Fan R. P. M. control loop stabilization using high rotor speed

• US 4,104,876 A
• Filed: 12/02/1976
• Issued: 08/08/1978
• Est. Priority Date: 04/23/1976
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Larsen, Hals N., Kamber, Peter W.
• Primary Examiner(s): Garrett, Robert E.
• Application Number:
  US05/746,649
• Time in Patent Office: 614 Days
• Field of Search: 60/226 R, 60/262, 60/39.16 R, 60/39.28 R, 60/39.28 T
• US Class Current: 60/226.1
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F02C 9/56 with power transmission control
• CPC Class Codes: F05D 2270/023 of different spools or shafts
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A fan spool stabilization loop which improves the stability of the low speed or fan spool in a two spool turbofan engine. In a preferred embodiment, the actual rate of rotation of the high speed spool is compared with the desired rate of rotation determined by integrating the difference between the desired rate of rotation of the fan spool and the actual rate of rotation. The difference therebetween controls the flow of fuel to the turbofan engine. In an alternate preferred embodiment of the invention, the rate of change of rotation of the high speed spool is added to the actual rate of rotation of the fan spool and the result is compared with the desired rate of rotation of the fan spool. The difference therebetween is utilized to control the flow of fuel to the turbofan engine.

Claims

1. In a twin spool turbofan engine having a high speed spool, a fan spool, and fuel controller, a fan spool control loop stabilization system comprising:

means for generating a first speed dependent signal as a function of fan spool speed of rotation;

means for generating a second speed dependent signal as a function of the rate of change of the high speed spool speed of rotation;

signal summing means for adding said first speed dependent signal to said second speed dependent signal;

means for comparing said sum with a signal indicative of a desired fan spool speed of rotation and producing therefrom an error signal porportional to the difference therebetween; and

,

means for adjusting the flow of fuel to said turbofan engine from said fuel controller in response to said difference signal such that the rotation of the fan spool is equivalent to and stable with said desired fan spool speed of rotation.

2. The apparatus of claim 1 wherein said means for generating a first speed dependent signal comprises a magnetic pick-up contained within said turbofan engine and a magnetic element contained within the fan blades of said fan spool such that said magnetic pick-up senses the revolution of the fan blades and produces a signal proportional to the rate therewith.

3. The apparatus of claim 1 wherein said means for generating a second speed dependent signal comprises an operational amplifier such that the output signal from said amplifier is the differentiation of the input signal.

4. The apparatus of claim 1 wherein said signal summing means comprises an operational amplifier.

5. The apparatus of claim 1 wherein said comparing means comprises an operational amplifier.

6. The apparatus of claim 1 wherein said means for adjusting the flow of fuel to said turbofan engine comprises a torque motor adapted to control a fuel meter valve wherein said torque motor adjusts the fuel meter valve in response to said difference signal.