Abstract: A leading edge structure (11) for a flow control system of an aircraft (1), including a leading edge panel (13) surrounding a plenum (17) and having a first side portion (21), a second side portion (27), an inner surface (33) facing the plenum (17) and an outer surface (37) in contact with an ambient flow (39), wherein the leading edge panel (13) includes micro pores (45), wherein a first port device (49) is arranged in the first side portion (21) fluidly connected to the plenum (17) via a duct (53) defined by a duct structure (105), and wherein the first port device (49) comprises a first door (55) pivotable by a first hinge (57) about a first hinge axis (59).

Abstract: A leak testing apparatus is provided, for testing connections between tubes penetrating a plate material. A housing is disclosed having a central cylindrical longitudinal hollow. A piston arranged inside the housing, where a distal end of the piston in use is inserted into the tube. A seal arranged circumferentially on the piston, such that in use the second seal may be brought into sealing engagement with the tube. A second end of the housing is closed by an endcap where at least one channel is provided longitudinally in the piston and a connection to the channel allowing connection to a source of pressurized medium is provided, connecting the pressurized medium to a space, in use limited by the first seal, the plate material, the tube and the second seal, and optionally part of the piston and part of the housing.

Abstract: A leading edge structure (11) for a flow control system of an aircraft (1), including a leading edge panel (13) that surrounds a plenum (17), wherein the leading edge panel (13) has a first side portion (21), a second side portion (27), an inner surface (33) and an outer surface (37), wherein the leading edge panel (13) having micro pores (45) forming a fluid connection between the plenum (17) and the ambient flow (39), wherein a first air inlet/outlet device (49) is arranged in the first side portion (21) and a second air inlet outlet/device (51) is arranged in the second side portion (27), fluidly connected to the plenum (17), and wherein the first air inlet/outlet device (49) comprises a pivotable first door (55) and the second air inlet outlet/device (51) comprises a pivotable second door (61).

Abstract: A leading edge structure (1) for a flow control system of an aircraft (101) including a double-walled leading edge panel (3) surrounding a plenum (7). The leading edge panel (3) has a first side portion (11) extending to a first attachment end (17), a second side portion (13) extending to a second attachment end (19), an inner wall element (21) facing the plenum (7), an outer wall element (23) for contact with an ambient flow (25), a core assembly (97). The outer wall element (23) includes micro pores (31) forming a fluid connection between the core assembly (97) and the ambient flow (25). The inner wall element (21) includes openings (33) forming a fluid connection between the core assembly (97) and the plenum (7). The outer wall element (23) extends from the first attachment end (17) to the second attachment end (19).

Abstract: A leading edge structure (1) for a flow control system of an aircraft (101) including a double-walled leading edge panel (3) with a first side portion (11) extending to a first attachment end (17), a second side portion (13) extending to a second attachment end (19), an inner wall element (21) facing a plenum (7), an outer wall element (23) facing ambient flow (25), and a core assembly (97). The outer wall element (23) includes micro pores (31) and the inner wall element (21) includes openings (33) which form a fluid connection from ambient flow, through the core assembly (97) and to the plenum (7). The thickness of the outer wall element is reduced due to the first attachment end (17) and/or at the second attachment end (19) attached to the inner wall element (21) by both bonding and fasteners (85, 87, 89, 91).

Abstract: A leading edge structure (11) for a flow control system of an aircraft (1), including a leading edge panel (13) that surrounds a plenum (17), wherein the leading edge panel (13) has a first side portion (21), a second side portion (27), an inner surface (33) and an outer surface (37), wherein the leading edge panel (13) having micro pores (45) forming a fluid connection between the plenum (17) and the ambient flow (39), wherein a first air inlet/outlet device (49) is arranged in the first side portion (21) and a second air inlet outlet/device (51) is arranged in the second side portion (27), fluidly connected to the plenum (17), and wherein the first air inlet/outlet device (49) comprises a pivotable first door (55) and the second air inlet outlet/device (51) comprises a pivotable second door (61).

Abstract: A leading edge structure (11) for a flow control system of an aircraft (1), including a leading edge panel (13) surrounding a plenum (17) and having a first side portion (21), a second side portion (27), an inner surface (33) facing the plenum (17) and an outer surface (37) in contact with an ambient flow (39), wherein the leading edge panel (13) includes micro pores (45), wherein a first port device (49) is arranged in the first side portion (21) fluidly connected to the plenum (17) via a duct (53) defined by a duct structure (105), and wherein the first port device (49) comprises a first door (55) pivotable by a first hinge (57) about a first hinge axis (59).

Abstract: A leading edge structure for an aircraft flow control system includes a leading edge panel curvingly surrounding a plenum. The leading edge panel has a first side portion and a second side portion with an inner surface facing the plenum and an outer surface contacting an ambient flow. The leading edge panel includes a plurality of micro pores forming a fluid connection between the plenum and the ambient flow. An air outlet is arranged in the first or second side portion and is fluidly connected to the plenum for letting out air from the plenum into the ambient flow. The air outlet is formed as a fixed air outlet including an outlet panel extending in a fixed manner from the leading edge panel into the ambient flow, such that a rearward facing outlet opening is formed between the leading edge panel and a rear edge of the outlet panel.

Abstract: An information processing apparatus and a method for volume data visualization is provided. The information processing apparatus stores an auto-encoder that includes an encoder network and a decoder network. The encoder network includes a loss function and a first plurality of neural network (NN) layers. The information processing apparatus inputs volume data to an initial NN layer of the first plurality of NN layers and generates a latent image as an output from a final NN layer of the first plurality of NN layers based on application of the encoder network on the input volume data. The information processing apparatus estimates a distance between the generated latent image and a reference image based on the loss function and updates the encoder network based on the estimated distance. Finally, the information processing apparatus outputs the updated encoder network as a trained encoder network based on the estimated distance being a minimum.

