This application relates to a mechanical linkage for driving a compressor inlet guide vane system for gas turbine engines, wherein a spring preload is included into the mechanical linkage.
Gas turbine engines include a compressor which compresses air and delivers it into a combustion section where it is mixed with fuel and burned. Products of this combustion pass downstream over a turbine section, driving turbine rotors to provide power to the gas turbine engine.
Inlet guide vanes typically control the flow of air to the compressor section. Variable vane systems are known. In such systems, an angle of incidence provided by the vanes, for guiding the air to the compressor, is varied depending upon the amount of air that is to be delivered to the compressor.
In one such system, a ring gear is driven to rotate through a mechanical linkage including a plurality of rods, and a hydraulic motor for driving the rods. The ring gear drives a plurality of sector gears to cause a plurality of vanes to rotate as the ring gear is driven to rotate between a full open and full closed position.
One challenge with these systems is that variables in the flow of air to the guide vanes, and the compressor, can cause vibration on the variable vanes, ring and sector gears, and across the mechanical linkage.
A variable vane system includes a plurality of vanes each being pivotal about an axis. A mechanical linkage drives the plurality of vanes to rotate about the axis. The mechanical linkage includes a ring gear meshing with a plurality of sector gears, which in turn drives the plurality of vanes. There is at least one rod to drive the ring gear to rotate. The rod is driven by a hydraulic motor. A spring bias force is provided in the mechanical linkage to resist oscillation.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
A turbine engine 120 is illustrated in
As shown schematically in
An actuation system 134 for driving the variable vanes is illustrated in
As can be appreciated from these Figures, as the rod 40 is driven to move inwardly and outwardly of the housing of the hydraulic motor 60, it causes pivot housing 160 to pivot on the pin 65. This causes the rod 36 to also move toward and away from the device 31, and in turn cause the device, and hence the ring gear, to rotate.
Spring 66 is shown schematically in
With either of the disclosed embodiments, the spring will resist any oscillation in the mechanical linkage that might be imposed by variable flow characteristics such as vortices, etc.
Although embodiments of this invention have been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention, such as using torsional spring at sector gear locations. For that reason, the following claims should be studied to determine the true scope and content of this invention.
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Number | Date | Country | |
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20110110765 A1 | May 2011 | US |