PATENT CLAIM ANALYSIS

Application Number: 15928600
Application Type: Utility
Filing Date: 2018-03
Publication Date: 2019-05
Patent Classification: ["244", "00700C"]

Abstract:
An aircraft includes a tiltwing where the tiltwing is a single wing to which starboard-side and non-foldable outer propeller, a port-side and non-foldable outer propeller, a starboard-side and foldable inner propeller, and a port-side and foldable inner propeller are coupled to. Those rotors rotate at least some of the time when the tiltwing is in a vertical takeoff and landing position. The starboard-side and foldable inner propeller and the port-side and foldable inner propeller are stowed at least some of the time when the tiltwing is in a forward flight position. The tiltwing rotates about an axis of rotation, when rotating between the vertical takeoff and landing position and the forward flight position, that is higher than the aircraft's center of mass.

Claim (Index 1):
An aircraft, comprising:\n a fuselage which includes a windshield; a starboard-side non-foldable outer propeller; a port-side non-foldable outer propeller; a starboard-side foldable inner propeller; a port-side foldable inner propeller; and a tiltwing, wherein:\n the tiltwing is a single common wing to which the starboard-side non-foldable outer propeller, the port-side non-foldable outer propeller, the starboard-side foldable inner propeller, and the port-side foldable inner propeller are coupled to; \n the starboard-side non-foldable outer propeller, the port-side non-foldable outer propeller, the starboard-side foldable inner propeller, and the port-side foldable inner propeller rotate at least some of the time when the tiltwing is in a vertical takeoff and landing position; \n the starboard-side foldable inner propeller and the port-side foldable inner propeller are stowed at least some of the time when the tiltwing is in a forward flight position; and \n the tiltwing is coupled to the fuselage above and aft of the windshield and the tiltwing rotates about an axis of rotation, when rotating between the vertical takeoff and landing position and the forward flight position, that is higher than the aircraft's center of mass.

Metadata:
- Claim Count in Document: 26.0
- Percentile: 90.0
- Lexical Diversity: 2.4
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15801052', '10414874', '15612671', '11667366', '14559529']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8542555053471804
- 35 USC 102 Novelty (BERT): 0.562645446084912
- Combined Prediction Score: 0.8250944994209536
- Mean Citation Score: 280.967378
- Max Citation Score: 525.2831
- Similarity Product: 360.94446323038335

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

Dataset: test