Start-Up Control For a Compact Lightweight Turbine

• US 20100132365A1
• Filed: 12/03/2009
• Published: 06/03/2010
• Est. Priority Date: 04/20/2004
• Status: Abandoned Application

• Current Assignee: Mandolin Financial Properties Inc.
• Original Assignee: Mandolin Financial Properties Inc.
• Inventors: Labala, Gustavo Francisco
• Application Number:
  US12/630,513
• Publication Number:
  US 20100132365A1
• Time in Patent Office: Days
• US Class Current: 60/776
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F02C 7/26 Starting; Ignition
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

In a turbo-engine system, oil is circulated by means of a positive-displacement pump directly driven by the output shaft. The pump output pressure is monitored to trigger fuel injection when the turbine reaches sufficient speed during the start-up sequence.

Claims

1. A method for controlling the start-up sequence of a turbo-engine, said turbo-engine including:

a rotary shaft and other moving parts,

a combustion chamber for driving said rotary shaft and adapted for fuel to be injected therein,

an oil circulation system for lubricating said moving parts, said system including an oil pump directly coupled to said rotary shaft for circulating the oil through said system under pressure,

starter means for driving rotation of said rotary shaft during said start-up sequence and

means for turning said starter means on upon initiation of said start-up sequence;

said method comprising;

monitoring said oil circulation pressure,

deriving a logical signal indicative of whether said oil pressure is above or below a predetermined threshold and

using said derived logical signal to trigger fuel injection into said combustion chamber during said start-up sequence in response to said logical signal exceeding the predetermined threshold.

2. The method of claim 1, wherein said logical signal is an electrical signal.

3. The method of claim 1, wherein said predetermined oil-pressure threshold is greater than zero and less than a normal oil-circulation pressure after said start-up sequence is terminated.

4. A turbo-engine including:

a rotary shaft and other moving parts,

an oil circulation system for lubricating said moving parts, said system including an oil pump coupled to said rotary shaft for circulating the oil through said system under pressure,

starter means for driving rotation of said rotary shaft during said start-up sequence,

means for turning said starter means on upon initiation of said start-up sequence,

a switch arranged to trip during said start-up sequence in response to the pressure of the oil in said system increasing above a predetermined threshold and

means responsive to said switch tripping to trigger the fuel injection system on during said start-up sequence.

5. The turbo-engine of claim 4, wherein said switch comprises a calibrated bulb coupled to said oil pump.

6. The turbo-engine of claim 5, wherein said calibrated bulb coupled to the outlet of the oil pump.

7. The turbo-engine of claim 4, wherein said oil pump is a positive-displacement pump directly coupled to said rotary shaft.

8. The turbo-engine of claim 4, wherein said oil pump is coupled to said rotary shaft through a gearbox mechanism.

9. In a turbo-engine including a combustion chamber and means for injecting fuel into said combustion chamber a finite time after said turbo-engine is started, the use of means monitoring oil pressure in the turbo-engine to initiate fuel injection in response to the oil reaching a preset pressure in the turbo engine.