Aircraft flight data acquisition and transmission system
AssigneeTeledyne Technologies Incorporated
InventorsJohn Francis Grabowsky, David Ray Stevens
Life of this patent
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AssigneeTeledyne Technologies Incorporated
InventorsJohn Francis Grabowsky, David Ray Stevens
Estimating the term…
An aircraft data transmission system used with an aircraft having a data acquisition unit. The system includes a communications unit located in the aircraft and in communication with the data acquisition unit. The system also includes a cellular infrastructure in communication with the data communications unit after the aircraft has landed. The system further includes a data reception unit in communication with the cellular infrastructure.
An aircraft data transmission system, the aircraft having a data acquisition unit, comprising:
A data system for an aircraft, comprising:
An aircraft, comprising:
An aircraft data transmission system, the aircraft having a data acquisition unit, comprising:
A method of transmitting aircraft flight data from an aircraft, comprising:
A computer-implemented method of transmitting aircraft flight data from an aircraft, comprising:
A computer-implemented method of transmitting aircraft flight data from an aircraft, comprising:
A computer-implemented method of transmitting aircraft flight data from an aircraft, comprising:
A computer readable medium having stored thereon instructions which when executed by a processor, cause the processor to perform the steps of:
Dependencies are inferred from the claim text.
No related US applications are recorded in the indexed filing history.
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Equipment not otherwise provided for
Registering or indicating the working of vehicles: communicating information to a remotely located station
Arrangements for acquiring, generating, sharing or displaying traffic information: transmission of traffic-related information between aircraft…
Navigation or guidance aids: for control when on the ground, e.g. taxiing or rolling
Term ended 30 Jul 2018 (estimated)
USPTO file history isn’t available for this patent, so only indexed dates are shown.
(Not Applicable)
1. Field of the Invention
The present invention is directed generally to an aircraft flight data acquisition and transmission system and, more particularly, to an on-board cellular data transmission system.
For the present invention to be clearly understood and readily practiced, the present invention will be described in conjunction with the following figures, wherein:
FIG. 1 illustrates an aircraft data acquisition and transmission system;
FIG. 2 is a block diagram illustrating a more detailed embodiment of the system illustrated in FIG. 1;
It is to be understood that the figures and descriptions of the present invention have been simplified to illustrate elements that are relevant for a clear understanding of the present invention, while eliminating, for purposes of clarity, other elements found in a typical communications system. It can be recognized that other elements are desirable and/or required to implement a device incorporating the present invention. For example, the details of the cellular communications infrastructure, the Internet, and the public-switched telephone network are not disclosed. However, because such elements are well known in the art, and because they do not facilitate a better understanding of the present invention, a discussion of such elements is not provided herein.
FIG. 1 illustrates an aircraft data acquisition and transmission system 10. An aircraft 12, which has stored flight data, is illustrated after landing. The aircraft 12 transmits flight data as cellular communications signals to a cellular infrastructure 14. The cellular infrastructure 14 acts as a communications channel to the communications medium 16. A flight operations center 18 is connected to the medium 16 by any conventional connectivity medium such as, for example, a leased line. Once the cellular connections are made via the medium 16 data can flow bidirectionally from or to the aircraft.
FIG. 2 is a block diagram illustrating a more detailed embodiment of the system 10 illustrated in FIG. 1. The aircraft 12 includes a data system 19 having a data acquisition unit 20. The data acquisition unit 20 includes a digital flight data acquisition unit (DFDAU) processor 22, which includes a storage media for storing flight data in a digital format. The DFDAU processor 22 receives signals from sensors 24 which sense parameters such as air speed, altitude, vertical acceleration, heading, time, etc. The flight data are transferred to a communications unit 26 via a bus 28. The bus 28 is connected to an I/O interface 30 in the communications unit 26. The I/O interface 30 can be a standard bus interface such as, for example, an ARINC 429 bus interface.