PATENT CLAIM ANALYSIS

Application Number: 16130997
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-04
Patent Classification: ["244", "118100"]

Abstract:
In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.

Claim (Index 28):
The UAV of  claim 22 , wherein the payload is secured with a hinge.

Metadata:
- Claim Count in Document: 47.0
- Percentile: 97.0
- Lexical Diversity: 1.92683
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13730828', '15007206', '15829214', '15899214', '15851654']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8514090383775677
- 35 USC 102 Novelty (BERT): 0.5267293348127925
- Combined Prediction Score: 0.8189410680210901
- Mean Citation Score: 279.454378
- Max Citation Score: 352.61462
- Similarity Product: 251.2479546932745

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