Control method for optimizing exploitation costs of an engine aerodyne such as aircraft in the climb phase

• US 4,827,417 A
• Filed: 09/09/1985
• Issued: 05/02/1989
• Est. Priority Date: 09/10/1984
• Status: Expired due to Term

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Berger, Dominique, Rivron, Vincent
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black, Thomas G.
• Application Number:
  US06/773,813
• Time in Patent Office: 1,331 Days
• Field of Search: 364/433, 364/442, 364/431.07, 364/427-428, 244/180, 244/182, 73/178 T
• US Class Current: 701/5
• CPC Class Codes: G05D 1/0005 with arrangements to save energy
• CPC Class Codes: G05D 1/0607 specially adapted for aircraft

Abstract

There is proposed a method of controlling an engine aerodyne in the climb phase, wherein a velocity variation law as a function of altitude is imposed. Moreover, there is set a law of variation of the engine speed corresponding generally to progerssive decrease in such speed as altitude increases. Optimization of exploitation costs in the climb phase can be reached mainly by taking into account the engine maintenance costs by means of a wear model.

Claims

1. A method of piloting an aerodyne with an engine, in the climb phase, with the aerodyne having means to adjust the velocity of the aerodyne and the speed of the engine comprising the steps of

varying the velocity of the aerodyne in accordance with the increase in altitude of the aerodyne;

maintaining the speed of the engine for at least a portion of the climb at a greater rate of speed than the maximum authorized engine speed for a constant engine speed climb, as authorized for the engine in said aerodyne;

and varying the speed of the engine by progressively decreasing the speed of the engine from the greater than maximum authorized engine speed as the altitude of the aerodyne increases.

2. The method of claim 1, wherein the step of varying the velocity of the aerodyne includes the steps of increasing the velocity of the aerodyne and then decreasing the velocity of the aerodyne with the increase in altitude of the aerodyne.

3. The method of claim 1, wherein the steps of varying the velocity of the aerodyne and varying the speed of the engine are varied as a function of minimizing the sum of fuel costs, flight duration costs, and engine maintenance costs.

4. The method of claim 1, wherein the steps of varying the velocity of the aerodyne and varying the speed of the engine are varied as a function of time during the climb from a damage curve giving cost per time unit under given engine operating conditions.

5. A method of piloting an engine aerodyne in the climb phase having adjustable velocity and adjustable engine speed, comprising changing said velocity of said aerodyne according to altitude thereof, based on a first variation law as well as changing said engine speed, based on a second variation law corresponding substantially to progressive decrease in such engine speed as altitude increases, said engine speed, at least for a portion of the climb, remaining higher than maximum authorized engine speed for a constant engine speed climb, said laws imposed upon velocity and engine speed as functions of the altitute being defined so as to minimize the exploitation costs of the aerodyne during the climb, the first variation velocity and the second variation speed laws being defined so as to minimize the sum of the fuel costs, the flight duration costs and the engine maintenance costs.

6. A method according to claim 5, wherein the maintenance cost is defined as the integral, as a function of time during the climb, of a damage curve giving a cost per time unit under given engine operating conditions.

7. A method according to claim 5, wherein the variation laws imposed upon velocity and engine speed are redefined at least once during the climb mainly as a function of the external environmental parameters.