Fan containing fan blades with a U-shaped slot having a decreased length planar section

Patent metadata

Field	Value
Publication number	US-10364687-B2
Application number	US-201514847889-A
Country	US
Kind code	B2
Filing date	Sep 8, 2015
Priority date	Oct 6, 2014
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

A fan for gas turbine engine that includes hub and annular array of fan blades mounted to hub and extending radially outwardly from hub, each fan blade includes blade root. The hub includes a plurality of hub grooves having shape complimentary to shape of blade root and each hub groove receives and radially retains one blade root. A slot is provided on the suction side and on the pressure side of each blade root. Plurality of keys is provided, each key engages with slots in one blade root and with corresponding hub groove so as to axially retain fan blade. The key includes two arms and joining member, two arms are received in slots provided on blade root and joining member extends between the arms. Interface is defined between key arms and slots in blade root, and greater or equal percentage of interface is curved than is planar.

First claim

The invention claimed is:

1. A fan for a gas turbine engine comprising:
a hub defining a plurality of grooves and a plurality of keys, one of the plurality of keys respectively disposed in each of the plurality of grooves;
an annular array of fan blades, each fan blade including a blade root, each blade root being receivably mounted in a corresponding groove of the plurality of grooves so as to be radially retained therein and fitted to a corresponding key of the plurality of keys;
each blade root having a bottom surface defining a generally U-shaped slot, the U-shaped slot extending along the bottom surface from a pressure side to a suction side of each blade root and opening out at the pressure side and the suction side of each blade root;
each key of the plurality of keys is formed in a U-shape so as to be at least partially fitted respectively in each generally U-shaped slot when the blade root is receivably mounted in the corresponding groove of the hub; and
each U-shaped slot being formed from a plurality of planar sections and a plurality of curved sections defined in the blade root, the plurality of planar sections including a first planar section, a second planar section and a third planar section, the second planar section being positioned at a deepest portion of each U-shaped slot intermediate the first planar section and the third planar section, and when each U-shaped slot is viewed in cross section along a length of each blade root in a chordwise direction of each blade root, each first planar section, second planar section and third planar section has a cross-sectional peripheral dimension being a length in the chordwise direction or a height generally perpendicular to the chordwise direction,
wherein, for each generally U-shaped slot, at least one of:
(i) the cross-sectional peripheral length in the chordwise direction of the second planar section is less than at least one of the cross-sectional peripheral height of the first planar section or the cross-sectional peripheral height of the third planar section, or
(ii) the plurality of curved sections each have a respective cross-sectional peripheral dimension having a radius of curvature, and the total cross-sectional peripheral dimension of the radius of curvatures of the plurality of curved sections is greater than the total cross-sectional peripheral dimension of the plurality of planar sections.

2. The fan according to claim 1 , wherein the radius of curvature of each curved section of the plurality of curved sections is equal to or between 3 and 15 mm.

3. The fan according to claim 1 , wherein surfaces of each blade root that define each U-shaped slot are surface treated using low plasticity burnishing.

Assignees

• Rolls Royce Plc

Inventors

• Goldfinch Keith Christopher
• Kalochairetis Antonios

Classifications

• F01D5/323 Primary

  Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor · CPC title

• F05D2250/71

  curved · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F04D29/322

  Blade mountings · CPC title

• F02K3/06

  with front fan · CPC title