Engine assembly with direct drive of generator
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
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Jun 12, 2018
Issued Date -
N/A
app pub date -
Jun 7, 2017
filing date -
Jun 25, 2015
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
An engine assembly for use as an aircraft auxiliary power unit, having internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the internal combustion engine inlet, and a turbine having an inlet in communication with the internal combustion engine outlet. The turbine may be a first stage turbine, and the assembly may include a second stage turbine having an inlet in communication with the first stage turbine outlet. A method of providing electrical power to an aircraft is also discussed.
First Claim
Family
International Classification(s)
- H02K:DYNAMO-ELECTRIC MACHINES
- H02P:CONTROL OR REGULATION OF ELECTRIC MOTORS, GENERATO....
- B64D:EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SU....
- F02C:GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION....
- F01C:ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR EN....
- F01D:NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g....
- F03G:SPRING, WEIGHT, INERTIA, OR LIKE MOTORS; MECHANICA....
- [Classification Symbol]
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