IP Library Granted Patent US 12700315
Granted Patent B2
US 12700315 · App. 18/332,060 · Granted Aug 4, 2026

Aircraft modular data collection platform

Inventors: Nathan D. Hiller (Irvine, CA); Claudia E. Fritz-Thompson (Bothell, WA)
Assignee: The Boeing Company
G08G5/21B64D47/00G08G5/76B64C2211/00B64D43/00G01S13/953G01W1/08
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Quick Facts
Patent No.
US 12700315
App. No.
18/332,060
Granted
Aug 4, 2026
Kind
B2
Abstract

An aircraft data collection system comprising a set of removable data collection units and a computer system. The set of removable data collection units is loadable into a compartment in a commercial aircraft. The computer system is configured to control operation of the set of removable data collection units to collect data during a flight of the commercial aircraft on a flight path. A third party can use a smart phone or other electronic device to control the data collection unit during a commercial aircraft flight. The third party is different from the airline operating the commercial aircraft.

Claims (50)

1 . An aircraft data collection system comprising:

a set of removable data collection units that are loadable into a compartment comprising a cargo bay in a commercial aircraft, wherein a removable data collection unit in the set of removable data collection units comprises a removable container that is loadable in the compartment and a sensor system configured to collect data relating to conditions outside of the commercial aircraft, wherein the removable container has a set of ports and a power connection configured to connect to a power source in the commercial aircraft; and

a computer system configured to control operation of the set of removable data collection units to collect data during a flight of the commercial aircraft on a flight path.

2 . The aircraft data collection system of claim 1 , wherein the computer system controls operation of the set of removable data collection units in response to instructions from a third party that is different from an airline operating the commercial aircraft.

3 . The aircraft data collection system of claim 1 , wherein the sensor system is a weather data sensor system configured to collect weather data.

4 . The aircraft data collection system of claim 3 , wherein the removable container has a shape that corresponds to a cross section of the cargo bay and conforms to an inner wall of the cargo bay.

5 . The aircraft data collection system of claim 3 , wherein the cargo bay has a set of ports selected from at least one of a window or a launch tube.

6 . The aircraft data collection system of claim 1 , wherein the removable container is loadable in a space of the compartment that has been reserved.

7 . The aircraft data collection system of claim 1 , wherein the sensor system is selected from at least one of a visible camera system, an infrared camera system, a dropsonde system, or a weather radar system.

8 . The aircraft data collection system of claim 1 , wherein the set of removable data collection units is a set of removable weather data collection units configured to:

detect parameters in an atmosphere during the flight of the commercial aircraft along the flight path; and

generate weather data from the parameters detected.

9 . The aircraft data collection system of claim 1 , wherein the compartment is a cargo bay, and wherein the sensor system comprises:

dropsondes in the removable container, wherein the dropsondes are configured to be dropped, via a dropsonde launch system, from the commercial aircraft during the flight of the commercial aircraft along the flight path; and

wherein the computer system is further configured to receive weather data from the dropsondes and send the weather data to a storage system.

10 . The aircraft data collection system of claim 9 , wherein the weather data is at least one air temperature data, sea temperature data, pressure data, humidity data, turbulence data, wind speed measurements, wind direction data, geolocation, or images.

11 . The aircraft data collection system of claim 1 , wherein the computer system comprises computing devices located in at least one of the set of removable data collection units, a ground location, or the commercial aircraft.

12 . The aircraft data collection system of claim 1 , wherein the data is selected from at least one of weather data, economic data, or environmental data.

13 . The aircraft data collection system of claim 1 , wherein removable data collection units detect at least one of electromagnetic waves in an infrared spectrum, optical data, radio frequency regions of an electromagnetic spectrum, communications data, or radio frequency signals.

