Abstract: A system for starting a gas turbine engine includes a rotor drive system and a hydraulic motor system operatively connected to the rotor drive system. A gas turbine engine is operatively connected to the hydraulic motor system for starting the gas turbine engine. A method for starting an engine includes initiating single-engine-operation on a multi-engine aircraft. Single-engine operation includes operating a first engine and powering down a second engine. The method includes running a hydraulic motor system. The hydraulic motor system is driven by the rotor drive system and is operatively connected to the second engine. The method includes identifying a need to start the second engine and starting the second engine using the hydraulic motor system.

Abstract: In a gas turbine engine that includes a compressor and a combustor, wherein the combustor includes a primary fuel injector within a fuel nozzle and a secondary fuel injector that is upstream of the fuel nozzle and configured to inject fuel into a flow annulus of the combustor, a method for detecting a flame holding condition about a fuel injector. The method may include the steps of: detecting an upstream pressure upstream of the secondary fuel injector; detecting a downstream pressure downstream of the secondary fuel injector; determining a measured pressure difference between the upstream pressure and the downstream pressure; and comparing the measured pressure difference to an expected pressure difference.

Abstract: A vehicle control system is programmed to stop the vehicle's internal combustion engine upon certain conditions including the vehicle being stopped and engine temperature having reached a minimum operating level. On vehicles equipped with air brakes and having an engine driven air compressor, engine restarts are provided by an air pressure supported hydraulic motor once triggered by operator actions such as releasing the brake and/or depressing the vehicle's accelerator indicative of the driver's intention to move the vehicle.

Abstract: A starter drive assembly includes a starter output shaft having a plurality of circumferentially-spaced axial grooves, a clutch assembly, and a barrel assembly. The clutch assembly includes a clutch plate configured to engage the axially grooves of the output shaft such that the output shaft and the clutch plate rotate together during an engine starting operation. The clutch assembly further includes a screw shaft selectively matingly couplable to the clutch plate, wherein the screw shaft is configured to engage the clutch plate during rotation in a first direction and disengage the clutch plate in a second direction such that the screw shaft and the clutch plate rotate together in the first direction. The barrel assembly includes a first end configured to threadably engage the screw shaft, and a second end that includes a pinion gear configured to engage the ring gear during the engine starting operation.

Abstract: A method of starting an engine with an engine starter that includes pressurizing a motor supply chamber with a fluid, selectively pressurizing an actuating chamber in response to the pressure in the motor supply chamber, moving a first valve along a first axis in response to pressure in the actuating chamber and moving a pinion toward engagement with the engine in response to movement of the first valve. The method further includes further pressurizing the actuating chamber, moving a second valve along a second axis in response to the further pressure in the actuating chamber, rotating the pinion in response to movement of the second valve, meshing pinion teeth with teeth on the engine, and starting the engine in response to rotation of the pinion.

Abstract: A redundant engine starting system is disclosed that includes at least first and second sub-starters that rotate corresponding sub-starter output shafts affixed by a joining gear to rotate an engine starter shaft to start the engine. Each sub-starter includes a speed sensor for detecting rotational speed of the sub-starter, and a control valve to control rotational speed of the sub-starter. A system control intelligence interprets sensed rotational speeds of the sub-starters and commands the control valves, so that the control valve of an operative sub-starter is commanded to allow increased rotational speed of the sub-starter and therefore its corresponding output shaft whenever the system control intelligence interprets the sensed rotational speed of an inoperative sub-starter.

Abstract: Engine pre-engage starters formed of compactly interfit sections featuring a universally applicable high speed turbine rotor, formed preferably of nylon based plastic, the body of which is distinguished by low tensile strength, high impact resistance, radial growth and adjustment in correspondence with the speed of its rotation, minimal evidence of stress and no material fracture even under the most adverse conditions of its use and a structural composition which reduces to powder form when subjected to friction at such time the speed of its rotation reaches and exceeds a prescribed limit. The rotor is so connected with its power transmission shaft to position beyond and form an axial extension of one end thereof. The rotor is contained by a peripherally encompassing structurally complementary plastic buffer which enhances its fail safe properties. Optionally, the starter housing may be provided with discretely positioned sound deadening inserts.

Abstract: The disclosed electrically controlled starter valve (10) regulates the flow of compressed gas to an air turbine starter (11) and precisely controls the way in which the flow is reduced after start of the aircraft engine. The electronic control system (30) is responsive to previously uncompensated for engine system variables. The main valve is a butterfly valve (12) controlled by an air actuator (14). A solenoid valve (16) in the air supply line (15, 17) to the actuator (14) is switched on and off at discrete intervals to provide for positioning of the butterfly valve (12). A position transducer (R2) senses position of the butterfly valve (12) and provides a position feedback signal. A pressure transducer (R1) senses pressure at the inlet to the butterfly valve (12) and provides an inlet pressure feedback signal. The position and pressure feedback signals are fed to an electronic control circuit (30) and are used to compensate for changing conditions to provide a consistent valve (12) closing pattern.

Abstract: Starting method for an internal combustion engine at least one cylinder whereof is equipped with a starting valve connected to a source of compressed fluid, said fluid being introduced into the cylinder or cylinders when the pistons are in the combustion phase of the engine cycle, whereby the opening lead of the exhaust valve or valves of each cylinder equipped with a starting valve is temporarily reduced to improve utilization of the energy contained in the starting fluid.

Abstract: A method of improving the effectiveness of braking a reversible four-stroke V type Diesel engine with an even number of at least ten working cylinders fitted with individual starting valves sequentially fed from an engine-driven rotary pressure air distributor, the method consisting in reducing the duration of pressure air inlet to the distributor for one bank of cylinders with respect to the other bank and optimizing such a shortened duration for each starting valve of one bank of cylinders during the braking step and possibly optimizing that for each starting valve of the other bank of cylinders for the restarting step.

Abstract: A radial motor powered by pressurized gas is disclosed as used for starting the internal combustion engine of a portable implement such as a powered chain saw or lawn mower. The motor is designed for economical manufacture and assembly, durability, and economy of gas used. It includes pistons formed of stiff resilient material that in assembly are snapped onto the outer ends of connecting rods and held in place during operation of the motor without the use of retaining rings, pivot pins or screws. The inner ends of these connecting rods are held in sockets in connecting rod mounting means either by the shapes of the sockets or by the resilience of either or both of the connecting rod and mounting means. The motor includes a rotatable valve driven by a free end of the crankshaft to feed gas to the cylinders.