Abstract: The invention relates to an assembly between an aircraft pylon (30) and a turbomachine (20) of longitudinal axis (X), the pylon (30) and the turbomachine (20) each comprising front and rear longitudinal regions, the assembly comprising a rear support (40) configured to connect the rear region of the turbomachine (20) to the rear region of the pylon (30), the assembly being characterized in that the rear support (40) comprises a sliding pivot connection arranged between the rear region of the turbomachine (20) and the rear region of the pylon (30), so as to allow the turbomachine (20) only translational and rotational movements along and about the longitudinal axis (X) and along and about a vertical axis (Z) and a rotational movement about a transverse axis (Y).

Abstract: Connector (1) for flexible printed circuit (FPC) (3) comprising a connector housing (5) including an insertion slot (4) adapted to receive the FPC (3). The connector comprises a shield (18) adapted to be electrically connected to a ground path (2a) of a circuit substrate (2) on which the connector (1) is to be mounted. Said insertion slot (4) comprises a signal side corresponding to conductive tracks (29) of the FPC and a ground side (26a) opposite to said signal side. The shield comprises at least one electrically conductive tooth (25), movable from a retracted position outside the insertion slot (4), to a protruding position where said tooth (25) protrudes from the ground side (26a) to the inside of the insertion slot (4).

Abstract: Electrical connector including a sealing mat made of a deformable material body having a thick portion and a thin portion having: an upper face a lower face parallel to the upper face, hollow passageways extending along a longitudinal axis from the upper face to the lower face, a housing including a receiving portion, a grid including a compression portion, the sealing mat being compressed between the receiving and compression portions.

Abstract: Electrical connector including a sealing mat made of a deformable material body having a thick portion and a thin portion having: an upper face a lower face parallel to the upper face, hollow passageways extending along a longitudinal axis from the upper face to the lower face, a housing including a receiving portion, a grid including a compression portion, the sealing mat being compressed between the receiving and compression portions.

Abstract: An electrical connector includes a sealing joint having a passageway for receiving an electrical connection member, the passageway having a retention region including a first lip a second lip, and an inter-lip gap between said lips, each of said lip including an internal face, an external face opposite said internal face and a top face having an internal diameter Di.

Abstract: The invention relates to a macro-porous composite that can be used as a bone reconstitution material. The composite is made up of a combination of synthetic aragonite and at least one medicinal substance such as notably, an antibiotic. The invention also relates to a method of producing a composite which includes producing a mixture includes grains of synthetic aragonite and at least one porogenic agent, compacting the mixture and heating the product obtained in such a way as to eliminate the porogenic agent. At least one medicinal substance is included before or after the step of eliminating of the porogenic agent.

Abstract: The invention relates to a macro-porous composite that can be used as a bone reconstitution material characterised in that it is made up of a combination of synthetic aragonite and at least one medicinal substance such as notably, an antibiotic. The invention also relates to a method of producing a composite characterised in that it consists of producing a mixture comprising grains of synthetic aragonite and at least one porogenic agent, compacting said mixture and heating the product obtained in such a way as to eliminate said porogenic agent, at least one medicinal substance being included before or after said step of eliminating of said porogenic agent.

Abstract: An apparatus and method for decoupling of the behavior of an aircraft which may determine a first control demand that is representative of the actuation of a control member, determine a transfer function that is representative of the behavior of an aircraft upon actuation of the control member, determine a second control demand that is capable of generating a decoupling based at least on a partial inversion of the transfer function and a non-inverted part of the transfer function, calculate an overall demand from the sum of the first and second control demands, and apply the overall demand to the aircraft.