Safran Seats

Safran Seats USA LLC

Zodiac Seats France

Snecma

Sanfran Seats

Societe Industrielle Et Commerciale De Material Aeronautique

Patrick Herault

Bastien Bonnefoy

Arthur K Glain

Eric O Freienmuth

Victor Carlioz

Matthew Cleary

Christopher La Montagna

Jeremy Cailleteau

Philippe Roy

Christophe Ducreux

Franck Jasny

Jean-Jacques Varin

Michel Boulnois

Christian Boudereau

Hassan Boussaboun

Charles Caruana

Jean-Marc Caux

Francis Chareyre

Gerard Defrocourt

Clement Sampaio

Clement Sampaieo

Eric Freienmuth

Arthur Glain

Passenger seats having improved comfort emergency egress solutions for mini suites or other types of passenger seats that have a privacy screen, wall, or sliding door that divides the passenger seat from the aisle area or other common area. Specific embodiments find particular use on-board passenger transportation vehicles, such as aircraft, where comfort and privacy must be balanced with safety and federal regulations.

Mini suite emergency egress solutions

The invention relates mainly to a closure device, notably for closing a passage formed in a cabin of an aircraft, comprising: characterized in that, notably in the case of a malfunction, the locking system is able to pass into an unlocked state, in which the closing wall is disconnected from the support means, such that the closing wall is movable on its own in the sliding direction.

Device for closing a passage between two seat units

The invention relates to a seat arrangement, in particular designed to be installed in an airplane cabin, comprising:

Seat arrangement, in particular for an airplane

The invention relates mainly to a closure device, notably for closing a passage formed in a cabin of an aircraft, comprising:

The present invention generally relates to passenger aircraft seats. The disclosure focuses on a seat unit arrangement () for a cabin and seat units that provide different comfort positions. In some embodiments, a side cushion () forms part of a bed surface when the seats are converted to a bed position. In some embodiments, a bed extension () is deployed from a stowed position to form a part of the bed surface. In some embodiments, a seat backrest () does not form part of the bed surface when the seat unit is in the bed position. In some embodiments, a lounge position is provided when the seat backrest rotates toward a side cushion. In such an embodiment, the passenger may be positioned toward the side cushion such that the passenger may comfortably rest their legs on the side cushion without converting the seat to a bed position.

Aircraft seat configuration and arrangement systems and methods

Embodiments of the invention provide premium seats for aircraft and other passenger transport vehicles that provide extra seat room by providing an improved tray table configuration, which also enhances privacy for each passenger. Certain embodiments also provide an improved outer armrest configuration.

Premium seat offering extra wide bed

A process for repairing a metallic shroud of a gas turbine blade includes a step of removing a portion of an anti-wear layer to a removal depth that is greater than a depth of wear of the anti-wear layer. Further, the process includes a step of leaving a trace of the anti-wear layer to subsist, wherein the trace of the anti-wear layer extends at least in a re-entrant zone of the Z profile of the blade. The process also includes a step of depositing a new layer of anti-wear material on the trace of the anti-wear layer.

Process for repairing metallic pieces especially turbine blades of a gas turbine motor

The invention relates to a seat for a transport vehicle or craft, the seat including a support structure () and at least one armrest () comprising a rest element () mounted on one end of a strut whose other end is hinged to the support structure about a first pivot () to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat. The strut is L-shaped with a first arm () hinged at its free end about the first pivot and extending substantially rearwards from the first pivot when the strut is in the in-use position, and a second arm () extending substantially upwards when the strut is in the in-use position, and the rest element is hinged to the free end of the second arm of the strut about a second transverse axis ().

Seat for a transport vehicle or craft, in particular an aircraft

Growing community of inventors

Saint Hilaire en Lignieres, France

Patrick Herault