Chocking and retaining device
10145250 ยท 2018-12-04
Assignee
Inventors
Cpc classification
F05D2300/603
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/282
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/96
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/432
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/323
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/326
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/3053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/3007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/611
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D5/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A device for chocking and retaining a dovetail root of a blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a disc includes a retention body having a key portion receivable in a keyway formed in the base of the slot, and a mating portion for mating with a complementary mating portion of the root to prevent relative axial movement between the retention body and the root. The retention body has a lowered position in which the key portion is received sufficiently deeply in the keyway to allow the root to be positioned in the slot without interference from the retention body and also has a raised position in which, after the root is positioned in the slot, a part of the key portion is still received in the keyway while the mating portion mates with the complementary mating portion of the root.
Claims
1. A device for chocking and retaining a dovetail root of a blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a disc, the device including: a retention body having: a key portion receivable in a keyway formed in the base of the slot, the key portion comprising one or more legs and the keyway comprising one or more slots for respectively receiving the legs, a mating portion for mating with a complementary mating portion of the root to prevent relative axial movement between the retention body and the root, and the retention body having a lowered position in which the key portion is received sufficiently deeply in the keyway to allow the root to be positioned in the slot without interference from the retention body, and a raised position in which, after the root is positioned in the slot, a part of the key portion is still received in the keyway while the mating portion mates with the complementary mating portion of the root; a slider which is axially insertable in the slot; wherein the slider and the retention body are configured so that, on axial insertion of the slider in the slot after the root is positioned in the slot, the slider moves the retention body from its lowered position to its raised position, whereby the retention body urges the blade radially outwardly thereby mating flanks of the root to flanks of the slot, while the part of the key portion still received in the keyway retains the root axially in the slot.
2. A device according to claim 1, wherein the retention body has a chamfered lead-in portion against which the slider slides on axial insertion of the slider in the slot to move the retention body from its lowered position to its raised position.
3. A device according to claim 1, wherein the slider has a chamfered or rounded leading edge.
4. A device according to claim 1, wherein the mating portion forms an arc-shaped surface of the retention body and the complementary mating portion forms a correspondingly arc-shaped surface of the root, the normal to the plane of the arc of each arc-shaped surface being substantially perpendicular to the engine axis, whereby the arc-shaped surfaces mate to prevent relative axial movement between the retention body and the root.
5. A device according to claim 4, wherein the normal to the plane of each arc is substantially perpendicular to the radial direction.
6. A device according to claim 4, wherein the arc-shaped surface of the retention body is a convex surface.
7. A device according to claim 4, wherein the arc-shaped surface of the retention body is a concave surface.
8. A device according to claim 1, wherein of the mating portion of the retention body has a relatively compliant outer layer for enhanced contact of the retention body with the root.
9. A device according to claim 1, wherein the slider has one or more chock springs which are arranged to act, in use, on the root to also urge the blade radially outwardly.
10. A device according to claim 1, wherein the slider has a stop at an end thereof which, in use, abuts a face of the disc or the root when the slider is fully inserted in the slot to prevent over-insertion of the slider.
11. A device according to claim 1 including a plurality of the retention bodies, each movable by the slider from its lowered position to its raised position.
12. A rotor assembly of a gas turbine engine, the assembly having: a disc; a circumferential row of blades, each blade having a dovetail root which is retained in a corresponding axially-extending slot in the rim of the disc; and a plurality of devices according to claim 1 for chocking and retaining the dovetail roots of the blades in the slots; wherein each slot has a keyway formed in the base thereof, the key portion of the retention body of each device is received in a respective one of the keyways, and the slider of each device is inserted in a respective one of the slots to move its retention body to the raised position.
13. A gas turbine engine having the rotor assembly of claim 12.
14. A device for chocking and retaining a dovetail root of a blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a disc, the device including: a retention body having: a key portion receivable in a keyway formed in the base of the slot, a mating portion for mating with a complementary mating portion of the root to prevent relative axial movement between the retention body and the root, the mating portion forming an arc-shaped surface of the retention body and the complementary mating portion forming a correspondingly arc-shaped surface of the root, the normal to the plane of the arc of each arc-shaped surface being substantially perpendicular to the engine axis, whereby the arc-shaped surfaces mate to prevent relative axial movement between the retention body and the root, and the retention body having a lowered position in which the key portion is received sufficiently deeply in the keyway to allow the root to be positioned in the slot without interference from the retention body, and a raised position in which, after the root is positioned in the slot, a part of the key portion is still received in the keyway while the mating portion mates with the complementary mating portion of the root; a slider which is axially insertable in the slot; wherein the slider and the retention body are configured so that, on axial insertion of the slider in the slot after the root is positioned in the slot, the slider moves the retention body from its lowered position to its raised position, whereby the retention body urges the blade radially outwardly thereby mating flanks of the root to flanks of the slot, while the part of the key portion still received in the keyway retains the root axially in the slot.
