Invention Grant
- Patent Title: Turbine rotor with air separation ferrules for cooling of blade and disk coupling portions, for a turbomachine
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Application No.: US15698927Application Date: 2017-09-08
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Publication No.: US10598031B2Publication Date: 2020-03-24
- Inventor: Stéphane Pierre Guillaume Blanchard , Joao Antonio Amorim , Maxime Aurélien Rotenberg , Nicolas Xavier Trappier
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCTAFT ENGINES
- Current Assignee: SAFRAN AIRCTAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1658367 20160908
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/08

Abstract:
A turbine rotor is fitted to a turbomachine and includes disks each containing a coupling portion with recesses each holding a root of a blade, and coupled to one another by a first annular ferrule attached to one of them close to the recesses, and second rotationally coupled ferrules, which are respectively coupled radially to the disks, which each consists of at least two semi-annular sectors, and which form with the associated disk a space which communicates with the recesses of the coupling portion of this latter disk. In addition, each first ferrule includes through-holes enabling air to enter this space, and then the recesses, intended to cool the coupling portion which couples its disk and the blade roots.
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