Abstract: A method for manufacturing a turbine engine part in which a first rough casting element includes a first face and a second face opposite to each other is assembled by the second face on an orifice which has a second element of the part. The method includes machining a through-cavity in the first element which opens at the first face and from the second face of the first element and machining the first face of the first element so as to form an area suitable for ensuring the attachment of a conduit on the first element. The machining of the cavity and of the first face is achieved by using a machining reference frame based on the second element.

Abstract: A method for manufacturing a turbine engine part in which a first rough casting element includes a first face and a second face opposite to each other is assembled by the second face on an orifice which has a second element of the part. The method includes machining a through-cavity in the first element which opens at the first face and from the second face of the first element and machining the first face of the first element so as to form an area suitable for ensuring the attachment of a conduit on the first element. The machining of the cavity and of the first face is achieved by using a machining reference frame based on the second element.

Abstract: A method for manufacturing a turbine engine part in which a first rough casting element includes a first face and a second face opposite to each other is assembled by the second face on an orifice which has a second element of the part. The method includes machining a through-cavity in the first element which opens at the first face and from the second face of the first element and machining the first face of the first element so as to form an area suitable for ensuring the attachment of a conduit on the first element. The machining of the cavity and of the first face is achieved by using a machining reference frame based on the second element.

Abstract: For the cosmetic field, omniphobic cosmetic pigments under the form of a core shell structure: the core is or includes of a metal oxide on which is adsorbed poly(?-(1?4)-D-glucosamine) chains; the chains being acetylated, or partially or totally deacetylated. Also, the process for manufacturing the omniphobic cosmetic pigments, including: (i) preparing an acidic aqueous solution including metal oxide particles and a poly (?-(1?4)-D-glucosamine), the poly (?-(1?4)-D-glucosamine) being acetylated, or partially or totally deacetylated; and (ii) increasing the pH until 12, of the solution obtained at step (i) in order to obtain the adsorption of said poly (?-(1?4)-D-glucosamine on the metal oxide particles and the precipitation of the resulting metal oxide particles coated with the poly (?-(1?4)-D-glucosamine.

Abstract: A method for manufacturing a turbine engine part in which a first rough casting element includes a first face and a second face opposite to each other is assembled by the second face on an orifice which has a second element of the part. The method includes machining a through-cavity in the first element which opens at the first face and from the second face of the first element and machining the first face of the first element so as to form an area suitable for ensuring the attachment of a conduit on the first element. The machining of the cavity and of the first face is achieved by using a machining reference system based on the second element.

Abstract: A packing structure including: a cap secured to at least one first substrate and forming at least one cavity between the cap and the first substrate; a layer of at least one first material permeable to a gas, arranged in the cap and/or in the first substrate and/or at the interface between the cap and the first substrate, and forming at least one part of a wall of the cavity; a portion of at least one second material non-permeable to said gas, the thickness of which is higher than or equal to that of the layer of the first material, and surrounding at least one first part of the layer of the first material forming said part of the wall of the cavity; an aperture passing through the cap or the first substrate and opening onto or into said part of the layer of the first material.

Abstract: Method comprising steps as follows: a) depositing a meltable ball on a first conducting zone located in a blind hole formed on a first face of a first support, b) assembling the first support with a second support by transfer of the meltable ball on a second conducting zone, the transfer also being made by thermo-compression so as to compress the ball, the compressed ball being held at a distance from the side walls of the blind hole.

Abstract: A pump including a first substrate in a plane with a side having a cavity formed therein. There are intake and discharge channels in the side for admitting and discharging a fluid. There is a second substrate having a side joined to the first substrate, to close the channels and form tubes in which pumped fluid flows. The second substrate also has a membrane to close the cavity to form a leak-tight chamber. The membrane is deformable: in order to expel the fluid out of the chamber via the discharge channel, and to suck the fluid into the chamber via the intake channel. There is actuator capable of converting the energy into movement of the membrane and an assembly for measuring the temperature/flow rate of the fluid. There is a temperature probe placed on the exterior side of the insulating material to insulate thermally the probe from the substrate.

