US3698145A - Hollow structure with core of interwoven strips - Google Patents

Hollow structure with core of interwoven strips Download PDF

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US3698145A
US3698145A US60601A US3698145DA US3698145A US 3698145 A US3698145 A US 3698145A US 60601 A US60601 A US 60601A US 3698145D A US3698145D A US 3698145DA US 3698145 A US3698145 A US 3698145A
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Prior art keywords
strips
hollow structure
backing member
perforations
strip
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US60601A
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Paul Newman
Maxwell John Holland
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UK Secretary of State for Defence
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UK Secretary of State for Defence
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    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/40—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of a number of smaller components rigidly or movably connected together, e.g. interlocking, hingedly connected of particular shape, e.g. not rectangular of variable shape or size, e.g. flexible or telescopic panels
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62—Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00—Thermal insulation in general
    • F16L59/06—Arrangements using an air layer or vacuum
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/025—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
    • F28F3/027—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements with openings, e.g. louvered corrugated fins; Assemblies of corrugated strips
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
    • E04C2002/3444—Corrugated sheets
    • E04C2002/3461—Corrugated sheets with rectangular corrugations

Definitions

  • the strips are perforated and attached to a backing member either (a) with the perforations facing away from the backing member to act as an acoustic liner, or (b) with the perforations in contact with the backing member and aligned with perforations therein for supply of cooling fluid, so that the structure can be used as an impingement cooled heat shield.
  • the present invention relates to hollow structures and relates in particular to a hollow structure suitable for use as a lining for a wall.
  • a hollow structure comprises a plurality of strips of relatively rigid material each of which is formed into a rectangular wave-form and which are woven together to form a hollow structure having two opposite substantially continuous surfaces with chambers there-between.
  • the structure may be used as a liner for a wall and one of the surfaces may therefore be attached to a wall by any suitable means, for example riveting or spot welding.
  • the strips may be metallic, in which case the structure formed according to the invention is capable of withstanding high temperature gradients across it without distortion and is therefore suitable as a lining for hot gas ducts.
  • the structure is designed as a cooled liner for a wall exposed to high temperatures and one of the surfaces is perforated so that cooling fluid can be passed through the perforations to impingement cool the inside of the opposite surface which is exposed to high temperatures in use.
  • the perforated surface in this case is attached to a wall which is also perforated, the perforations being aligned, and cooling fluid is passed through the wall.
  • the wall to which the liner is attached is a surface of a honeycomb structure or other hollow structure, to the interior of which cooling fluid is supplied to effect said impingement cooling of the liner.
  • the structure is designed as an acoustic liner for a wall.
  • the structure may be made from metallic strips where the wall is exposed to high temperatures.
  • the structure may be made from plastic resinous or fiber re-inforced composite materials which are moulded into the rectangular wave-form. The structure is attached by one surface to the wall and the other surface is perforated. Sound pressure waves impinging on the wall therefore pass through the perforations and are attenuated in the chambers between the surfaces of the structure.
  • each strip is preferably square so that the chambers formed in the woven structure are square, otherwise strips of different widths would have to be used if chambers having sides of unequal length were required.
  • FIG. 1 is an exploded pictorial view of the parts of the structure and a backing plate.
  • FIG. 2 is a pictorial view of a structure assembled onto a hollow backing structure for use as an impingement cooled liner.
  • FIG. 3 is a pictorial view of a structure mounted on a single backing member and perforated for use as an acoustic liner.
  • FIG. 1 there is shown a backing plate 1 in which are formed a plurality of holes 2 for rivets (not shown), and three metal strips 3 and 4 which are bent into a square wave form.
  • the strips 3 and 4 are woven, in a manner very similar to cloth weaving, and are eventually disposed at right angles with the tops of the waves of one strip 3 corresponding with the bottoms of the waves of another strip 4, so that in the assembledform the strips form two substantially continuous, opposing surfaces with individual chambers in between (see FIG. 2).
  • the method of weaving is to start with two strips (3 and 4) which are to form the two edges of an assembly, and to rivet the strip 3 at the rivet hole 2a.
  • the adjacent strips 3 and 4 are then positioned and riveted at the holes 2b and 2c and the process continued until the whole structure has been built up.
  • a structure made in this way is capable of withstanding temperature differentials of up to 400C without buckling since the folded strips are capable of expansion without affecting the backing plate.
  • FIG. 2 there is shown an embodiment of the invention in which the structure forms a liner for an outer wall 10 and is cooled so that it can withstand even higher differentials.
  • the backing plate 1 forms one side ofthe outer wall 10 which itself is a sandwich construction having surfaces 1 and 11 spaced apart by a plurality of webs 12 which define passages for the flow of cooling air therebetween.
  • the metal strips 3 and 4 are perforated with cooling air holes 15 and rivet holes 16 prior to bending so that when they are bent into the correct form the perforations all lie on the same side of the wave form.
  • the structure When the structure is woven from the strips therefore it presents a perforated surface and an unperforated surface.
  • the backing sheet is also perforated with corresponding cooling air holes and rivet holes and the strips are woven and attached to the backing plate so that the perforated surfaces are in contact and the perforations aligned.
  • cooling fluid is passed along the spaces between the webs 12 in the outer wall, and passes through the perforations so that jets of cooling fluid impinge on the inside of the unperforated surface which is exposed to a high temperature.
  • An application for such a structure is as a liner for a jet pipe or exhaust cone of a gas turbine engine.
  • a liner for a jet pipe or exhaust cone of a gas turbine engine By impingement cooling the surface which is exposed to the exhaust gases the temperature difference across the liner can be brought down to the region of 400C, which the liner can withstand without distortion.
  • the hollow outer wall may be replaced by a honeycomb structure as long as apertures are provided for passing cooling air to the perforations in the liner.
  • the method of attachment may be by blind rivetting or spot welding, otherwise explosive rivets may be used.
  • FIG. 3 Another embodiment of the invention is shown in FIG. 3 wherein the structure is adapted to act as a sound absorbing structure.
  • metal strips 3 and 4 are woven together and attached by rivets to a backing plate 1 but in this case perforations are formed in the opposite side of the wave to the rivet holes so that the perforated surface is exposed to a gas stream in use.
  • the perforations should cover approximately one quarter of the surface area of the surface of the liner.
  • the chambers formed between the surfaces of the liner have metallic walls and the energy in sound waves entering the chambers through the perforations is destroyed by reflection from the walls and turbulence in the chamber.
  • a liner constructed from folded metal strips has the capability of withstanding thermal gradients across it as described above and can therefore be used as an acoustic liner for jet pipes of gas turbine engines.
  • the liner may be formed from moulded plastic strips or fiber reinforced resin materials which can be bonded to a backing plate.
  • a hollow structure comprising a plurality of Iongitudinally and transversely arranged and interwoven strips of relatively rigid material, said strips being of the same width and each strip being of a rectangular waveform so that each strip has successive top and bottom portions lying in spaced apart parallel planes and interconnected by vertical web portions, the longitudinal strips and the transverse strips being interwoven in such a manner that the top portions of any one longitudinal strip overlie aligned bottom portions of adjacent transverse strips, and the bottom portions of said longitudinal strip are overlaid by top portions of said adjacent transverse strips, each top portion of any strip being congruent with the bottom portion overlaid by it, and all of the vertical web portions being of the same height, said interwoven strips forming substantially closed chambers in which each web forms a common wall for two adjacent chambers, and all the top and bottom portions of the strips being contiguous with the top and bottom portions respectively of the adjacent longitudinal and transverse strips to form two continuous surfaces in spaced apart parallel planes.
  • a hollow structure according to claim 4 and wherein the backing member comprises two spaced apart walls with passages therebetween for the supply of a cooling fluid to the perforations.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • General Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Electromagnetism (AREA)
  • Acoustics & Sound (AREA)
  • Thermal Sciences (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)

