Abstract: The present invention relates to a groove-type vacuum insulation material and a method of manufacturing the same. The groove-type vacuum insulation material includes core materials each having a block shape, at least one lateral wall of which has an inclined surface; a groove-type insulation board, in which the core materials are arranged on a plane of the board to be separated from each other, with the inclined surfaces thereof facing each other; an outer skin material formed in a film pouch shape and surrounding the entirety of upper and lower sides of the groove-type insulation board, the outer skin material being brought into close contact with the groove-type insulation board by vacuum-sealing, and exhibiting bending characteristics in a space between the core materials. The present invention also relates to a method of manufacturing the same.

Abstract: A method of making a composite structure (1) that comprises a curved body (5) and an integral rim (3) extending from an end of the curved body. The method comprises the steps of: forming a diaphragm pack (19) comprising a flat stack (13) of composite plies between two diaphragms (15 A, 15B), wherein each ply (L1, L2, L3) of the flat stack (13) is made up of a plurality of composite tiles (9). Each tile (9) includes at least a first portion (9A) and a second portion (9B) that have side edges of the first portion (9A) configured to abut against side edges of adjacent tiles and side edges of the second portion (9B) configured to overlap side edges of adjacent tiles. Air is evacuated from within the diaphragm pack (19) either before or after placing the diaphragm pack (19) within a double diaphragm forming apparatus comprising a hollow forming tool (23), wherein the first portion (9A) of the composite tiles (9) is supported on an upper surface (23 A) of the tool (23).

Abstract: Methods and apparatus for fabricating adhesive bonded joints while minimizing the voids and/or porosity found in the cured bondline. In accordance with various embodiments, the apparatus comprises an evacuation chamber combined with a pressure inducing device to produce bonded joints that are both void free and thoroughly compacted. The surfaces to be bonded are continuously evacuated throughout the bonding process (pre-mating, mating, debulking and cure). Continuous evacuation is provided via standard vacuum, while the induced pressure can be pneumatically or mechanically provided.

Abstract: A method of manufacturing a hermetically sealed container provided with first and second substrates includes the steps of disposing, within a chamber, the first and second substrates opposite to each other to form a gap therebetween, and separating an edge portion of at least the first substrate from the second substrate, for processing to warp the first substrate, within the chamber. Additional steps include exhausting a space between the first and second substrates, by exhausting an inside of the chamber in a state of warping the first substrate, and hermetically connecting the first and second substrates through a bonding material, within the chamber, in a state of exhausting the space between the first and second substrates.

Abstract: The invention relates to an interior lining for vehicles and aircraft having a carrier and a heating layer and an upper layer, wherein the at least one heating layer is arranged between the carrier and the upper layer, and the heating layer and the upper layer are directly or indirectly interconnected, and to a method for producing such an interior lining, wherein at least one heating layer is pre-laminated onto an upper layer to form a layer composite, and the layer composite is press-laminated, membrane-laminated or vacuum-laminated onto a carrier, or alternatively, in order to produce such an interior lining, a heating layer is pre-laminated onto a carrier to form a carrier/layer composite, and an upper layer is press-laminated, membrane-laminated or vacuum-laminated onto the carrier/layer composite.

Abstract: According to the invention, one or more thermoplastic sheets (NdT: “feuilles thermoplastique” in the original) (2) are applied on a flat or curved tool (13), and strips (NdT: “des bande” in the original) of a polymer are applied and pressed onto the sheets (2). They are maintained by suction pumps (8), the orifices (4) of which open into a closed volume or one substantially delimited by a sealing joint (3) and occupied by a draining fabric (7). The heating treatment concomitant to the deposition to harden or consolidate the prepreg softens the sheets (2), distorts them to the curvature of the tool (13) and incorporates them in the structure of the prepreg. Application to methods of draping parts with composite material.

Abstract: The present invention relates to a glass laminate including a glass substrate and a supporting glass plate, in which a surface of the glass substrate and a surface of the supporting glass plate are directly contacted to each other, in which each of the surface of the glass substrate and the surface of the supporting glass plate that are contacted to each other is a smooth flat surface, and the both surfaces are closely adhered.