Abstract: A method of encapsulating at least one microelectronic device is provided, including encapsulating the device in a cavity hermetically sealed against air, a cap of the cavity including at least one wall permeable to at least one noble gas; injecting the noble gas into the cavity through the wall permeable to the noble gas; hermetically sealing the cavity against air and the injected noble gas; forming the device on at least one first substrate; bonding at least one second substrate to the first substrate, thereby forming the cavity hermetically sealed against air, the wall permeable to the noble gas being formed by part of the second substrate; and forming, between the encapsulating and the injecting, at least one portion of material impermeable to the noble gas such that said portion partially covers the part of the second substrate that forms the wall permeable to the noble gas.

Abstract: A process for encapsulating a microelectronic device, comprising the following steps: make the microelectronic device on a first substrate; make one portion of a first material not permeable to the ambient atmosphere and permeable to a noble gas in a second substrate comprising a second material not permeable to the ambient atmosphere and the noble gas; secure the second substrate to the first substrate, forming at least one cavity inside which the microelectronic device is encapsulated such that said portion of the first material forms part of a wall of the cavity; inject the noble gas into the cavity through the portion of the first material; hermetically seal the cavity towards the ambient atmosphere and the noble gas.

Abstract: A method for encapsulating at least one micro-device, comprising at least the following steps: bonding a face of a first substrate comprising at least one material impermeable to noble gases, in contact with a second substrate comprising glass and with a thickness of about 300 ?m or more; etching at least one cavity through the second substrate such that side walls of the cavity are at least partly formed by remaining portions of the second substrate and that an upper wall of the cavity is formed by part of said face of the first substrate; anodic bonding of the remaining portions of the second substrate in contact with a third substrate in which the micro-device is formed, such that the micro-device is encapsulated in the cavity.

Abstract: A coating, ink, or article containing a pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III).

Abstract: A cosmetic containing a pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III).

Abstract: A pearlescent pigment, wherein the pigment is an inorganic material and the color of a homogeneous coating of the pigment, measured over a white background, is selected from the group consisting of: a CIELAB L* value of about 30 or less and a chroma value of about 3 or less; a CIELAB hue angle, hab, from about 50 to about 80 degrees, wherein L* is not more than about 85, and the chroma value is greater than 22; a CIELAB hue angle, hab, from about 80 to about 275 degrees, wherein L* is not more than about 80, and the chroma value is greater than about 10; and a CIELAB hue angle, hab, from not less than about 275 to not more than about 50 degrees, wherein L* is not more than about 85, and the chroma value is greater than about 9. The pigments may be used in a variety of applications including cosmetics, plastics, automotive, or architectural coatings.

Abstract: A cosmetic containing a pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III).

Abstract: A cosmetic containing a pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III).

Abstract: A pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III). A process for making these pearlescent pigment, comprise reducing a metal oxide substrate with a hydrogen source in the presence of a noble metal catalyst in a liquid medium. The pigments may be used in a variety of applications including cosmetics, plastics, automotive, or architectural coatings.

Abstract: A pearlescent pigment comprising a substrate and a first layer, wherein the first layer comprises iron oxide, wherein the iron has from about 1% to about 30% Fe(II) and from about 70% to about 99% Fe(III). A process for making these pearlescent pigment, comprise reducing a metal oxide substrate with a hydrogen source in the presence of a noble metal catalyst in a liquid medium. The pigments may be used in a variety of applications including cosmetics, plastics, automotive or architectural coatings.

Abstract: The invention relates to a process for collective manufacturing of cavities and/or membranes (24), with a given thickness d, in a wafer said to be a semiconductor on insulator layer, comprising at least one semiconducting surface layer with a thickness d on an insulating layer, this insulating layer itself being supported on a substrate, this process comprising: etching of the semiconducting surface layer with thickness d, the insulating layer forming a stop layer, to form said cavities and/or membranes in the surface layer.

Abstract: A pearlescent pigment, wherein the pigment is an inorganic material and the color of a homogeneous coating of the pigment, measured over a black background has a CIELAB hue angle, hab, from about 40 to about 320 degrees, wherein L* is from about 35 to about 80, and the chroma value is less than 5. A substrate is coated with iron oxide by oxidizing an iron salt to form a pigment. The pigment may be made by a process of coating iron oxide on a substrate by oxidizing an iron salt. During the coating of the iron oxide, the pH of the mixture is increased. The coating formed has a Fe(III)/Fe(II) ratio of greater than 2. The pigments may be used in a variety of applications including coating, ink, plastic, and cosmetic compositions.