IP Library Granted Patent US 12,546,262
Granted Patent B2
US 12,546,262 · App. 18/628,480 · Granted Feb 10, 2026

Predicting fuel burn and emissions for aircraft

Inventor: Samet Ayhan (Fairfax, VA)
Assignee: The Boeing Company
F02C9/26G06Q10/04G06Q10/0631G06Q50/40F02D2200/0625F05D2220/323F05D2270/31F05D2270/709
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Quick Facts
Patent No.
US 12,546,262
App. No.
18/628,480
Granted
Feb 10, 2026
Kind
B2
Abstract

A method for fueling an aircraft comprises (a) predicting a sequence of fuel-burn quantities over a planned flight based on at least one sequence of multivariate flight data recorded during a prior flight and on a hidden state of a trained machine. For each of a pre-selected series of prior flights, a corresponding sequence of multivariate flight data recorded during the prior flight is processed in a trainable machine to develop the hidden state, which minimizes an overall residual for replicating the fuel-burn quantities in each corresponding sequence. The method further comprises (b) summing the fuel-burn quantities over the planned flight to obtain a fueling estimate; and (c) fueling the aircraft based in part on the fueling estimate.

Claims (41)

1 . A method for fueling an aircraft, the method comprising:

predicting a sequence of fuel-burn quantities over a planned flight based on at least one sequence of multivariate flight data recorded during a prior flight and on a hidden state of a trained machine,

wherein for each of a pre-selected series of prior flights, a corresponding sequence of multivariate flight data recorded during the prior flight is processed in a trainable machine to develop the hidden state, which minimizes an overall residual for replicating the fuel-burn quantities in each corresponding sequence;

summing the fuel-burn quantities over the planned flight to obtain a fueling estimate; and

fueling the aircraft based in part on the fueling estimate.

2 . The method of claim 1 wherein, for each of the pre-selected series of prior flights, the corresponding sequence spans a climb phase, a cruise phase, and a descent phase of the prior flight.

3 . The method of claim 2 further comprising, for each of the pre-selected series of prior flights, adjusting the corresponding sequence to provide a common climb length for the climb phase, a common cruise length for the cruise phase, and/or a common descent length for the descent phase.

4 . The method of claim 3 wherein adjusting each corresponding sequence comprises padding the corresponding sequence in the climb phase, the cruise phase, and/or the descent phase.

5 . The method of claim 1 ,

wherein replicating the fuel-burn quantities comprises transforming the multivariate flight data from a previous time step in each corresponding sequence based on the hidden state, and

wherein predicting the sequence of fuel-burn quantities comprises transforming the multivariate flight data from a previous time step in the at least one sequence based on the hidden state.

6 . The method of claim 1 wherein at least the trained machine comprises a trained encoder arranged logically upstream of a trained decoder, wherein the encoder is trained to emit a vector that featurizes an input sequence of multivariate flight data, and wherein the decoder is trained to replicate the fuel-burn quantities of the input sequence based on the vector, thereby generating an output sequence.

7 . The method of claim 6 wherein the encoder and the decoder are configured according to a long short-term memory (LSTM) architecture.

8 . The method of claim 7 wherein at least the trained machine comprises an encoder-decoder LSTM (E-D LSTM) model, a convolutional neural-network (CNN) LSTM encoder-decoder (CNN LSTM E-D) model, or a convolutional LSTM encoder-decoder (ConvLSTM E-D) model.

9 . The method of claim 6 wherein at least the trained machine further comprises a fully connected layer configured to interpret the fuel burn quantities at each time step of the output sequence.

10 . The method of claim 1 wherein the at least one sequence and each corresponding sequence of multivariate flight data includes flight-data recorder (FDR) data selected via principle-component analysis.

11 . The method of claim 1 wherein the at least one sequence and each corresponding sequence of multivariate flight data includes atmospheric data.

12 . The method of claim 1 wherein the at least one sequence of multivariate flight data share a departure airport, an arrival airport, and an aircraft specifier of the planned flight.

13 . The method of claim 1 wherein the trainable machine, after development of the hidden state, is the trained machine.

14 . The method of claim 1 wherein the trainable machine is distinct from the trained machine, the method further comprising:

receiving, in the trained machine, a plurality of parameter values defining the hidden state as developed on the trainable machine.

15 . The method of claim 1 wherein the planned flight is one of a plurality of candidate flights of a plurality of candidate routes between a departure airport and an arrival airport, the method further comprising:

for each of the plurality of candidate flights:

predicting a sequence of fuel-burn quantities over the candidate flight based on at least one sequence of multivariate flight data recorded during a prior flight and on the hidden state of the trained machine, and

summing the fuel-burn quantities over the candidate flight to obtain a flight-wise fueling estimate;

for each of the plurality of candidate routes, summing every flight-wise fueling estimate along the candidate route to obtain a route-wise fueling estimate for the candidate route,

wherein the planned flight is a flight on the candidate route with a lowest route-wise fueling estimate.

16 . A trained machine comprising:

an input engine configured to receive at least one sequence of multivariate flight data recorded during a prior flight;

a prediction engine configured to predict a sequence of fuel-burn quantities over a planned flight based on at least one sequence of multivariate flight data recorded during a prior flight and on a hidden state of the trained machine,

wherein for each of a pre-selected series of prior flights, a corresponding sequence of multivariate flight data recorded during the prior flight is processed in a trainable machine to develop the hidden state, which minimizes an overall residual for replicating the fuel-burn quantities in each corresponding sequence

a summation engine configured to sum the fuel-burn quantities over the planned flight, to obtain a fueling estimate; and

an output engine configured to output the fueling estimate.

17 . The machine of claim 16 wherein the output engine is further configured to output an emissions estimate based on the fueling estimate.

18 . A trainable machine comprising:

an input engine configured to receive, for each of a pre-selected series of prior flights, a corresponding sequence of multivariate flight data recorded during the prior flight;

a training engine configured to process each corresponding sequence to develop a hidden state, which minimizes an overall residual for replicating the fuel-burn quantities in each corresponding sequence;

an output engine configured to expose at least a portion of the hidden state.

19 . The machine of claim 18 wherein each corresponding sequence includes flight-data recorder (FDR) data selected via principle-component analysis.

20 . The machine of claim 18 wherein for each of the pre-selected series of prior flights, the corresponding sequence spans a climb phase, a cruise phase, and a descent phase of the prior flight, the trainable machine further comprising:

an adjustment engine configured to adjust each corresponding sequence to provide a common climb length for the climb phase, a common cruise length for the cruise phase, and a common descent length for the descent phase.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 5, 2024
From: AYHAN, SAMET
To: THE BOEING COMPANY
Reel/Frame 067024/0041 →
Continuity (2)
Provisional Application 63600995 · Nov 20, 2023
Related Publication 20250163855A1 · May 22, 2025
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