Abstract: Provided is a hybrid silicon wafer comprising a structure in which a single-crystal wafer is embedded in a sintered polysilicon wafer. Also provided is a method for manufacturing a hybrid silicon wafer having a structure in which a single-crystal wafer is embedded in a sintered polysilicon wafer, wherein a part of the sintered polysilicon is hollowed, a single crystal ingot is inserted into the hollowed portion, these are mutually bonded through thermal diffusion bonding based on HIP to prepare a complex of the sintered polysilicon and the single-crystal silicon ingot, and the complex is sliced. Thereby provided are a hybrid silicon wafer comprising functions of both the polysilicon wafer and the single-crystal wafer, and a method for manufacturing such a hybrid silicon wafer.

Abstract: Apparatuses, systems and methods for forming elongated composite structural members are provided. One disclosed method includes providing a substantially elongated mandrel having an exterior surface exhibiting a desired geometry. A plurality of plies of fiber material preimpregnated with a thermosetting resin are laid up and pressed onto the mandrel, Pressing the plies of material may include passing one or more rollers over the mandrel and over the plurality of plies along a length of the mandrel. The roller or rollers may be at least partially complementary in shape with the mandrel while maintaining the plies of material in a substantially uncured state during the pressing. The method may include sequentially passing a plurality of rollers over the mandrel and the plies of material. The method may also include configuring a first roller to partially complementarily engage the mandrel and configuring another roller to substantially fully complementarily engage the mandrel.

Abstract: A novel moldable ballistic armor panel having a first outwardly-positioned fracturable layer formed of a ceramic material; a second inwardly-positioned fragment containment layer formed of a consolidated stack of ballistic-resistant laminate sheets, the fragment containment layer being substantially coextensive with the fracturable layer and laminated thereto; and an encapsulation material formed of a resin-impregnated high strength fiber material, the resin-impregnated fiber material at least partially encapsulating the laminated fracturable and fragment containment layers.

Abstract: There is provided a bonding apparatus for holding a semiconductor chip by using a bonding head and bonding the semiconductor chip onto a substrate. The bonding head includes: a holding part for holding the semiconductor chip; gas exhausting means for surrounding the holding part and exhausting gas toward the holding part; and an elevator means for lifting down/up the gas exhausting means to a lift-down state, in which at least a portion of the gas exhausting means protrudes downward from the bottom face of the holding part, and a lift-up state, in which any portion of the gas exhausting means does not protrude downward from the bottom face of the holding part. When the bonding apparatus holds and conveys the semiconductor chip by using the bonding head, the bonding apparatus brings the gas exhausting means to the lift-down state and exhausts the gas toward the semiconductor chip.

Abstract: A method of assembling a chair includes providing a first chair component composed of a first polymeric material and a second chair component composed of a second polymeric material. An adhesive is positioned on or in the first chair component. The adhesive is composed of a third polymeric material and at least one ferromagnetic susceptor. The second chair component is positioned in engagement with the adhesive and adjacent to the first chair component. A magnetic field or electromagnetic waves are applied to the adhesive to activate the adhesive. A force is also applied to at least one of the first chair component and the second chair component to press the first chair component and the second chair component. A chair is also provided that includes the first and second chair components and the adhesive.

Abstract: In a method of manufacturing a blade shell half of a pre-bent wind turbine blade by means of vacuum-assisted resin transfer moulding (VARTM), a fibre lay-up (16) is placed on a mould surface (14) and a distribution layer (24) is placed above the fibre lay-up (16). At least one segmentation area is provided in the distribution layer by providing at least one transversely extending flow barrier in the distribution layer (24) preventing or restricting longitudinal resin flow to the distribution layer. A longitudinally extending first feed channel (27) is placed above the distribution layer (24). The first feed channel (27) is divided into at least two feed channel sections, a feed channel section being arranged in each distribution layer segment. A vacuum bag (43) is arranged on top of the mould part (13) to define a mould cavity. The mould cavity (44) is evacuated and liquid resin is supplied to each feed channel section through a resin inlet to fill the mould cavity and impregnate the fibre lay-up.

Abstract: A bow wave in a composite laminate generated during part consolidation is reduced by transmitting atmospheric pressure loads to a region of the part having low compaction pressure due to bridging of a vacuum bag at an edge of the part.

