PATENT CLAIM ANALYSIS

Application Number: 15747439
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["701", "003000"]

Abstract:
A method and system for designing a cooperatively-driven aircraft system. A cooperatively-driven aircraft system comprises an aircraft, a movable ground monitor station or a fixed ground monitor station, a data link of a composite data chain, and a relay communication device. A flight management system is disposed inside the aircraft. The aircraft is connected to the movable ground monitor station or the fixed ground monitor station by means of the radio data link of the composite data chain. Telemetering data information about the flight management system is issued to the movable ground monitor station or the fixed ground monitor station by means of the composite data chain. A manned aircraft technology and an unmanned aerial vehicle system technology are combined, cooperative air and ground driving is constructed, and a new technology aircraft system integrating easy flight and safe flight is provided.

Claim (Index 5):
A cooperatively-driven aircraft system, wherein: the cooperatively-driven aircraft system comprises an aircraft, a movable ground monitor station or a fixed ground monitor station, a data link of a telemetering remote control and information transmission system or abbreviated as a composite data chain and a relay communication device; a flight management system is disposed inside the aircraft, a pilot uses a telex manipulation system to perform a flight, the flight management system performs automatic control of the flight in a signal activation way or in a flight task management way; the aircraft is connected to the movable ground monitor station or the fixed ground monitor station by means of the radio data link of the composite data chain, telemetering data information about the flight management system is issued to the movable ground monitor station or the fixed ground monitor station by means of the composite data chain, so that the ground monitor station monitors flight data or state of the aircraft; by means of the data link of the composite data chain, the movable ground monitor station or the fixed ground monitor station uploads control instructions or an executable predetermined airline to the flight management system of the aircraft to perform control of the flight of the aircraft, achieves cooperative air and ground driving; a plurality of movable ground monitor stations or fixed ground monitor stations is connected in a ground wired connection way, or by means of the radio data link of the composite data chain, to form a mutually communicated network system; the composite data chains of the aircraft are allowed to open data communication connecting to the composite data chains, forming a data sharing local area network, the flight management system is a central system of an on-board system of the aircraft, is formed by a flight management computer and a control apparatus; the flight management computer and units thereof in the flight management system are connected with the on-board system of the aircraft according to the following classification, to form a main operation system with mutual input and feedback;\n a first one is that the flight management computer and the units thereof in the flight management system are connected with a navigation monitor system, an engine parameter sensor and an undercarriage/airplane wheel parameter sensor as parameter sensor subsystems, to obtain input of data information of relevant monitoring parameters; a second one is that the flight management computer and the units thereof in the flight management system are connected with the composite data chain and a cabin integrated avionic system as monitor/manipulation subsystems, so that relevant data information and control data are communicated with each other for being displayed and operated on the aircraft, or are issued to the ground monitor station for use by the monitor personnel; a third one is that the flight management computer and the units thereof in the flight management system are connected with a flight control system, a thrust control system and a takeoff and landing control system as execution subsystems, wherein they output control data, perform control of corresponding control objects, the flight management computer and units thereof may be used in combination with the computer of the flight control system and again is used in combination with the computer of the thrust control system and the takeoff and landing control system to use on-board computer resources reasonably; a fourth one is that, units of the flight management computer in the flight management system, comprising an option display component or a control display component CDU, are on-board apparatuses or easily detachable mobile apparatuses, are human machine interaction interfaces for the pilot and the flight management computer, provide functions of displaying, inputting and modifying data or instructions.

Metadata:
- Claim Count in Document: 16.0
- Percentile: 94.0
- Lexical Diversity: 2.57627
- Patent Class: 701.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['13694746', '14121622', '13998833', '13420664', '12246681']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4677337546612569
- 35 USC 102 Novelty (BERT): 0.4857492345424514
- Combined Prediction Score: 0.4695353026493763
- Mean Citation Score: 229.569678
- Max Citation Score: 230.38179
- Similarity Product: 169.13591540242732

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 0
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test