Abstract: At least one liquid tank has an outlet opening and a drain stub extending therefrom. A circular flange has plural connection openings with connection stubs respectively extending therefrom. A drain line is connected to the circular flange and communicates with all of the connection stubs. The drain stub of each tank is flange-connected to a respective connection stub extending from the circular flange. Unneeded connection stubs can be closed with blind flanges. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: At least one liquid tank has an outlet opening and a drain stub extending therefrom. A circular flange has plural connection openings with connection stubs respectively extending therefrom. A drain line is connected to the circular flange and communicates with all of the connection stubs. The drain stub of each tank is flange-connected to a respective connection stub extending from the circular flange. Unneeded connection stubs can be closed with blind flanges. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: At least one liquid tank has an outlet opening and a drain stub extending therefrom. A circular flange has plural connection openings with connection stubs respectively extending therefrom. A drain line is connected to the circular flange and communicates with all of the connection stubs. The drain stub of each tank is flange-connected to a respective connection stub extending from the circular flange. Unneeded connection stubs can be closed with blind flanges. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: At least one liquid tank has an outlet opening and a drain stub extending therefrom. A circular flange has plural connection openings with connection stubs respectively extending therefrom. A drain line is connected to the circular flange and communicates with all of the connection stubs. The drain stub of each tank is flange-connected to a respective connection stub extending from the circular flange. Unneeded connection stubs can be closed with blind flanges. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: A liquid tank has an outlet opening and a drain stub extends therefrom and has a circular-sector-shaped partial flange on its free end. At least one complementary flange adjoins and complements the partial flange to form a complete first circular flange. The complementary flange may be another partial flange with a throughhole connected to another tank, or a solid blind flange. The first circular flange is sealed and secured to a second circular flange connected to a single drain line. The two circular flanges may have the same diameter and the same aligned circle centerpoint. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: A liquid tank has an outlet opening in its bottom. A pipe-shaped drain stub extends from the outlet opening and has a circular-sector-shaped partial flange on its free end. At least one complementary flange adjoins and complements the partial flange to form therewith a complete first circular flange. The complementary flange may be another partial flange with a throughhole connected to another tank, or a solid blind flange. The first circular flange is sealed and secured to a second circular flange, which is further connected to a single drain line. The two circular flanges may have the same diameter and the same aligned circle centerpoint. Alternatively, the drain stub of each tank is flange-connected to a respective connection stub extending from a circular flange. This provides a modular reconfigurable system allowing a selected plurality of liquid tanks to be connected to a single drain line through the flange arrangement.

Abstract: Connectors for joining protective ducts and/or hoses for the installation of insulated electrical conductors and/or cables in an aircraft are equipped with lids that are easily opened even without a tool. The lids are preferably permanently secured to the connectors. The lids are constructed as roll-up tapes or as flat or curved plates. The curved plates are held in place in the closed condition by springs. A flat plate lid is held in place, for example by a circlip, or by a leg spring or by a hinge.

Abstract: A system of interconnected heating conductors, suitable for preventing freezing of water lines in an aircraft for example, includes a plurality of heater units (1, 12) electrically coupled together by respective coupling plugs (9, 10). Each heater unit comprises one or more heating conductor bands or cables (2, 21, 22), with a respective socket contact plug (9) connected to one end thereof and a respective pin contact plug (10) connected to the other end thereof. Each plug (9, 10) includes a housing (6) wherein the conductors of the heater band (2) are crimp-connected to electrical connectors (7), which include pin contacts (723) in the case of the pin contact plug (10) and socket contacts (77) in the case of the socket contact plug (9). The housing (6) is completely filled with a sealing compound (19) which is injected through a fill hole in the housing wall.

Abstract: A system of interconnected heating conductors, suitable for preventing freezing of water lines in an aircraft for example, includes a plurality of heater units (1, 12, 14) electrically coupled together by respective extension cables (3) and electrical coupling elements (42). Each heater unit comprises one or more heating conductor bands, tapes or strips (2, 21, 22) connected to respective connection modules (5, 51, 52, 52', 53) at the ends thereof. The connection modules may connect together several heater bands within one heater unit, and may connect the terminal ends of the heater bands of one heater unit to the extension cables by which several respective heater units may be connected together. Each connection module includes a housing (6) enclosing an inner chamber (61) therein, and at least one electrical connector element (7) such as a crimpable connector fixed within the housing (6).

Abstract: Connectors for joining protective ducts and/or hoses for the installation of insulated electrical conductors and/or cables in an aircraft are equipped with lids that are easily opened even without a tool. The lids are preferably permanently secured to the connectors. The lids are constructed as roll-up tapes or as a flat or curved plates. The curved plates are held in place in the closed condition by springs. A flat plate lid is held in place, for example by a circlip, or by a leg spring or by a hinge.

Abstract: A connector element is provided for variably laying and protecting insulated electrical conductors or cables for interconnecting the electrotechnical devices and lightning protective systems in aircraft and spacecraft. The connector element (29) includes a protective corrugated hose (25) connected to a screw-on component (1) by a collar nut (3) screwed onto the screw-on component (1). The collar nut (3) engages a flange (26A) on an end of the hose (25) and clamps it against the screw-on component (1). Insulated electrical conductors or cables (8) are guided through the hose (25), which is conductively connected to the aircraft structure. The hose (25) serves to protect, hold, and guide the electrical cables (8) in a desired configuration. The corrugated hose (25) includes a compressed portion (25A) with a small corrugation spacing, whereby the hose (25) is bendable into a desired configuration, yet is form-retaining and flexurally stiff to maintain the bent configuration.

