PATENT CLAIM ANALYSIS

Application Number: 15893833
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-08
Patent Classification: ["415", "214100"]

Abstract:
A seal configuration for an aircraft engine includes a ring shaped sealing component defining an axis, a carrier disposed radially outward of the ring shaped sealing component and supporting the ring shaped sealing component, and a housing disposed at least partially about the carrier. The housing is maintained in a static position relative to the carrier via a bellows spring. At least one of the carrier and the housing include a plurality of rotation inhibiting features disposed in a balanced configuration about the at least one of the carrier and the housing. Each of the rotation inhibiting features including a finger extending from the housing and at least one interface feature corresponding to each finger, and being disposed on the carrier. The at least one interface feature comprises one of a notch protruding radially into the carrier and a tab protruding radially outward from the carrier.

Claim (Index 4):
The seal configuration of  claim 3  wherein each of said tabs includes a surface facing the axially aligned finger, and wherein the surface is tapered.

Metadata:
- Claim Count in Document: 7.0
- Percentile: 88.0
- Lexical Diversity: 2.36923
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13316922', '14915755', '14935628', '14965501', '15617598']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8176074225835902
- 35 USC 102 Novelty (BERT): 0.4615050042957273
- Combined Prediction Score: 0.7819971807548038
- Mean Citation Score: 234.284176
- Max Citation Score: 266.0261
- Similarity Product: 187.88244265344144

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

Dataset: test