PATENT CLAIM ANALYSIS

Application Number: 16137368
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-01
Patent Classification: ["244", "118100"]

Abstract:
Particular embodiments include a non-dedicated, temporarily installed, airborne special mission payload mounting system comprising a pressurized door plug assembly installed in an opening on the side of an aircraft fuselage. A rotationally-actuated strut extends from a first end connected to an interior of the aircraft fuselage, through the pressurized door plug assembly, to a second end of the strut connected to one or more payloads. The rotational axis of the strut is exterior to the aircraft fuselage.

Claim (Index 2):
The apparatus of  claim 1 , wherein the first end of the strut is coupled to an adaptive mounting system (AMS) plate adapted to attach to one or more Air Deployment System (ADS) rails of the aircraft.

Metadata:
- Claim Count in Document: 15.0
- Percentile: 97.0
- Lexical Diversity: 1.68
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15692903', '15265681', '14150710', '12734159', '15658277']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8950139770798607
- 35 USC 102 Novelty (BERT): 0.5988715245441723
- Combined Prediction Score: 0.8653997318262919
- Mean Citation Score: 494.592814
- Max Citation Score: 552.86896
- Similarity Product: 474.5109683030605

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