Abstract: A membrane includes a composite material of a silicone polymer and 0.1 wt % to 15 wt % of a scavenging filler. The membrane has a thickness of at least 1 mm and exhibits a tensile retention index of at least 35%.

Abstract: Provided are a device for producing a sheet structure including a flexible sheet and a structure formed on the sheet whereby the sheet structure can be easily produced and a method for producing the sheet structure. The production device 1 includes: a table 10 having in a surface thereof a holding region 12; a formation mechanism 31 for forming a structure 2b; a holding mechanism 25 for holding a sheet 2a on the holding region 12; and a control unit 40. The holding mechanism 25 includes: porous materials 14b and 15b provided so that they are at least partly located within the holding region 12 and having interconnected cells; a negative-pressure generating mechanism 17; and a positive-pressure generating mechanism 20. The control unit 40 allows the negative-pressure generating mechanism 17 to generate a negative pressure to hold the sheet 2a, then allows the formation mechanism 31 to form the structure 2b, and then allows the positive-pressure generating mechanism 20 to generate a positive pressure.

Abstract: Disclosed is a method for preparing a multilayer film laminate having a first layer comprising a perfluorinated copolymer resin layer adhered to a second layer comprising an olefin ester copolymer that has been blended with an organosilane. The multilayer laminate is useful in photovoltaic modules. Methods for preparing photovoltaic modules are also included.

Abstract: Disclosed is a method for preparing a multilayer film laminate having a first film layer comprising a perfluorinated copolymer resin layer adhered to a polymeric second film layer that has been surface treated with an aminosilane. The multilayer laminate is useful as a photovoltaic module component. Methods for preparing photovoltaic modules that include the multilayer laminate are also disclosed.

Abstract: Methods for assembling an active array system are described. In one exemplary embodiment, an active subarray panel assembly having a first surface with a first array of electrical contacts and a radiator aperture with an array of radiator structures and an aperture mounting surface with a second array of electrical contacts are assembled together. The first surface of the panel assembly and the aperture mounting surface of the radiator aperture are brought into contact with an adhesive layer including microwave interconnects in a pattern corresponding to the first array of electrical contacts and the second array of electrical contacts so that the adhesive layer is between the first surface of the panel assembly and the aperture mounting surface of the radiator aperture. Pressure, heat and vacuum are applied to cure the adhesive and complete engagement of the microwave interconnects.

Abstract: A method for fabricating an air-filled cellular structure for use as a resilient cushion. The method includes providing a molding structure including a shelf substantially surrounding a depression, and a platform that fits within the depression and is selectively movable between a plurality of positions relative to the shelf, moving the platform to a preselected position relative to the shelf, wherein the preselected position corresponds to a substantially predetermined amount of air to be contained by the air-filled cellular structure, and using a vacuum device to draw air from within the depression.

Abstract: A multilayer film comprises a layer consisting essentially of a fluorinated copolymer resin and a layer consisting essentially of an ethylene copolymer ionomer blend. The ethylene copolymer ionomer blend, or the product of crosslinking the blend, can be used as an encapsulant layer for solar cells, and the multilayer film is useful as a component of photovoltaic modules. Methods for preparing the multilayer films and the photovoltaic modules are also described.

Abstract: A machine cell for the forming and joining of a first sheet material to a second sheet material includes an upper gate and a lower nest. The lower nest includes a vacuum pad having a recessed channel defined therein. A vacuum system is fluidly connected to the recessed channel to hold the first sheet material to the lower nest during the joining of the first and second sheet materials. The machine cell further includes an arrangement for aligning the first sheet material to the second sheet material.

Abstract: The present invention relates to a process for manufacturing composite structures formed by two subcomponents of the same material, characterized in that it comprises the following steps: providing a first subcomponent (13), particularly a skin; providing a tool (15) made of a composite and precured for the manufacture of the second subcomponent (17), particularly a stiffener; positioning said tool (15) on said first subcomponent (13); applying preimpregnated composite (21) on said tool (15) so as to form the second subcomponent (17); consolidating the composite structure by means of a process of curing the assembly resulting from the previous steps under suitable pressure and/or temperature conditions.

