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 9):
The cooperatively-driven aircraft system according to  claim 5 , wherein: the flight control system comprises a flight control computer, a controller and a control mechanism, is connected with a pneumatic control plane of a control object, performs control of respective pneumatic control planes, achieves control of the attitude and the airline of the aircraft; the thrust control system comprises a controller and a control mechanism, is connected with an engine accelerator of the control object, controls a thrust of an engine, cooperates with the flight control system to achieve control of an airline profile and a flight speed of the aircraft; the takeoff and landing control system comprises a controller and a control mechanism, is connected with an undercarriage operation device/an airplane wheel brake of the control object, cooperates with the flight control system to achieve control of landing and gliding of the aircraft; the flight management system performs combination control on the connected flight control system, the thrust control system and the takeoff and landing control system according to a control level or a control mode.

Metadata:
- Claim Count in Document: 16.0
- Percentile: 94.0
- Lexical Diversity: 2.57627
- Patent Class: 701.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['13694746', '14121622', '13998833', '13420664', '12246681']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4975073975160305
- 35 USC 102 Novelty (BERT): 0.4876299701617046
- Combined Prediction Score: 0.496519654780598
- Mean Citation Score: 229.569678
- Max Citation Score: 230.38179
- Similarity Product: 170.00718595134973

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