Patent ID: 8870116
Filing Date: 2014-10-28
Classification: B64D,G06Q

Abstract:
1. An aircraft seating system comprising: a fuselage having an untapered section and a tapered section; a first type of seat having first dimensions configured to seat a first type of passenger; a second type of seat having second dimensions configured to seat a second type of passenger in which the second dimensions are different from the first dimensions in which the first type of passenger has a hip width that is unable to fit in the second type of seat; a first plurality of seats in the untapered section having a selected number of seats in a selected row; and a second plurality of seats located in one row of the tapered section, the second plurality of seats having at least one less seat in the one row as compared to the first plurality of seats in the selected row in which the second plurality of seats includes at least one more seat of the first type of seat as compared to the first plurality of seats.