Aircraft Procedural Trainer Interface

US2017316712A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2017316712-A1
Application numberUS-201615375292-A
CountryUS
Kind codeA1
Filing dateDec 12, 2016
Priority dateApr 27, 2016
Publication dateNov 2, 2017
Grant date

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A control and simulation system (CSS) has a flight system configured to selectively provide flight mode of operation of an aircraft and a simulation system configured to selectively provide a simulation mode of operating the aircraft.

First claim

Opening claim text (preview).

What is claimed is: 1 . A control and simulation system (CSS), comprising: a flight system configured to selectively provide flight mode of operation of an aircraft; and a simulation system configured to selectively provide a simulation mode of operating the aircraft. 2 . The CSS of claim 1 , wherein the aircraft must be grounded prior to entering the simulation mode. 3 . The CSS of claim 1 , wherein the CSS is configured to poll a status of a weight on wheels sensor. 4 . The CSS of claim 1 , wherein the CSS is configured to determine whether an auxiliary ground power unit is connected to the aircraft. 5 . The CSS of claim 1 , wherein the CSS requires a passcode authentication prior to entering the simulation mode. 6 . The CSS of claim 1 , wherein at least one functionality of the aircraft in the flight mode is prevented from being utilized during operation of the aircraft in the simulation mode. 7 . The CSS of claim 1 , wherein the CSS is a ground-based system. 8 . The CSS of claim 7 , wherein the aircraft is simulated. 9 . The CSS of claim 7 , wherein the aircraft is configured so as not to be able to achieve flight. 10 . An aircraft, comprising: a control and simulation system (CSS), comprising: a flight system configured to selectively provide flight mode of operation of the aircraft; and a simulation system configured to selectively provide a simulation mode of operating the aircraft. 11 . The aircraft of claim 10 , wherein the aircraft must be grounded prior to entering the simulation mode. 12 . The aircraft of claim 10 , wherein the CSS is configured to poll a status of a weight on wheels sensor. 13 . The aircraft of claim 10 , wherein the CSS is configured to determine whether an auxiliary ground power unit is connected to the aircraft. 14 . The aircraft of claim 10 , wherein the CSS requires a passcode authentication prior to entering the simulation mode. 15 . The aircraft of claim 10 , wherein at least one functionality of the aircraft in the flight mode is prevented from being utilized during operation of the aircraft in the simulation mode. 16 . The aircraft of claim 10 , wherein the aircraft comprises a helicopter. 17 . The aircraft of claim 10 , wherein the aircraft comprises a tiltrotor aircraft. 18 . The aircraft of claim 10 , wherein the aircraft comprises an airplane.

Assignees

Inventors

Classifications

  • by projected image ({G09B9/307,} G09B9/36 take precedence) · CPC title

  • including display or recording of simulated flight path · CPC title

  • including aircraft sound simulation · CPC title

  • G09B9/46Primary

    the aircraft being a helicopter · CPC title

  • Simulation of view from aircraft · CPC title

Patent family

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External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2017316712A1 cover?
A control and simulation system (CSS) has a flight system configured to selectively provide flight mode of operation of an aircraft and a simulation system configured to selectively provide a simulation mode of operating the aircraft.
Who is the assignee on this patent?
Bell Helicopter Textron Inc
What technology area does this patent fall under?
Primary CPC classification G09B9/46. Mapped technology areas include Physics.
When was this patent published?
Publication date Thu Nov 02 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).