15. A device according to claim 14, wherein the normal to the plane of each arc is substantially perpendicular to the radial direction.
16. A device according to claim 14, wherein the arc-shaped surface of the retention body is a convex surface.
17. A device according to claim 14, wherein the arc-shaped surface of the retention body is a concave surface.
18. A device for chocking and retaining a dovetail root of a blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a disc, the device including: a retention body having: a key portion receivable in a keyway formed in the base of the slot, a mating portion for mating with a complementary mating portion of the root to prevent relative axial movement between the retention body and the root, and the retention body having a lowered position in which the key portion is received sufficiently deeply in the keyway to allow the root to be positioned in the slot without interference from the retention body, and a raised position in which, after the root is positioned in the slot, a part of the key portion is still received in the keyway while the mating portion mates with the complementary mating portion of the root; a slider which is axially insertable in the slot, the slider having one or more chock springs which are arranged to act, in use, on the root to also urge the blade radially outwardly; wherein the slider and the retention body are configured so that, on axial insertion of the slider in the slot after the root is positioned in the slot, the slider moves the retention body from its lowered position to its raised position, whereby the retention body urges the blade radially outwardly thereby mating flanks of the root to flanks of the slot, while the part of the key portion still received in the keyway retains the root axially in the slot.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Embodiments of the invention will now be described by way of example with reference to the accompanying drawings in which:
(2)
(3)
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(5)
DETAILED DESCRIPTION AND FURTHER OPTIONAL FEATURES OF THE INVENTION
(6) With reference to
(7) During operation, air entering the intake 11 is accelerated by the fan 12 to produce two air flows: a first air flow A into the intermediate-pressure compressor 13 and a second air flow B which passes through the bypass duct 22 to provide propulsive thrust. The intermediate-pressure compressor 13 compresses the air flow A directed into it before delivering that air to the high-pressure compressor 14 where further compression takes place.
(8) The compressed air exhausted from the high-pressure compressor 14 is directed into the combustion equipment 15 where it is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive the high, intermediate and low-pressure turbines 16, 17, 18 before being exhausted through the nozzle 19 to provide additional propulsive thrust. The high, intermediate and low-pressure turbines respectively drive the high and intermediate-pressure compressors 14, 13 and the fan 12 by suitable interconnecting shafts.
(9) The fan 12 comprises a fan disc and a circumferential row of fan blades extending from the disc. Each blade has as a dovetail root 30 which is retained in a corresponding axially-extending slot 34 in the rim of the disc 32. To chock the flanks of roots radially outwardly against the flanks of the slots, and to retain the roots axially within the slots, each blade has a chocking and retaining device according to the present invention.
(10)
(11)
(12) The retention body 36 also has a chamfered lead-in portion 48 located between the two legs of the key portion 38. With the root 30 fully inserted in the slot 34, a slider 50 of the device is also inserted into the slot 34. The slider has a chamfered leading edge 52 which engages with the chamfered lead-in portion 48. Further insertion of the slider then pushes the retention body into a raised position, which is shown schematically in the longitudinal cross-sectional view of the retention body, root and disc of
(13) In the raised position, the retention body 36 urges the blade radially outwardly thereby mating flanks of the root 30 to flanks of the slot 34. Moreover, the two mating portions 44, 46 mate with each other, their arc-shaped surfaces preventing relative axial movement between the retention body and the root. In this way, axial loads on the blade can be transmitted via its root to the retention body, and then transferred via shear at the key portion 38 and keyway 40 to the disc 32.
(14) Advantageously, the arc-shaped surfaces can reduce stress concentration in the root 30 by their gradual curvatures. Generally, the normal to the plane of the arc of each arc-shaped surface is substantially perpendicular to the engine axis (and conveniently also substantially perpendicular to the radial direction). This helps the mating portions 44, 46 to prevent relative axial movement between the retention body 36 and the root. The arc-shaped surfaces are also preferably shallow and in the complementary mating portion 46 do not break the root ends or flanks. Under extreme axial loading of the blade, the arc-shaped surfaces can help to redistribute some of the axial load as a compressive force driving the root 30 radially up in the slot 34.
(15)
(16) As shown schematically in
(17) As shown in
(18) As shown in
(19) While the invention has been described in conjunction with the exemplary embodiments described above, many equivalent modifications and variations will be apparent to those skilled in the art when given this disclosure. Accordingly, the exemplary embodiments of the invention set forth above are considered to be illustrative and not limiting. Various changes to the described embodiments may be made without departing from the scope of the invention.