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Gearbox and turbine engine with geared fan

A gearbox and planetary gear technology, applied in gear transmissions, engine components, machines/engines, etc., can solve problems such as increased complexity of gearboxes, shortened system-level life, and lack of axial flexibility.

Active Publication Date: 2014-12-17
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, working ball joints with moving parts are subject to wear and slack, and their presence will result in increased gearbox complexity
[0005] Also, using traditional steel bearings (e.g. M50 steel alloy or similar) will reduce system level life due to the number of bearings in the gearbox
[0006] Ceramic rolling elements are known to provide longer life than steel rollers, however, they are used in the form of spherical or spherical rollers which are not axially compliant and therefore not suitable for some helical gear configurations

Method used

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  • Gearbox and turbine engine with geared fan
  • Gearbox and turbine engine with geared fan
  • Gearbox and turbine engine with geared fan

Examples

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Embodiment Construction

[0020] Referring to the drawings, wherein like reference numerals represent like elements throughout the various drawings, figure 1 An exemplary gas turbine engine 100 constructed in accordance with an aspect of the present invention is shown. Engine 100 has a longitudinal axis 102 and includes a fan 104, a low pressure compressor or "supercharger" 106, and a low pressure turbine ("LPT") 108, collectively referred to as the "low pressure system". The LPT 108 drives the supercharger 106 via an internal shaft 110 , also referred to as the "LP shaft."

[0021] The inner shaft 110 is also connected to a reduction gearbox, generally designated "G," which in turn is connected to the fan 104 . In the illustrated embodiment, the fan 104 is located in front of the LPT 108 and the gearbox G is located behind the fan 104 . However, gearbox G may be located in front of or behind LPT 108 , and fan 104 may be located in front of or behind LPT 108 . The fan 104 may be surrounded by ductin...

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PUM

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Abstract

A gearbox (10) includes: a carrier (16) having a central axis and forward and aft walls with respective forward an aft coaxial bores; a pin received in the bores, and secured against axial movement; an inner race mounted on the pin between the forward and aft ends, and secured against axial movement relative to the carrier (16); a planet gear mounted for rotation about the pin, wherein a cylindrical interior surface of the planet gear defines an outer race surrounding the rollers, wherein either the inner race or the interior surface of the planet gear defines at least two axially-spaced apart annular raceways; a plurality of generally cylindrical rollers made of a ceramic material disposed in each of the raceways, between the inner and outer races; a sun gear mounted for rotation about the central axis and engaged with the planet gear; and a ring gear engaged with the planet gear.

Description

Background technique [0001] The present invention relates generally to a planetary gearbox and, in particular, to a carrier support device and bearings for a planetary gearbox. [0002] Planetary gearboxes are often used in aircraft engines to transmit power, for example, to drive propellers or fans for power turbines. Gearboxes for aircraft applications must be lightweight, capable of transmitting high torque loads and highly reliable. From a technical point of view, the system-level reliability of the gearbox is the biggest challenge. [0003] In operation, the planetary gears in the gearbox transmit high loads into the carrier, causing the gearbox's bearings and gears to shift and misalign. To prolong commercial lifetime, these deflections and misalignments must be minimized. [0004] It is known to support a gearbox carrier centrally using spherical bearings to transfer loads at an axial midpoint in the carrier. This enables isolation of the torque fingers connecting t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/36F16H57/08
CPCF02C7/36F16H57/082F16H2057/085Y02T50/60F16C19/28F16C33/585F16C2361/61Y10T74/2186F16H57/025F16H1/28
Inventor G.范德默维D.霍尔曼O.比于基西克D.布拉德利R.安特洛
Owner GENERAL ELECTRIC CO
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