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Systems And Methods For A Gas Turbine Engine With Combined Multi Directional Gearbox Deflection Limiters And Dampers

Abstract: A planet gear train (200) for an engine casing (226) includes a sun gear (204) rotatable by a shaft (202), a ring gear (208), a plurality of planet gears (206) rotatably mounted in a planet carrier (210) and meshing with the sun gear (204) and the ring gear (208), and a damping system. The damping system includes a soft mount (212) disposed about the shaft (202) and coupling the planet carrier (210) the engine casing (226). The soft mount (212) includes a flexible inner sleeve (214) and a flexible outer sleeve (216). The flexible inner sleeve (214) and the flexible outer sleeve (216) are fixedly coupled together at respective central portions thereof near the shaft (202). The damping system further includes a plurality of damping couplers (218) disposed about an outer flange (232) of the planet carrier (210). The plurality of damping couplers is configured to flexibly couple the flexible inner sleeve (214) to the flexible outer sleeve (216). Fig. 1

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
28 October 2016
Publication Number
36/2017
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
remfry-sagar@remfry.com
Parent Application

Applicants

GENERAL ELECTRIC COMPANY
1 River Road Schenectady, NY 12345 USA

Inventors

1. MILLER, Brandon Wayne
1 Neumann Waytoad Cincinnati, OH 45215 US
2. VONDRELL, Randy M.
1 Neumann Way Cincinnati, OH 45215 US
3. BRADLEY, Donald Albert
1 Neumann Way Cincinnati, OH 45215 US
4. ERTAS, Bugra Han
One Research Circle KWD 215 Niskayuna, NY 12309 US

Specification

WE CLAIM:
1. A planet gear train (200) for an engine casing (226), comprising:
a sun gear (204) rotatable by a shaft (202);
a ring gear (208);
a plurality of planet gears (206) rotatably mounted in a planet carrier (210) and meshing with said sun gear (204) and said ring gear (208); and
a damping system comprising:
a soft mount (212) disposed about said shaft (202) and coupling said planet carrier (210) to said engine casing (226), said soft mount (212) including a flexible inner sleeve (214) and a flexible outer sleeve (216), said flexible inner sleeve (214) and said flexible outer sleeve (216) being fixedly coupled together at respective central portions thereof near said shaft (202); and
a plurality of damping couplers (218) disposed about an outer flange (232) of said planet carrier (210), said plurality of damping couplers (218) flexibly coupling said flexible inner sleeve (214) to said flexible outer sleeve (216).
2. The planet gear train (200) of Claim 1, wherein said plurality of damping couplers (218) each further comprise a central axial spring (306) and an outer radial spring (302, 304).
3. The planet gear train (200) of Claim 2, wherein said central axial spring (306) comprises a structure (310) configured to provide flexible rigidity in an axial direction of rotation of said shaft (202).
4. The planet gear train (200) of Claim 2, wherein said outer radial spring (302, 304) comprises a structure (420, 422) configured to provide flexible rigidity in a radial direction perpendicular to the axial rotation of said shaft (202).

5. The planet gear train (200) of Claim 4, wherein said outer radial
spring (302, 304) comprises:
a coupling ring (302) coupled to the engine casing (226, 320), said coupling ring (302) including slots (330) spaced circumferentially about an inner circumference (326) of said coupling ring (302), each slot (330) comprising a cross-section; and
a spline ring (304) coupled to said planet carrier (210, 318), said spline ring (304) including a plurality of radially extending splines (420, 422) shaped to match the cross section of a respective slot (416, 418), the cross section of each slot (416, 418) including at least one shoulder configured to engage a surface of a respective spline when a relative position between said coupling ring (302) and said spline ring (304) changes by a predetermined amount such that a deflection of at least one of said coupling ring (302) and said spline ring (304) is limited in the radial and circumferential directions.
6. The planet gear train (200) of Claim 5, wherein said spline ring (304) further comprises a cylindrical interior (326), and wherein said central axial spring (306) is disposed within the cylindrical interior (326).
7. The planet gear train (200) of Claim 6, wherein said central axial spring (306) is fixedly coupled to said outer flange (318) of said planet carrier (210).
8. The planet gear train (200) of Claim 6, wherein said coupling ring (302) is fixedly coupled to one of the engine casing (226, 320) and said flexible outer sleeve (216).
9. The planet gear train (200) of Claim 5, further comprising a supply (220) of damping agent to each slot (330, 414), said supply of damping agent configured to resist a movement of said spline (420, 422) in each slot (414) such

that a vibratory motion between said coupling ring (302) and said spline ring (304) is damped.
10. The planet gear train (200) of Claim 9, wherein said damping agent is a fluid.

Documents

Application Documents

# Name Date
1 PROOF OF RIGHT [28-10-2016(online)].pdf 2016-10-28
2 Priority Document [28-10-2016(online)].pdf 2016-10-28
3 Power of Attorney [28-10-2016(online)].pdf 2016-10-28
4 Form 5 [28-10-2016(online)].pdf 2016-10-28
5 Form 3 [28-10-2016(online)].pdf 2016-10-28
6 Drawing [28-10-2016(online)].pdf 2016-10-28
7 Description(Complete) [28-10-2016(online)].pdf 2016-10-28
8 Correspondence by Agent_Assignment_Priority Document_09-11-2016.pdf 2016-11-09
9 201644037056-RELEVANT DOCUMENTS [28-02-2019(online)].pdf 2019-02-28
10 201644037056-FORM 13 [28-02-2019(online)].pdf 2019-02-28
11 201644037056-FORM-26 [06-03-2019(online)].pdf 2019-03-06
12 Correspondence by Agent_Form26_14-03-2019.pdf 2019-03-14