Autofeather state maintenance

• US 4,845,617 A
• Filed: 06/01/1987
• Issued: 07/04/1989
• Est. Priority Date: 06/01/1987
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Kamenetz, Jeffry K., Simmons, Howard E.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black, Thomas G.
• Application Number:
  US07/057,069
• Time in Patent Office: 764 Days
• Field of Search: 364/424, 364/900, 360/5, 371/12
• US Class Current: 701/35
• CPC Class Codes: B64D 31/10 for preventing asymmetric thrust
• CPC Class Codes: G05D 1/0072 to counteract a motor failure

Abstract

Each engine of a multi-engine aircraft is monitored to determine if it has become inoperative during a critical flight mode such as takeoff or landing. If so, the propeller of the inoperative engine is feathered and the remaining engine or engines is uptrimmed. A "state machine" indicative of the various states of the aircraft is established and the present state of the aircraft is stored in a non-volatile memory; if an electrical power interruption occurs during a critical flight mode the identity of the present operating state may be quickly recalled for immediate refeathering of an inoperative engine and reuptrimming of the remaining engine or engines.

Claims

1. A method of controlling an aircraft, comprising the steps of:

monitoring one or more parameter signals indicative of one or more corresponding parameters relating to said aircraft;

identifying a present state of said aircraft according to predefined state criteria defined by the magnitudes of one or more of said monitored parameter signals, said present state being one of a plurality of predefined operating states of said aircraft;

storing said present state signal in a nonvolatile storage medium;

providing one or more control signals for said aircraft at least partially in response to said present state signal; and

checking for the presence of electrical power, and, upon detection of a restoration of electrical power after an interruption, retrieving said stored present state signal from said nonvolatile storage medium and providing one or more control signals to said aircraft at least partially in response to said retrieved present state signal.

2. The method of claim 1, wherein said nonvolatile storage medium comprises electrically erasable programmable read only memory.

3. A method of controlling an aircraft, comprising the steps of:

retrieving a signal from a nonvolatile storage medium, said retrieved signal being indicative of a last state of said aircraft, said last state being one of a plurality of predefined operating states of said aircraft;

monitoring one or more parameter signals indicative of one or more corresponding parameters relating to said aircraft;

identifying a present state of said aircraft according to predefined state criteria defined by the magnitudes of one or more of said monitored parameter signals;

providing a signal indicative of said present state;

comparing said last state signal to said present state signal to determine whether a difference exists therebetween, and, upon determination of such a difference, storing said present state signal in said nonvolatile storage medium whereby said stored present state signal is indicative of the last state of said aircraft; and

checking for the presence of electrical power, and, upon detection of a restoration of electrical power after an interruption, retrieving said stored present state signal indicative of the last state of said aircraft from said nonvolatile storage medium and providing one or more control signals to said aircraft at least partially in response thereto.

4. The method of claim 3, wherein said nonvolatile storage medium comprises electrically erasable programmable read only memory.

5. Apparatus for controlling an aircraft, comprising:

sensor means for sensing the magnitudes of one or more aircraft parameters, and for providing sensed signals indicative of the current magnitudes thereof;

nonvolatile storage means for storing signal indicative of a plurality of predefined operating states of said aircraft; and

signal processing means, responsive to said sensed parameter signals, for providing a signal indicative of a present state of said aircraft, said present state signal defined according to predefined state criteria defined by the magnitudes of one or more of said sensed parameter signals, for storing said present state signal in said nonvolatile storage means, for providing one or more control signals to said aircraft at least partially in response to said present state signal, and for checking for the presence of electrical power, and, upon detection of a restoration of electrical power after an interruption, for retrieving said stored present state signal from said nonvolatile storage medium and for providing one or more control signals to said aircraft at least partially in response to said retrieved present state signal.

6. The apparatus of claim 5, wherein said nonvolatile storage means comprises electrically erasable programmable read only memory.

7. Apparatus for controlling an aircraft, comprising:

sensor means for sensing the magnitudes of one or more aircraft parameters, and for providing sensed signals indicative of the current magnitudes thereof;

nonvolatile storage means for storing signals indicative of a plurality of predefined operating states of said aircraft; and

signal processing means, responsive to said sensor means, for retrieving a signal from said nonvolatile storage means indicative of a least state of said aircraft, for providing a signal indicative of a present state of said aircraft, said present state signal defined according to predefined state criteria defined by the magnitudes of one or more of said sensed parameter signals, for comparing said last state signal to said present state signal to determine whether a difference exists therebetween, and, upon the determination of such a difference, for storing said present state signal in said nonvolatile storage means whereby said stored present state signal is indicative of the last state of said aircraft, and for checking for the presence of electrical power, and, upon detection of a restoration of electrical power after an interruption, for retrieving said stored last state signal from said nonvolatile storage medium and for providing one or more control signals to said aircraft at least partially in response to said retrieved last state signal.

8. The apparatus of claim 7, wherein said nonvolatile storage means comprises electrically erasable programmable read only memory.