Rohr Patente

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A centerbody assembly (48) includes a center tube (56), a forward bulkhead (58), an aft bulkhead (60), at least one baffle (64), and an outer skin (52). The center tube (56) extends circumferentially about an axial centerline (34). The center tube (56) extends between and to a first axial tube end (88) and a second axial tube end (90). The forward bulkhead (58) is mounted to the center tube (56) at the first axial tube end (88). The aft bulkhead (60) is mounted to the center tube (56) at the second axial tube end (90). The at least one baffle (64) extends axially from the forward bulkhead (58) to the aft bulkhead (60). At least the forward bulkhead (58), the aft bulkhead (60), or the at least one baffle (64) include one or more thermal beads (112, 142). The outer skin (52) circumscribes the center tube (56), the forward bulkhead (58), the aft bulkhead (60), and the at least one baffle (64) to form an acoustic cavity (66) radially inside the outer skin (52).

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A shape forming tool (120) for pre-carbonization compression of a fibrous preform (110) includes a female forming tool (122) comprising a die recess (182), a first die half (126) configured to be received by the die recess, a second die half (128) configured to be received by the die recess, an expander tool coupled between the first die half and the second die half. The expander tool is configured to move the first die half laterally toward a first side of the female forming tool away from the second die half to compress the fibrous preform between the first die half and the female forming tool. The expander tool is further configured to move the second die half laterally toward a second side of the female forming tool away from the first die half to compress the fibrous preform between the second die half and the female forming tool.

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A nacelle (22) for a gas turbine engine (20) includes a fixed nacelle portion (48), a cowl panel (52), and a latch assembly. The fixed nacelle portion (48) extends circumferentially about an axial centerline. The cowl panel (52) is axially adjacent the fixed nacelle portion (48). The cowl panel (52) is moveable relative to the fixed nacelle portion (48) between an open position and a closed position. The latch assembly includes a first latch portion and a second latch portion. The first latch portion is mounted to the cowl panel (52). The first latch portion includes a pin configured for translation along a pin axis between an extended pin position and a retracted pin position. The second latch portion is mounted to the fixed nacelle portion (48). The second latch portion includes a pin guide. The pin guide is configured to receive and engage the pin with the pin in the extended position and the cowl panel (52) in the closed position.

A mechanical connection system is provided that includes a ceramic skin panel, at least one bushing, and at least one bolt. The ceramic skin panel includes a first surface, a second surface, and at least one aperture extending between the first surface and the second surface. The aperture has an axial centerline, a chamfered portion contiguous with the first surface, and an axial portion contiguous with the second surface. The chamfered portion includes a tapered surface disposed at a first angle such that a line extending along the tapered surface intersects the axial centerline at a plane of the second surface. The bushing has a housing and a collar. The housing is configured to mate with the chamfered portion of the aperture disposed within the ceramic skin panel. The collar is configured for engagement with the housing.

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An acoustic panel is provided that includes a perforated first skin, a second skin and a core. The core includes a first wall, a second wall and a stiffener. The core forms a plurality of cavities that extend vertically between the perforated first skin and the second skin and that extend laterally between the first wall and the second wall. The plurality of cavities include a first cavity. The stiffener projects partially into the first cavity and is connect to the first wall and the second wall.

A manufacturing method is provided. A preform is arranged over a surface of an inner mold line (100). The preform is folded over sides of the inner mold line (100). An end of the preform is pressed into a grip strip (804) coupled to a side of the inner mold line (100). The grip strip (804) is translated in a first direction to tension the preform into a shaped body.

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A latch mechanism (34) is provided that includes a latch housing (36), latch keeper (40), and a latch hook adjustment assembly (38). The latch hook adjustment assembly (38) includes a latch frame (44), latch handle (46), hook member (48), bearing block (50), a nut (52), and a spring member (54). The latch frame (44) has a front wall (56), an interior wall (66), and a forward cavity (70). The hook member (48) has a partially threaded shaft (84). The bearing block (50) has a flange (92), indexing features (96), and a bore. The flange (92) has opposing first and second side surfaces. The indexing features (96) project outwardly from the second side surface (102) and are disposed adjacent the bore. The nut (52) has first and second axial end surfaces (104, 106), a threaded nut bore (110), and index cavities (114) disposed in the first axial end surface (104) adjacent the nut bore (110). The bearing block (50), nut (52), and spring member (54) are disposed in the forward cavity (70). The latch hook adjustment assembly (38) is disposable in engaged and disengaged configurations.