Method and device for sharing data between on-board systems in an aircraft
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G01C-023/00
G05D-001/00
G05D-003/00
G06F-007/00
G06F-017/00
G06F-007/70
G06F-019/00
G06G-007/00
G06G-007/76
G07C-005/08
G08G-005/00
출원번호
US-0539354
(2009-08-11)
등록번호
US-8996201
(2015-03-31)
우선권정보
FR-08 55652 (2008-08-20)
발명자
/ 주소
Vial, Jean-Sebastien
출원인 / 주소
Airbus Operations SAS
대리인 / 주소
Oblon, McClelland, Maier & Neustadt, L.L.P.
인용정보
피인용 횟수 :
1인용 특허 :
13
초록▼
A method and a device are disclosed for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft, in order to permit one of the systems to determine the consequences of an event detected in the other of the systems. After at least one event
A method and a device are disclosed for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft, in order to permit one of the systems to determine the consequences of an event detected in the other of the systems. After at least one event has been detected in one of the technical management and mission management systems of the aircraft, at least one information item pertaining to the detected event is transmitted to the other of the technical management and mission management systems of the aircraft. The consequences of the event detected in the other of the technical management and mission management systems of the aircraft are then determined. The adaptation of at least one datum of the other of the technical management and mission management systems of the aircraft is evaluated in response to the determination.
대표청구항▼
1. A method for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft to permit each of the systems to determine consequences of an event detected in the other of the systems, the event including a fault detection, a datum received from
1. A method for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft to permit each of the systems to determine consequences of an event detected in the other of the systems, the event including a fault detection, a datum received from an aircraft or external system, or a datum acquired by a pilot, the technical management system and the mission management system are independent of each other so that the technical management system manages technical management data and the mission management system manages mission management data, the method comprising: detecting, in one of the technical management system and the mission management system of the aircraft, at least one event including the fault detection, the datum received from the aircraft or external system, or the datum acquired by the pilot;transmitting, from each one of the technical management system and the mission management system, at least one information item pertaining to the detected event to the other of the technical management system and the mission management system of the aircraft;determining, in the other of the technical management system and the mission management system of the aircraft, consequences of the detected event;evaluating, by the mission management system, whether at least one datum in the mission management data managed by the mission management system should be adapted based on the at least one information item pertaining to the detected event, when the technical management system transmits the at least one information item pertaining to the detected event; andevaluating, by the technical management system, whether at least one datum in the technical management data managed by the technical management system should be adapted based on the at least one information item pertaining to the detected event, when the mission management system transmits the at least one information item pertaining to the detected event. 2. The method according to claim 1, further comprising: modifying the at least one datum of the other of the technical management system and the mission management system of the aircraft in response to the evaluating of the adaptation of the at least one datum. 3. The method according to claim 1, further comprising: displaying the evaluation of the adaptation of the at least one datum of the other of the technical management system and the mission management system of the aircraft. 4. The method according to claim 3, further comprising: validating the evaluation of the adaptation of the at least one datum of the other of the technical management system and the mission management system of the aircraft. 5. The method according to claim 4, wherein the displaying further comprises displaying an activatable representation of a control command of at least one device of at least one of the technical management system and the mission management system of the aircraft, and the validating further comprises activating the control command. 6. The method according to claim 4, wherein the displaying and validating are employed in a centralized software interface of the technical management system and the mission management system of the aircraft. 7. The method according to claim 1, further comprising: analyzing the detected event, and the transmitting of the at least one information item pertaining to the detected event is effected in response to the analyzing. 8. The method according to claim 1, further comprising: determining a state of the aircraft;determining the consequences of the detected event as a function of the state; andevaluating the adaptation of the at least one datum as a function of the state. 9. A device for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft to permit each of the systems to determine consequences of an event detected in the other of the systems, the event including a fault detection, a datum received from an aircraft or external system, or a datum acquired by a pilot, the technical management system and the mission management system are independent of each other so that the technical management system manages technical management data and the mission management system manages mission management data, the device comprising: a detecting section, in one of the technical management system and the mission management system of the aircraft, configured to detect at least one event including the fault detection, the datum received from the aircraft or external system, or the datum acquired by the pilot;a transmitter configured to transmit, from each one of the technical management system and the mission management system, at least one information item pertaining to the detected event to the other of the technical management system and the mission management system of the aircraft;a determining section, in the other of the technical management system and the mission management system of the aircraft, configured to determine consequences of the detected event; andan evaluating section configured to evaluate when the technical management system transmits the at least one information item pertaining to the detected event, whether at least one datum in the mission management data managed by the mission management system should be adapted based on the at least one information item pertaining to the detected event, andwhen the mission management system transmits the at least one information item pertaining to the detected event, whether at least one datum in the technical management data managed by the technical management system should be adapted based on the at least one information item pertaining to the detected event. 10. An aircraft system in an aircraft for exchanging data between a technical management system of the aircraft and a mission management system of the aircraft to permit each of the technical management and mission management systems to determine consequences of an event detected in the other of the systems, the event including a fault detection, a datum received from an aircraft or external system, or a datum acquired by a pilot, the technical management system and the mission management system are independent of each other so that the technical management system manages technical management data and the mission management system manages mission management data, the aircraft system comprising: a detecting section, in one of the technical management system and the mission management system of the aircraft, configured to detect at least one event including the fault detection, the datum received from the aircraft or external system, or the datum acquired by the pilot;a transmitter configured to transmit, from each one of the technical management system and the mission management system, at least one information item pertaining to the detected event to the other of the technical management system and the mission management system of the aircraft;a determining section, in the other of the technical management system and the mission management system of the aircraft, configured to determine consequences of the detected event; andan evaluating section configured to evaluate when the technical management system transmits the at least one information item pertaining to the detected event, whether at least one datum in the mission management data managed by the mission management system should be adapted based on the at least one information item pertaining to the detected event, andwhen the mission management system transmits the at least one information item pertaining to the detected event, whether at least one datum in the technical management data managed by the technical management system should be adapted based on the at least one information item pertaining to the detected event. 11. The method according to claim 1, wherein: the technical management system includes a technical management interface having screens for the pilot to manage the technical management data, and the mission management system includes a mission management interface having screens for the pilot to manage the mission management data. 12. The device according to claim 9, wherein: the technical management system includes a technical management interface having screens for the pilot to manage the technical management data, and the mission management system includes a mission management interface having screens for the pilot to manage the mission management data. 13. The system according to claim 10, wherein: the technical management system includes a technical management interface having screens for the pilot to manage the technical management data, and the mission management system includes a mission management interface having screens for the pilot to manage the mission management data.
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이 특허에 인용된 특허 (13)
Kolb,Kurt; Jacobs,Kent; Jacobs,Darryl, Aircraft flight data management system.
Ching Ron ; Webster Lawrence ; Faivre Fran.cedilla.ois,FRX, Device for the control of an aircraft system in manual pilot mode using notably a head-up display.
Records Roger M. (Kent WA) Taylor John A. (Mercer Island WA) Shontz William D. (Renton WA) McKenzie William A. (Federal Way WA), System for creating a single electronic checklist in response to multiple faults.
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