14 . A method for collecting data, the method comprising:

loading a set of removable data collection units in a compartment comprising a cargo bay in a commercial aircraft, wherein a removable data collection unit in the set of removable data collection units comprises a removable container that is loadable in the compartment and a sensor system configured to collect data relating to conditions outside of the commercial aircraft, wherein the removable container has a set of ports and a power connection configured to connect to a power source in the commercial aircraft; and

collecting, by a computer system, the data during a flight of the commercial aircraft along a flight path using the set of removable data collection units.

15 . The method of claim 14 , wherein said collecting the data comprises:

detecting parameters in an atmosphere during the flight of the commercial aircraft along the flight path using the set of data collection units; and

generating weather data from the parameters detected.

16 . The method of claim 14 , wherein the sensor system comprises dropsondes in the removable container, and wherein said collecting the data comprises:

dropping the dropsondes into an atmosphere from the removable container during the flight of the commercial aircraft along the flight path;

receiving weather data from the dropsondes; and

sending the weather data received from the dropsondes to a storage system.

17 . The method of claim 14 , wherein the removable container is loadable in the cargo bay and the sensor system is a weather data sensor system configured to collect weather data.

18 . The method of claim 17 , wherein the removable container has a shape that corresponds to a cross section of the cargo bay and conforms to an inner wall of the cargo bay.

19 . The method of claim 17 , wherein the weather data sensor system is selected from at least one of a visible camera system, an infrared camera system, a dropsonde system, or a weather radar system.

20 . The method of claim 14 , wherein the data is selected from at least one of weather data, economic data, or environmental data.

21 . The method of claim 14 , wherein the compartment has a set of ports selected from at least one of a window or a launch tube.

22 . The method of claim 14 , wherein the computer system comprises computing devices located in at least one of the set removable data collection units, a ground location, or the commercial aircraft.

23 . The method of claim 14 , wherein the data is at least one of air temperature data, sea temperature data, pressure data, humidity data, turbulence data, wind speed measurements, wind direction data, geolocation, or images.

24 . The method of claim 14 , wherein the set of removable data collection units detect at least one of electromagnetic waves in an infrared spectrum, optical data, radio frequency regions of an electromagnetic spectrum, communications data, or radio frequency signals.

25 . An aircraft data collection system comprising:

a set of data collection units configured for use in a compartment comprising a cargo bay in a commercial aircraft, wherein the set of data collection units have a set of ports and a power connection configured to connect to a power source in the commercial aircraft; and

a computer system configured to control operation of the set of data collection units to collect data during a flight of the commercial aircraft on a flight path, wherein the computer system controls operation of the set of data collection units in response to instructions from a third party that is different from an airline operating the commercial aircraft.

26 . The aircraft data collection system of claim 25 , wherein the instructions from the third party are transmitted to the computer system from a computing device operated by the third party.

27 . The aircraft data collection system of claim 26 , wherein the computing device is selected from a group comprising a smartphone, a tablet, a phone, a laptop computer, and a desktop computer.

28 . The aircraft data collection system of claim 26 , wherein the computing device is located in a location selected from a group comprising a drone and a satellite.

29 . The aircraft data collection system of claim 28 , wherein drone is selected from a group comprising an aerial drone, an underwater drone, a surface drone, and a land-based drone.

30 . A method for collecting data, the method comprising:

receiving, by a computer system, instructions from a third party to operate a set of data collection units in a compartment comprising a cargo bay in a commercial aircraft, wherein the set of data collection units have a set of ports and a power connection configured to connect to a power source in the commercial aircraft; and

collecting, by the computer system, the data during a flight of the commercial aircraft along a flight path using the set of data collection units in response to receiving the instructions from the third party that is different from an airline operating the commercial aircraft.

31 . The method of claim 30 , wherein the third party is located in a location selected from a group comprising the commercial aircraft, a ground, and another aircraft.

32 . The method of claim 30 , wherein the instructions are sent from the third party using a handheld device selected from a group comprising a smartphone, a tablet, a phone, and a laptop computer.

33 . The method of claim 30 , wherein instructions from the third party are sent to an intermediator followed by transmission to the computer system, wherein the intermediator is selected from a group comprising a drone and a satellite.