IP Library Granted Patent US 8,376,462
Granted Patent B2
US 8,376,462 · App. 12/577,106 · Granted Feb 19, 2013

Aircraft seat with adjustable armrests

Inventors: Hector Noel Marini (Palm City, FL); Barry Oberly (Port St. Lucie, FL)
Assignee: PAC Seating Systems, Inc.
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Quick Facts
Patent No.
US 8,376,462
App. No.
12/577,106
Granted
Feb 19, 2013
Kind
B2
Abstract

An aircraft seat includes a seat bottom frame, a seat translation and rotation mechanism attached to the seat bottom frame allowing translation and rotational movement of the seat bottom frame. An armrest is removably attached to the side of the seat bottom frame, and can be set to different positions relative to the seat bottom. The armrest has a seat control mounted to an outside of the armrest, and an input transfer mechanism disposed inside the armrest. The input transfer mechanism has an end engaged to the seat control, and a receiver end. The input transfer mechanism is cable-less. A couple shaft is engaged with the receiver end and engaged with the seat translation and rotation mechanism. When the seat control is actuated, the input transfer mechanism causes the seat translation and rotation mechanism to allow the seat bottom frame to at least one of translate and rotate.

Claims (23)

1. An aircraft seat comprising:

a seat bottom frame having a side;

a seat translation and rotation mechanism attached to the seat bottom frame allowing at least one of translation and rotational movement of the seat bottom frame;

at least one armrest removably attached to the side of the seat bottom frame, the armrest comprising:

a seat control mounted to an outside of the armrest;

at least one armrest bracket disposed on the armrest, wherein the armrest bracket has a plurality of bracket holes;

a seat frame slot extending through the seat bottom frame from a first side of the seat bottom frame to a second side of the seat bottom frame, the seat frame slot configured to receive the armrest bracket, wherein the seat frame slot has a seat frame hole; and

a fastener engaging the armrest bracket and the seat bottom frame by passing consecutively through the seat frame hole and one of the plurality of bracket holes to attach the armrest to the seat bottom frame,

wherein the bracket holes are separately alignable with the seat frame hole and each bracket hole determines a different distance from the armrest to the seat bottom, and

wherein the fastener is a pin.

2. The aircraft seat of claim 1 , wherein the distance determines the width of a seat base disposed on the seat bottom frame.

3. An aircraft seat comprising:

a seat bottom frame having a side;

a seat translation and rotation mechanism attached to the seat bottom frame allowing at

least one of translation and rotational movement of the seat bottom frame;

at least one armrest removably attached to the side of the seat bottom frame, the armrest comprising:

a seat control mounted to an outside of the armrest;

at least two armrest brackets disposed on the armrest, wherein each armrest bracket has a plurality of bracket holes;

at least two seat frame slots each extending through the seat bottom frame from a first side of the seat bottom frame to a second side of the seat bottom frame, each configured to receive one of the armrest brackets, wherein each seat frame slot has at least one seat frame hole; and

at least one fastener engaging each of the armrest brackets and the seat bottom frame by passing consecutively through the seat frame hole and one of the plurality of bracket holes to attach the armrest to the seat bottom frame

wherein the bracket holes are separately alignable with the seat frame hole and each bracket hole determines a different distance from the armrest to the seat bottom, and

wherein the fastener is a pin.

4. The aircraft seat of claim 3 , wherein the distance determines the width of a seat base disposed on the seat bottom frame.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 10, 2009
From: MARINI, HECTOR NOEL; OBERLY, BARRY
To: PAC SEATING SYSTEMS, INC.
Reel/Frame 023496/0479 →
Continuity (1)
Related Publication 20110084527A1 · Apr 14, 2011