Abstract: Described certain plasticized poly(vinyl butyral) (PVB) interlayer sheets that may be used to produce safety glass and solar cell laminates having enhanced penetration resistance and adequate adhesion levels. In particular, the stress value of these interlayer sheets at an elongation of 120% is preferably in the range of from about 8 to about 15 N/mm2.

Abstract: According to the present invention, an electrolyte membrane having recesses and projections on the surface thereof is obtained. In addition, a membrane-electrode assembly comprising the electrolyte membrane, in which the effective contact area between the electrolyte membrane surface and an electrode catalyst layer is increased, is obtained. An electrolyte membrane 1 which comprises a fluorine-based electrolyte is heated and pressed with the use of plates 10a and 10b each having recesses and projections 11 on the surface thereof such that recesses and projections 2a and 2b are formed on the surface of the electrolyte membrane 1. Thereafter, the electrolyte membrane 1 is subjected to a treatment for imparting ion exchange properties to an electrolyte polymer, such as hydrolysis, such that an electrolyte membrane 3 having recesses and projections on the surface thereof is obtained.

Abstract: A process for bonding a vented hollow component includes placing a preformed component with an aircraft skin on a tool surface, with bonding agent applied between the component and the skin. A vacuum bag is sealed about a vent in the preformed component. The vent may be formed through the vacuum bag and the component, or the vent may be preexisting (i.e., an open end of the preformed component or an aperture through the component). The vacuum bag is sealed to the tool surface with a temporary seal or adhesive, to enclose the preformed component and the skin. A vacuum is applied within the bagging material, to compress the preformed component with the aircraft skin, and the bagged assembly is autoclaved to cure the bonding agent. The vent in the preformed component facilitates pressure equalization within and outside of the component to enhance compression against the aircraft skin.

Abstract: An attaching method for attaching a support plate to a surface of a substrate with an adhesive involves the steps of applying an adhesive to the surface of the substrate, heating and thereafter cooling the substrate, positioning centers of the substrate and the supporting plate to coincide with each other, and forming a layered structure by pushing the supporting plate onto the substrate with the adhesive therebetween in a pressure-reduced atmosphere. In the positioning step, after the supporting late has been placed on the substrate, it is possible to finely adjust the alignment of the supporting plate and a semiconductor wafer when attached because the adhesive is applied to the surface of the substrate, and thereafter the substrate is heated and cooled.

Abstract: Method for manufacturing a cuff on a plastic tube comprising an inner tube and an outer sheath covering said inner tube. The outer sheath comprises at least a portion to be molded for producing a cuff. The method comprises a covering step including an injection operation in which air is intermittently or continuously injected between the inner tube and sheath.

Abstract: Methods and apparatus for fabricating adhesive bonded joints while minimizing the voids and/or porosity found in the cured bondline. In accordance with various embodiments, the apparatus comprises an evacuation chamber combined with a pressure inducing device to produce bonded joints that are both void free and thoroughly compacted. The surfaces to be bonded are continuously evacuated throughout the bonding process (pre-mating, mating, debulking and cure). Continuous evacuation is provided via standard vacuum, while the induced pressure can be pneumatically or mechanically provided.

Abstract: The present invention provides a thin film drying method, an alignment film drying method and a method for manufacturing a display panel. The thin film drying method comprises the following steps: forming the thin film on a substrate; placing the substrate in a vacuum chamber; and reducing a pressure in the vacuum chamber. The thin film drying method can be applicable to the alignment film drying method and the method for manufacturing the display panel. The invention can enhance the film quality after drying.

Abstract: A process for bonding aircraft components with a surface, such as an aircraft skin, includes positioning the skin on a tool surface and placing a floorless component on the skin, with bonding agent therebetween. A vacuum bag is placed within the floorless component via a vent in the component, and sealed with opposing inner, lower walls of the component, creating a sealed surface over the skin within the component. Additional vacuum bags seal between lower, exterior legs of the floorless component and either (a) the tool surface (enclosing the skin) or (b) lower walls of adjacent aircraft components. Lower, opposing sides of the adjacent component are also bagged, and loose bag ends are sealed to the tool surface, such that the skin and all feet of the aircraft components are enclosed in vacuum bagging material. The bagged assembly is autoclave cured to bond the aircraft components with the skin.

