Propeller comprising a moveable dynamic scoop

US9790794B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9790794-B2
Application numberUS-201314433408-A
CountryUS
Kind codeB2
Filing dateOct 8, 2013
Priority dateOct 10, 2012
Publication dateOct 17, 2017
Grant dateOct 17, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The main purpose of the invention is a propeller ( 32 ) for a turbomachine ( 1 ) comprising a plurality of blades ( 48 ) and a blade support ring ( 47 ) fitted with housings ( 50 ) each of which holding a pivot ( 52 ) supporting the root ( 58 ) of one of said blades ( 48 ), characterized in that at least one of the pivots ( 52 ) is associated with at least one dynamic scoop ( 100 ), capable of moving between distinct positions, an open position in which a cooling airflow (F) can be captured, and a closed position as a function of the orientation of the corresponding blade.

First claim

Opening claim text (preview).

What is claimed is: 1. Propeller for a turbomachine comprising: a plurality of blades; and a blade support ring fitted with housings each of which holds a pivot supporting the root of one of said blades, wherein at least one of the pivots is connected to a ring that supports at least one dynamic scoop, the scoop being capable of moving between distinct positions, an open position in which a cooling airflow can be captured, and a closed position as a function of the orientation of the corresponding blade, and wherein the at least one dynamic scoop is movable relative to the root supported by at least one of the pivots. 2. Propeller according to claim 1 , wherein said at least one dynamic scoop is moved from the closed position to the open position by a centrifugal effect due to the rotation speed of the blade, when the blade moves into a position at a predetermined orientation. 3. Propeller according to claim 1 , wherein the pivot is provided with at least one counterweight system, the movement from the closed position to the open position of said at least one dynamic scoop being obtained by actuation of said at least one counterweight system on said at least one dynamic scoop. 4. Propeller according to claim 3 , wherein the counterweight system comprises a counterweight arm and a counterweight, the counterweight arm and/or the counterweight being capable of bearing on said at least one dynamic scoop to move it from the closed position to the open position. 5. The propeller of claim 1 , further comprising an outer propeller cover from which the blades will project outwards, the cover comprising an orifice through which said at least one dynamic scoop is moved from the open position to the closed position and vice versa. 6. Propeller according to claim 1 , wherein said at least one dynamic scoop is free to move between the open and closed positions through a pivot connection. 7. The propeller of claim 1 , further comprising an outer propeller cover from which the blades will project outwards, and wherein the ring and said at least one dynamic scoop are located radially inwards under the cover. 8. Turbomachine comprising a propeller according to claim 1 . 9. Turbomachine according to claim 8 , wherein said propeller is located downstream from a combustion chamber of said turbomachine. 10. The propeller of claim 5 , wherein said at least one dynamic scoop is configured to capture the cooling airflow disposed adjacent the cover. 11. Propeller according to claim 6 , wherein said pivot connection is a hinge connection. 12. Propeller according to claim 6 , wherein said pivot connection is a sliding connection.

Assignees

Inventors

Classifications

  • in turbines · CPC title

  • Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

  • Cross-Sectional Technologies · mapped topic

  • F01D5/081Primary

    Cooling fluid being directed on the side of the rotor disc or at the roots of the blades (F01D5/087 takes precedence) · CPC title

  • of axial insertion type · CPC title

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What does patent US9790794B2 cover?
The main purpose of the invention is a propeller ( 32 ) for a turbomachine ( 1 ) comprising a plurality of blades ( 48 ) and a blade support ring ( 47 ) fitted with housings ( 50 ) each of which holding a pivot ( 52 ) supporting the root ( 58 ) of one of said blades ( 48 ), characterized in that at least one of the pivots ( 52 ) is associated with at least one dynamic scoop ( 100 ), capable of …
Who is the assignee on this patent?
Snecma
What technology area does this patent fall under?
Primary CPC classification F01D5/081. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 17 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).