IN-FLIGHT MECHANICALLY ASSISTED TURBINE ENGINE STARTING SYSTEM
First Claim
1. An engine starting system for a rotary wing aircraft, comprising:
- a controller that receives a signal indicative of a start command for an engine;
a transmission input module that is mechanically coupled to a transmission system and an accessory gearbox; and
a starter motor that is mechanically coupled to a compressor drive shaft of the engine.
1 Assignment
0 Petitions
Accused Products
Abstract
An engine starting system for a rotary wing aircraft includes a controller that receives a signal indicative of a start command for an engine, a transmission input module that is mechanically coupled to a transmission system and an accessory gearbox and a starter motor that is mechanically coupled to a compressor drive shaft of the engine. Also, a method for restarting an engine in flight includes receiving by a controller a signal indicative of a start command for the engine, determining by the controller that an overrunning clutch is coupled to the engine, transmitting by a transmission system motive power to the engine in response to the determining that the overrunning clutch is coupled to the engine and driving via a compressor drive shaft a compressor section of the engine according to a design speed.
23 Citations
28 Claims
-
1. An engine starting system for a rotary wing aircraft, comprising:
-
a controller that receives a signal indicative of a start command for an engine; a transmission input module that is mechanically coupled to a transmission system and an accessory gearbox; and a starter motor that is mechanically coupled to a compressor drive shaft of the engine. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
-
-
17. A method for restarting an engine in flight for a rotary wing aircraft, comprising:
-
receiving by a controller a signal indicative of a start command for the engine; determining by the controller that an overrunning clutch is coupled to the engine; transmitting by a transmission system motive power to the engine in response to the determining that the overrunning clutch is coupled to the engine; and driving via an compressor drive shaft a compressor section of the engine according to a design speed. - View Dependent Claims (18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28)
-
Specification