Abstract: A transparent laminate having good transparency and good adhesion to transparent substrates, and containing a cured resin layer having excellent tear resistance. A process of producing a transparent laminate by interposing a curable resin composition containing an unsaturated urethane oligomer (A) which is a reaction product of a polyol component (A1) containing a polyol (a1) having from 2 to 3 hydroxy groups, a hydroxy value of 15 to 30 mgKOH/g and an oxyethylene group content of 8 to 50 mass %, a polyisocyanate (A2) and an unsaturated hydroxy compound (A3) or a reaction product of a polyol component (A1) and an unsaturated isocyanate (A4), and a monomer (B) represented by CH2?C(R)C(O)O—R2 (wherein R is a hydrogen atom or a methyl group, and R2 is a C3-4 hydroxyalkyl group having 1 to 2 hydroxy groups), between a pair of transparent substrates, and curing the curable resin composition.

Abstract: To improve the bonding of two parts (401, 403) of a component (400) of an EUV or UV lithography apparatus such that the probability of occurrence of additional stress over time in the bonded parts (401, 403) is lessened, a component (400) of an EUV or UV lithography apparatus comprising two parts (401, 403) bonded to each other by adhesive material (405) is proposed, wherein the adhesive material (405) is coated with a protective layer (407) insulating the adhesive material (405) from the surrounding gas environment.

Abstract: An extrudable polyvinyl chloride composition comprising from 80 to 99.9 percent by weight polyvinyl chloride for use in extruding a first part and a second part, wherein a fusion joint between the first extruded part and the second extruded part is formed by: A) composition at least a portion of a first terminal edge of the first extruded part and a first terminal edge of the second extruded part; B) engaging the melted terminal edges; and C) maintaining pressure between the engaged terminal edges to create a fused joint having a strength that is at least 50% of the tensile strength of the extruded part as measured by ASTM D638-2a. The extruded parts can be pipe sections.

Abstract: A method and apparatus for forming a vehicle window assembly utilizes one or more induction heating devices to adhesively bond an item of hardware to a glass substrate, which substrate is then adapted to fill an opening in a vehicle body. Preferably, the induction heating device(s) and one or more assembly aids are components of an assembly fixture which allows for automated or semi-automated production of such vehicle window assemblies.

Abstract: The present invention relates to a method of manufacturing a laminate with the formation of underpressure between a mould (103) and a vacuum foil (105) and supply of resin from injection areas to the layers of the laminate situated in the mould. The novel aspect according to the invention comprises movement of the injection areas while the resin is supplied, This is accomplished by use of a movable suction unit (200) which is arranged on top of the vacuum foil and which, by means of an underpressure between the suction unit and the vacuum foil, forms injection areas for supply of the resin, which can be moved by moving the suction unit. The invention further relates to such movable suction unit and the use thereof in the manufacture of laminates.

Abstract: Methods and systems are disclosed for printing and affixing an individual label onto an item having a machine readable code thereon. The method includes steps of scanning the machine readable code to obtain unique item information from the scanned machine readable code; supplying a label to a printer; sending the unique item information to the printer; printing information to the label using the unique item information; and affixing the printed label onto the item.

Abstract: Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure.

Abstract: An adhesive assembly is provided in particular for assembling a novel element on a structure or further for reinforcing a structure. The adhesive assembly includes a substrate, a rigid element placed with an interval relative to the substrate, at least one seal compressed between the substrate and the rigid element and defining a sealed space within said interval, and a hardened adhesive occupying said space. The seal is compressed by the rigid element that is held on the substrate by the hardened adhesive.

Abstract: A forming tool (100) for and a method of making a three dimensional composite component using double diaphragm forming. The forming tool (100) comprises a forming side having two or more regions of changing profile and one or more through holes associated with each region, the through holes exit on the forming side and are connectable to one or more vacuum sources such that vacuum can be selectively and discretely applied to each region.

Abstract: The present invention is premised upon a multi-layer laminate structure and method of manufacture, more particularly to a method of constructing the multi-layer laminate structure utilizing a laminate frame and at least one energy activated flowable polymer.

