# US 11,999,463 B2 · Mounting rail arrangement for an aircraft floor, floor structure and aircraft having the same

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- Number: US 11,999,463 B2
- Document ID: US11999463B2
- Status: Granted
- Kind: B2
- Application number: 17/850,491
- Filed: 2022-06-27
- Published: 2023-01-05
- Granted: 2024-06-04
- Earliest claimed: 2021-06-30
- Assignees: Airbus Operations GmbH
- Applicants: Airbus Operations GmbH
- Inventors: Claus-Peter Gross
- Web page: https://patentgrep.com/patent/US11999463B2

## CPC

- B64C 1/18: Floors
- B64C 1/20: specially adapted for freight
- B64D 11/0696: {Means for fastening seats to floors, e.g. to floor rails}
- B64C: AEROPLANES; HELICOPTERS
- B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT

## Abstract

A mounting rail arrangement for an aircraft floor, floor structure and aircraft having the same. To allow full floor structural decoupling for monuments and/or cabin attendant seats, a mounting rail arrangement includes two mounting rails having mounting holes distributed along their longitudinal direction. A mounting bolt is inserted into the mounting holes and an attachment bolt for fixing a cabin monument and/or a cabin attendant seat is inserted into the mounting bolt. As a result, the cabin monument and/or cabin attendant seat may be installed on at different locations and/or with different orientations using all kinds of configurations enabled by the mounting holes.

## Claims

### Claim 1

A mounting rail arrangement for an aircraft floor, the mounting rail arrangement comprising:
a first mounting rail having a first bottom leg, a first top leg, and a first mounting portion, wherein the first mounting portion is arranged between the first bottom leg and the first top leg;
a second mounting rail having a second bottom leg, a second top leg, and a second mounting portion, wherein the second mounting portion is arranged between the second bottom leg and the second top leg; and
a mounting bolt comprising a cross hole for receiving an attachment bolt, wherein the attachment bolt is inserted in the cross hole and fixed to the mounting bolt to protrude above the top legs and prevent the mounting bolt from sliding out of the mounting holes;
wherein the first and second mounting portions face each other and define a gap therebetween, the gap separating the first bottom leg from the second bottom leg and the first top leg from the second top leg;
wherein the first mounting rail is separated from the second mounting rail by the gap;
wherein the first mounting portion comprises a first mounting hole;
wherein the second mounting portion comprises a second mounting hole; and
wherein the first mounting hole is aligned with the second mounting hole and the mounting bolt extends through the first and second mounting holes.

### Claim 2 (depends on 1)

The mounting rail arrangement according to claim 1, wherein:
the mounting bolt is arranged so the cross hole is arranged within the gap to be accessible.

### Claim 3 (depends on 1)

The mounting rail arrangement according to claim 1, wherein the first mounting rail and/or the second mounting rail is made of metal.

### Claim 4 (depends on 1)

The mounting rail arrangement according to claim 1, wherein the first mounting rail and/or the second mounting rail is made of a fiber composite material.

### Claim 5 (depends on 1)

The mounting rail arrangement according to claim 1, comprising a lower plate member attached to the bottom legs.

### Claim 6 (depends on 1)

The mounting rail arrangement according to claim 1, comprising an upper plate member attached to the top legs, the upper plate member being configured for allowing protrusion of the attachment bolt.

### Claim 7 (depends on 6)

The mounting rail arrangement according to claim 6, further comprising at least one floor panel attached to the top legs or the upper plate member.

### Claim 8 (depends on 1)

A floor structure for a fuselage of an aircraft, the floor structure comprising a plurality of cross beams configured to horizontally extend in a direction orthogonal to a flight direction, and at least one mounting rail arrangement according to claim 1, wherein the first mounting rail and the second mounting rail are aligned parallel to the flight direction.

### Claim 9 (depends on 8)

The floor structure according to claim 8, comprising a plurality of support beams attached to at least one cross beam of the plurality of cross beams to allow support of the at least one cross beam on the fuselage.

### Claim 10 (depends on 8)

The floor structure according to claim 8, wherein at least two mounting rail arrangements are arranged in parallel and spaced apart from each other.

### Claim 11 (depends on 1)

A fuselage for an aircraft, the fuselage comprising the mounting rail arrangement according to claim 1.

### Claim 12 (depends on 11)

The fuselage according to claim 11, further comprising a cabin monument and/or cabin attendant seat attached to the mounting rail arrangement.

### Claim 13 (depends on 1)

An aircraft comprising the mounting rail arrangement according to claim 1.

### Claim 14 (depends on 8)

An aircraft comprising the floor structure according to claim 8.

### Claim 15 (depends on 11)

An aircraft comprising the fuselage according to claim 11.

### Claim 16 (depends on 8)

A fuselage for an aircraft, the fuselage comprising the floor structure according to claim 8.

### Claim 17 (depends on 16)

The fuselage according to claim 16, further comprising a cabin monument and/or cabin attendant seat attached to the floor structure.
