin; and a locking bar configured to be coupled to the clevis and to constrain ...
https://drivepatents.com/patents/1008727 · 12 Oct 2011
The gas turbine arrangement (1) comprises a casing (10) supported by rod shaped elements (7, 8) connected to a base frame (11). In a plane perpendicular to a longitudinal gas turbine axis (12), some of the rod shaped elements (8) have a longitudinal axis (...
https://drivepatents.com/patents/1014702 · 23 Mar 2011
A coupling assembly for an engine core of a turbomachine is provided. The coupling assembly comprises a duct (114) having a substantially circular shape and surrounding the engine core (112), and a plurality of coupling struts (116), each coupling strut ex...
https://drivepatents.com/patents/1067949 · 26 Apr 2006
The fastening device for the fastening of a turbocharger housing to a turbine casing (10) and compressor casing (20) has two pendulum supports (40,50) each installed on an axially outer end of the turbocharger housing. The fastening device has a support pl...
https://drivepatents.com/patents/1074986 · 17 Aug 2005
A method for assembling a gas turbine engine includes coupling an outer structure within the gas turbine engine, wherein the outer structure includes a socket (58) extending from a radially inner surface (60) of the outer structure, and coupling an inner s...