Abstract: Disclosed is a film sticking device that sticks a first film substrate and a second film substrate together on a curved-surface shape. The film sticking device includes a mold having a curved attachment surface formed into a desired curved-surface shape; an attracting and holding unit capable of relatively moving on the curved attachment surface and having plural vacuum chambers on which an attracting surface for attracting and holding the second film substrate is provided; and a suctioning unit capable of separately applying suction processing to the plural vacuum chambers. The suctioning unit starts, as the attracting and holding unit moves, the suction processing of the vacuum chamber corresponding to a position opposing the second film substrate and sequentially stops, as the second film substrate is stuck to the first film substrate, the suction processing of the vacuum chamber corresponding to the stuck second film substrate.

Abstract: A curved circularly polarized lens is used in a passive 3D system to view 3D multimedia. The lens is created in an advanced delicate process whereby two lens pieces are combined with a special glue and molded to a specific conformation. This unique method of production of curved circularly polarized lenses retains the molecular arrangement of the lens, reduces or eliminates optical distortion and physical warping, and eliminates movement between the lens layers.

Abstract: An intermediate sealing element and method for unsealing a vacuum membrane from one tool surface and transferring it to another tool surface without damaging the vacuum membrane. The intermediate sealing element forms a continuous path around the periphery of a vacuum membrane and is sealed directly to one or more vacuum membranes and a tool surface using any means known in the art to create an airtight seal between two surfaces. The intermediate sealing element is able to withstand high temperatures and high pressure without altering its structural characteristics. Because of its durability, the intermediate sealing element can be removed from the tool surface without tearing or elongating, subsequently allowing the vacuum membranes to be detached from the tool surface without tearing or elongating.

Abstract: A multilayer interlayer polymer film for use within and a high clarity and high efficiency fire-screen glazing or related fire-screen product uses a particular ordering of layers. The ordering of layers includes: (1) a core layer comprising one of a sulfur containing thermoplastic polymer material and a fluorine containing thermoplastic polymer material; (2) at least one intermediate layer laminated to the core layer and comprising the other of the sulfur containing thermoplastic polymer material and the fluorine containing thermoplastic polymer material; and (3) at least one skin layer laminated to the at least one intermediate layer and comprising a thermoplastic polyurethane material.

Abstract: A multilayer interlayer polymer film and a high clarity safety glass laminate made using the same include: (1) a core layer comprising one of an ionomer polymer material and a thermoplastic polyurethane polymer material; (2) at least one intermediate layer laminated to the core layer and comprising the other of the ionomer polymer material and the thermoplastic polyurethane polymer material; and (3) at least one skin layer laminated to the at least one intermediate layer and comprising a non-ionomer polyolefin polymer material. The multilayer interlayer polymer film provides the high clarity safety glass laminate with enhanced performance with respect to optical properties and manufacturability. In an alternative embodiment the at least one skin layer may be omitted when the intermediate layer comprises a thermoplastic polyurethane material with adequate adhesion to glass.

Abstract: A method of applying sealant to a narrow, deep gap in a surface includes covering the gap to form a covered channel, inserting a flared end of a dispensing nozzle into the covered gap at a first location, and applying a vacuum to the covered gap at a second location while using the nozzle to inject the sealant into the gap at the first location. This method may be used to seal gaps between ablative elements of a heat shield.

Abstract: A method for creating a vacuum setup for processing a semi-finished fiber composite into a cured fiber composite component is provided. The semi-finished fiber composite is positioned on a molding surface of a tool so that a non-planar surface of the semi-finished fiber composite faces away from the molding surface, covering the non-planar surface of the semi-finished fiber composite by applying an air-tight film and sealing the film with respect to the molding surface of the tool. Application of the film is performed using a plunger formed from a flexible material and having a plunger surface on which the film is retained.

Abstract: An improved wafer-to-wafer bonding method includes aligning an upper and a lower wafer and initiating a bond at a single point by applying pressure to a single point of the upper wafer via the flow of pressurized gas through a port terminating at the single point. The bond-front propagates radially across the aligned oppositely oriented wafer surfaces at a set radial velocity rate bringing the two wafer surfaces into full atomic contact by controlling the gas pressure and/or controlling the velocity of the motion of the lower wafer up toward the upper wafer.

Abstract: An autoclave may be reconfigured to accommodate differently shaped parts by relatively rotating portions of the autoclave.