PATENT CLAIM ANALYSIS

Application Number: 16027178
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-01
Patent Classification: ["244", "017170"]

Abstract:
The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.

Claim (Index 22):
A multi-rotor unmanned aerial vehicle (UAV), comprising:\n a housing having an outer surface and an inner surface, the inner surface defining a cavity, the housing having an \u201cX\u201d shaped arrangement and including:\n an upper body portion integrally formed from an upper central housing member and multiple upper branch housing members; and \n a lower body portion attached to the upper body portion and integrally formed from a corresponding lower central housing member and multiple corresponding lower branch housing members; \n a flight control module positioned in the cavity; a first landing stand attached to the outer surface of the housing at two corresponding attachment interfaces; a second landing stand attached to the outer surface of the housing at two corresponding attachment interfaces; a magnetometer attached to the first landing stand, and positioned at least 3 cm from the flight control module; a wire connected to the magnetometer and extending through an opening in one of the attachment interfaces of the first landing stand, and into the cavity; multiple actuator assemblies, with individual actuator assemblies including an actuator and a rotor, wherein an individual upper branch housing member and a corresponding individual lower branch housing member form an individual branch housing member, and wherein individual actuator assemblies are located at corresponding individual branch housing members; and multiple electronic speed controller (ESC) modules, with individual ESC modules coupled to corresponding individual actuator assemblies via corresponding electrical wires.

Metadata:
- Claim Count in Document: 4.0
- Percentile: 95.0
- Lexical Diversity: 1.37209
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['16005309', '14836344', '15947650', '14515357', '15175473']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8636444533913445
- 35 USC 102 Novelty (BERT): 0.5377664131728442
- Combined Prediction Score: 0.8310566493694945
- Mean Citation Score: 394.458492
- Max Citation Score: 415.89282
- Similarity Product: 343.36776734335183

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

Dataset: test