Turbofan thrust reverser system

Patent metadata

Field	Value
Publication number	US-10087886-B2
Application number	US-201414284893-A
Country	US
Kind code	B2
Filing date	May 22, 2014
Priority date	May 22, 2014
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

A gas turbine engine comprises a core engine, a fan, a bypass duct and a clutch. The fan is driven by the core engine. The bypass duct is configured to receive airflow from the fan. The clutch links the core engine and the fan. The core comprises a reverse-flow, two-spool gas generator in one embodiment. In another embodiment, the fan is driven by a free turbine aerodynamically powered by the core engine. In one embodiment, the clutch includes reverse gearing to reverse rotational output of the fan. In one embodiment, the clutch and reverse gearing are implemented in an epicyclic gear system.

First claim

The invention claimed is:

1. A gas turbine engine comprising:
a core engine;
a fan driven by the core engine;
a bypass duct configured to receive airflow from the fan;
a clutch linking the core engine and the fan; and
an epicyclic gear system coupling the clutch to the fan, the epicyclic gear system comprising:
a sun gear disposed at a center of the system;
a carrier concentrically surrounding the sun gear;
spur gears disposed within the carrier and engaged with the sun gear; and
a ring gear concentrically surrounding the carrier and engaged with the spur gears;

wherein the clutch comprises:
a spline collar configured to rotate with the ring gear or the carrier;
a spline ring anchored to ground; and
an actuator coupled to the spline collar and the spline ring, the actuator comprising:
a grounded lever coupled to the spline collar; and
a linkage connecting the lever and the spline ring; and

wherein the clutch switches the epicyclic gear between operating as a planet gear system and a star gear system by alternatively grounding the ring gear or the carrier.

2. The gas turbine engine of claim 1 , wherein the core engine comprises a two-spool reverse flow core, and wherein the two-spool reverse flow core exhausts to the bypass duct.

3. The gas turbine engine of claim 2 and further comprising:
a free turbine disposed between the core engine and the fan such that the free turbine is powered by the core engine and the clutch links the fan and the free turbine.

4. The gas turbine engine of claim 3 and further comprising:
a valve fluidly coupling the free turbine to the bypass duct.

5. The gas turbine engine of claim 3 and further comprising:
a vent duct fluidly coupling output of the free turbine with the bypass duct;
a transition duct fluidly coupling the free turbine and the core engine; and
a valve fluidly coupling the bypass duct and the transition duct.

6. The gas turbine engine of claim 1 , wherein the clutch reverses rotational output direction of the epicyclic gear system.

7. The gas turbine engine of claim 1 and further comprising an output shaft coupled to the clutch, wherein the clutch alternatively couples the output shaft to the ring gear or to the carrier.

Assignees

• United Technologies Corp

Inventors

• Penda Allan R
• Suciu Gabriel L
• Sheridan William G
• Lord Wesley K

Classifications

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F02C3/113

  with variable power transmission between rotors · CPC title

• F05D2260/40311

  of the epicyclical, planetary or differential type · CPC title

• F02C3/10

  with another turbine driving an output shaft but not driving the compressor · CPC title

• F02C3/145

  the combustion chamber being in the reverse flow-type · CPC title