Abstract: An illumination system for illuminating outer aircraft components of an airborne vehicle, such as an aircraft, includes a light projection system configured to project visual imagery to an outer surface of the airborne vehicle, and a projection controller having a light control processor configured to control the operation of the light projection system on the basis of at least one of operational flight status of the airborne vehicle, geographical location of the airborne vehicle and configuration data of movable surfaces of the airborne vehicle or on ambient light measurement.

Abstract: An information processing apparatus and a method for volume data visualization is provided. The information processing apparatus stores an auto-encoder that includes an encoder network and a decoder network. The encoder network includes a loss function and a first plurality of neural network (NN) layers. The information processing apparatus inputs volume data to an initial NN layer of the first plurality of NN layers and generates a latent image as an output from a final NN layer of the first plurality of NN layers based on application of the encoder network on the input volume data. The information processing apparatus estimates a distance between the generated latent image and a reference image based on the loss function and updates the encoder network based on the estimated distance. Finally, the information processing apparatus outputs the updated encoder network as a trained encoder network based on the estimated distance being a minimum.

Abstract: A display control apparatus includes: an image acquisition section that acquires a captured image obtained by imaging an imaging range; and a display control section that controls a display section in such a way that a virtual object corresponding to an imaging subject reflecting on the captured image is displayed. The display control section displays the virtual object in such a way that a ratio of an amount of movement of the virtual object in a virtual image to an amount of movement of the imaging range in real space changes according to an imaging magnification of the captured image.

Abstract: There is provided an information processing apparatus including an operation detection unit configured to detect an operation of a user, a display control unit configured to move and display first information formed by first components different from each other according to a movement operation of the user detected by the operation detection unit and to fix and display second information formed by second components different from each other, and an information acquisition unit configured to acquire, based on the selection operation, information regarding the second components displayed at positions corresponding to the first components based on a selection operation of the user detected by the operation detection unit.

Abstract: An image processing apparatus includes: an acquisition section configured to acquire positional information specified by a user on an input image for specifying area selection; and out of a calculation result of a transformation matrix between an object plane being a perspective projection plane formed by an object in the input image and an isothetic plane, a selected-area calculation section configured to calculate an area in the object plane as a selected area by the user using the transformation matrix of the object plane corresponding to the positional information specified by the user.

Abstract: [Object] To improve the usability for the user in the case of displaying a virtual object corresponding to an imaging area. [Solution] Provided is a display control apparatus including: an image acquisition section that acquires a captured image obtained by imaging an imaging range; and a display control section that controls a display section in such a way that a virtual object corresponding to an imaging subject reflecting on the captured image is displayed. The display control section displays the virtual object in such a way that a ratio of an amount of movement of the virtual object in a virtual image to an amount of movement of the imaging range in real space changes according to an imaging magnification of the captured image.

Abstract: Future fighting vehicles will require lighter, stronger and more space efficient armor for better protection, better survivability and better mobility. The invented lightweight armor component consists of armor-grade material (2), such as ceramic, encapsulated in fiber reinforced cementitious composite (FRCC) (1). The encapsulation FRCC pre-stress the armor-grade material. The resulting armor component of the present disclosure provides excellent ballistic protection against most types and sizes of Kinetic Energy (KE) threats and Chemical Energy (CE) threats. The armor component has low areal density, reduced damage area, improved multi-hit capability, flexible design and also provides high structural strength. It furthermore has the advantage, that it can be formed in virtually any shape. The present disclosure results in superior ballistic characteristics of an armor component.

Abstract: There is provided an information processing apparatus including an operation detection unit configured to detect an operation of a user, a display control unit configured to move and display first information formed by first components different from each other according to a movement operation of the user detected by the operation detection unit and to fix and display second information formed by second components different from each other, and an information acquisition unit configured to acquire, based on the selection operation, information regarding the second components displayed at positions corresponding to the first components based on a selection operation of the user detected by the operation detection unit.

Abstract: An image processing apparatus includes: an acquisition section configured to acquire positional information specified by a user on an input image for specifying area selection; and out of a calculation result of a transformation matrix between an object plane being a perspective projection plane formed by an object in the input image and an isothetic plane, a selected-area calculation section configured to calculate an area in the object plane as a selected area by the user using the transformation matrix of the object plane corresponding to the positional information specified by the user.

Abstract: A needle mounting system and methods for mounting a needle assembly on a needle mount are disclosed. The needle mounting system includes a needle hub having protrusions extending radially inward. A needle mount has a plurality of slots to receive the protrusions. The slots have a first portion that defines a passageway substantially parallel to a longitudinal axis of the needle mount and a second portion substantially perpendicular to the axis. The needle hub and mount provide a method wherein a needle assembly may be mounted on an injection device without completely rotating the needle hub relative to the needle mount.

Abstract: A needle mounting system and methods for mounting a needle assembly on a needle mount are disclosed. The needle mounting system includes a needle hub having protrusions extending radially inward. A needle mount has a plurality of slots to receive the protrusions. The slots have a first portion that defines a passageway substantially parallel to a longitudinal axis of the needle mount and a second portion substantially perpendicular to the axis. The needle hub and mount provide a method wherein a needle assembly may be mounted on an injection device without completely rotating the needle hub relative to the needle mount.