Patent classifications
F16L59/12
ASSEMBLY FOR AN AIRCRAFT NACELLE AND COMPRISING A SUPPORT PANEL, A THERMAL PROTECTION ELEMENT AND A FASTENING SYSTEM
An assembly including a support panel of an internal fixed structure, a thermal protection element and a plurality of fastening systems. Each fastening system includes a female part secured to the support panel and which has, in its interior, a circular shoulder, and a male part including a sleeve pierced with a main bore, a slide movable in translation in the main bore and a plurality of balls. For each ball, the sleeve has a secondary bore, and each ball is movable along the secondary bore between a locking position and an unlocking position. The slide is movable in translation between a blocking position and an unlocking position. Such an assembly makes it possible to fasten the thermal protection element to the support panel in a simple and rapid manner, also permitting easy removal if necessary.
Pipe insulation system
A pipe insulation system has a spacer wrap, an insulation material and a cladding. The spacer wrap has an upper surface and a lower surface. The upper surface of the spacer wrap has a plurality of convex protrusions. The upper surface is positioned against a pipe. The insulation material has an inner surface and an outer surface. The insulation material is positioned exterior to the lower surface of the spacer wrap. The cladding has an interior surface and an exterior surface. The cladding is positioned exterior to the outer surface of the insulation material.
Ultra-long thermally insulated pipeline and forming method thereof
The present invention provides an ultra-long thermally insulated pipeline, which includes a working steel pipe and an outer sleeve steel pipe sleeving the working steel pipe, where an annular vacuum cavity is formed between the working steel pipe and the outer sleeve steel pipe; two ends of the outer sleeve steel pipe are tightened; and the tightened parts of the outer sleeve steel pipe are sealed with an outer wall of the working steel pipe through a plurality of sealing rings. The ultra-long thermally insulated pipeline further includes a spiral ring supporting frame which is disposed outside the working steel pipe and is in contact with a wall of the working steel pipe. The spiral ring supporting frame is made of a phase change material The present invention further provides a forming method of an ultra-long thermally insulated pipeline.
Ultra-long thermally insulated pipeline and forming method thereof
The present invention provides an ultra-long thermally insulated pipeline, which includes a working steel pipe and an outer sleeve steel pipe sleeving the working steel pipe, where an annular vacuum cavity is formed between the working steel pipe and the outer sleeve steel pipe; two ends of the outer sleeve steel pipe are tightened; and the tightened parts of the outer sleeve steel pipe are sealed with an outer wall of the working steel pipe through a plurality of sealing rings. The ultra-long thermally insulated pipeline further includes a spiral ring supporting frame which is disposed outside the working steel pipe and is in contact with a wall of the working steel pipe. The spiral ring supporting frame is made of a phase change material The present invention further provides a forming method of an ultra-long thermally insulated pipeline.
Three-dimensional multi-shell insulation
A three-dimensional multi-shell insulation configured to conform to the shape of a spacecraft component to be insulated. The insulation may have a plurality of nested shell layers that are displaceable relative to each other for providing natural separation between the shell layers when the insulation is used in low-pressure and/or low-gravity space-related applications. To establish the spacing between shell layers, an edge clamp may be operatively coupled to an edge portion on at least one side of each shell layer. The shell layers may have sufficient flexibility and/or may be sufficiently displaceable relative to each other to allow the insulation to be installed or removed from the spacecraft component. One or more restraints may be provided in the space between the shell layers for restricting the relative lateral and/or transverse movement between shell layers for preventing contact. Additive manufacturing may be employed to fabricate the insulation and integrate features.
Flow pipe
There is provided a flow pipe including: a pipe body including a side wall having an opening portion; and a heat insulator arranged at an inner peripheral side of the pipe body and having a flow path through which a fluid flows. The heat insulator has an outer peripheral surface facing with the side wall, and the outer peripheral surface has a flow path structure configured to form a flow path that guides a water droplet generated between the heat insulator and the pipe body to the opening portion.
Insulating support bracket for jacketed pipe system
A saddle includes an arcuate central portion defining a first end and a second end opposite the first end; a first flange portion bent radially inward from the arcuate central portion at the first end; and a second flange portion bend radially inward from the arcuate central portion at the second end.
Thermoplastic polymeric foam pipe insulation
An article with at least two extruded thermoplastic polymer foam pieces that fit together to form a length of foam having a generally annular cross section, each piece having a concave surface such that the concave surfaces adjoin to form an internal edge defining a hole within the generally annular cross section; wherein each piece has a density less than 36 kilograms per cubic meter, a product of density times average cell size that is less than 17 millimeters*kilogram per cubic meter, and a thermal conductivity of 35 milliwatts per meter*Kelvin or less.
Thermoplastic polymeric foam pipe insulation
An article with at least two extruded thermoplastic polymer foam pieces that fit together to form a length of foam having a generally annular cross section, each piece having a concave surface such that the concave surfaces adjoin to form an internal edge defining a hole within the generally annular cross section; wherein each piece has a density less than 36 kilograms per cubic meter, a product of density times average cell size that is less than 17 millimeters*kilogram per cubic meter, and a thermal conductivity of 35 milliwatts per meter*Kelvin or less.
PIPE ARRANGEMENT WITH SUPPORT SECTIONS ON THE OUTER PIPE
The invention relates to a pipe arrangement (10) with a fluid-carrying inner pipe (12) and an outer pipe (14) that surrounds the inner pipe (12), wherein spacers (20, 24) are arranged between the inner pipe (12) and the outer pipe (14) in such a way that a gap (16) is formed between the inner pipe (12) and the outer pipe (14), wherein the outer pipe (14) is joined at its first axial end section (18) in a material-bonded or cohesive manner to a first spacer (20), which is joined to the inner pipe (12) in a material-bonded manner, and wherein the outer pipe (14) is arranged at its second axial end section (22) at least partially with a radial spacing (26) to a second spacer (24), which is joined to the inner pipe (12) in a material-bonded manner.