Abstract: A clamp for securing a protection hose to an electrical connector is formed as a cuff with a longitudinal gap. The cuff has an inherent bias which normally tends to close the gap. The cuff is provided with tool insertion elements for widening the gap to insert the protection hose into the cuff. When a tool is released the inherent bias generates force components so directed that the cuff will clamp the hose between the connector and the cuff. The tool insertion elements may also be used for electrically grounding the cuff made of electrically conducting material.

Abstract: A conductor channel is used for the laying of insulated electrical conductors (3) in an air- or spacecraft, whereby the channel can be integrated into a conductor channel system. The conductor channel is made of at least one open hollow section (2), wherein the conductors (3) are held by a retaining strip (8) held in place by edges (7) of the hollow section (2). The strip (8) closes the hollow section. A tension relief element (11) for the conductors (3) is arranged at each channel end. A mounting (13) having upper and lower parts (20, 20') for electrically grounding the hollow section (2) is installed to hold the hollow section (2) next to each tension relief element (11). Spacers (14) may be distributed between the two mountings (13) along the length of the hollow section (2). The mountings (13) are fastened to a support (23). The hollow section (2) is fixed in and fastened to the mountings (13), whereby the free ends of the hollow section .

Abstract: A two-part screw-type coupling suitable for coupling together electrical and/or mechanical components in an aircraft, for example, has a rotation lock feature that prevents the unintentional spontaneous loosening of the screwed connection as a result of vibration and shock. The coupling includes a generally cylindrical support body and a collar nut rotatably mounted thereon and retained by a retaining element. A rotation lock element locks the collar nut and the support body together against relative rotation. The lock element includes a spring or a spring-loaded ring, which is rigidly connected to the collar nut or the support body and which applies a sufficient clamping tension against the other part of the coupling to achieve the desired locking function. The rotation lock can provide a finely stepped static adjustment and locking, or a fine step-less dynamic adjustment and locking of the tightening torque of the collar nut on a component to which the coupling is screw-connected.

Abstract: A cable end with its terminal or connector is maintained in a curved installed position with the aid of a bent retaining jacket (25A). The jacket is preferably a corrugated metal hose having one end formed into a bushing that is clamped in place on a support body of the connector or terminal together with other cable components such as a protective hose system. The bend maintaining jacket has an inner diameter that is larger than the outer diameter of the protection hose system of the cable so that the jacket may be freely pushed over the cable end prior to the installation of the terminal or connector. The opposite end of the jacket remains open or rather unconnected, thus enabling the jacket to accommodate any twists that result from bending the cable end. Although the jacket is bendable, it has a bend retaining characteristic that will not change its curved configuration in response to impacts, vibrations, or the like. Only an intentional renewed bending can bring the jacket into a new curved shape.

Abstract: An electrical and mechanical cable connector is constructed for maintaining an electrical grounding circuit in electrical installations on board of an aircraft. For this purpose the connector has two bodies positioned coaxially to each other and rotatable to each other but restrained against relative axial movement by a spring ring. One of the two bodies has a plurality of contact springs formed by cutting axial slots integrally into a portion of the one body. The body with the contact springs rests at least partly in or on the respective support body. Both bodies have a common central axis and contact pressures are effective radially inwardly or radially outwardly relative to the common central axis and are axially distributed along the central axis, whereby both bodies are electrically interconnected to maintain the grounding circuit.

Abstract: Elongated components such as electrical wiring, electrical cables, piping, rods, ropes, and steel cables are mounted in place, for example, in an aircraft body, by a mounting device that has at least two mounting sections. At least one, preferably both mounting sections are provided with component holding channels. When the two mounting sections are held together they form a block in which the components are held in the respective through-going channels. The mounting block is locked to a support, such as a wall member. The closing and thus the connection of the two mounting sections to each other and the clamping of the elongated components in the channels as well as the locking of the device to the support is accomplished by a mechanism that performs all three functions. In one embodiment the mechanism includes a connecting bolt holding at one end an expander dowel and on its threaded other end a clamping nut, whereby the expander dowel is expanded by a pulling action.

Abstract: Electrical and optical couplings are provided in a common housing for electrically and optically interconnecting respective cable ends. Such cables have a central optical conductor surrounded by an electrical conductor, preferably a wire mesh conductor. The coupling components cooperate with each other for providing a secure electrical connection and a precise optical coupling, while simultaneously protecting the optical conductor against damage and against excessive bending. The electrical connection and the optical coupling are separate and do not interfere with each other.

Abstract: A nut and a screw bolt form a screw connector, wherein the nut is secured to the bolt by a configured spring locking member. The locking member engages with one end the screw bolt and with the other end the nut, whereby the locking member has such a configuration that one end has a projection to engage a cotter pin hole in the bolt, while the other end engages directly or indirectly the nut. The two locking member ends are interconnected by a spring section which has such a configuration that a nut tightening torque moment is exerted on the nut when the locking member is in place. Further, the locking member is so configured that it exerts an axial compression force when its ends engage the bolt and the nut. This construction minimizes any reduction in the force exerted by the screw connector on the interconnected structural components.

Abstract: For protecting electrical installations against electromagnetic interferences and especially against over-voltages as can for instance occur as a consequence of lightning strikes, electrical lines provided between individual electrical apparatus are laid in a flexible hollow tubular member having an electrically conducting surface and at least one separation or division in its longitudinal direction. The hollow member is also provided with an undulated profile. The hollow member can be designed either as divided tubular sections or as cable channels or ducts provided with a covering member.