Abstract

A liner for a wall is made from strips of rigid material bent into a rectangular wave form and woven to form two substantially plane surfaces with chambers in between. The strips are perforated and attached to a backing member either (a) with the perforations facing away from the backing member to act as an acoustic liner, or (b) with the perforations in contact with the backing member and aligned with perforations therein for supply of cooling fluid, so that the structure can be used as an impingement cooled heat shield.

Description

United States Patent Newman et al.
[54] HOLLOW STRUCTURE WITH COR OF INTERWOVEN STRIPS [72] Inventors: Paul Newman; Maxwell John Holland, both of Filton, England [73] Assignee: Secretary of State for Defence, Lon don, England 22 Filed: Aug. 3, 1970 [21] Appl. No.: 60,601
[30] Foreign Application Priority Data Aug. 18, 1969 Great Britain ..4l,l30/69 [52] US. Cl. ..52/144, 52/173, 52/505, 52/618,161/68,161/l35,161/113 [51] Int. Cl ..E04b 1/82, E04b 2/14 [58] Field of Search ..161/68, 113,127,135, 70; 52/144, 145, 505, 613, 615, 618, 622, 626,
[56] 1 References Cited UNlTED STATES PATENTS 3,318,064 5/1967 Mayfield et a1 ..52/613 1 Oct. 17, 1972 3,214,321 10/1965 Graham ..161/131 FOREIGN PATENTS OR APPLICATIONS 1,484,323 3/1969 Germany ..52/618 1,166,394 6/1958 France ..52/145 28,213 4/1964 East Germany ..52/618 Primary Examiner-Alfred C. Perham Attorney-Mawhinney & Mawhinney [57] ABSTRACT A liner for a wall is made from strips of rigid material bent into a rectangular wave form and woven to form two substantially plane surfaces with chambers in between. The strips are perforated and attached to a backing member either (a) with the perforations facing away from the backing member to act as an acoustic liner, or (b) with the perforations in contact with the backing member and aligned with perforations therein for supply of cooling fluid, so that the structure can be used as an impingement cooled heat shield.
8 Claims, 3 Drawing Figures PATENIEDH 1 I97? 3, 698 14S sum 1 OF 3 lNVEI/TO 8 PAUL NEWMAN firm.
BY M A Q 7 khW-un,
ATTFI.
PATENTEDUBT 11 I912 3.698.145
SHEET 3 UF 3 v MW MMR PAUL NEWMAN ETAL BY )1! r n Arm.
HOLLOW STRUCTURE WITH CORE OF INTERWOVEN STRIPS The present invention relates to hollow structures and relates in particular to a hollow structure suitable for use as a lining for a wall.
According to the present invention a hollow structure comprises a plurality of strips of relatively rigid material each of which is formed into a rectangular wave-form and which are woven together to form a hollow structure having two opposite substantially continuous surfaces with chambers there-between.
The structure may be used as a liner for a wall and one of the surfaces may therefore be attached to a wall by any suitable means, for example riveting or spot welding.
The strips may be metallic, in which case the structure formed according to the invention is capable of withstanding high temperature gradients across it without distortion and is therefore suitable as a lining for hot gas ducts.
In one embodiment of the invention the structure is designed as a cooled liner for a wall exposed to high temperatures and one of the surfaces is perforated so that cooling fluid can be passed through the perforations to impingement cool the inside of the opposite surface which is exposed to high temperatures in use. The perforated surface in this case is attached to a wall which is also perforated, the perforations being aligned, and cooling fluid is passed through the wall.
In a preferred form of the invention the wall to which the liner is attached is a surface of a honeycomb structure or other hollow structure, to the interior of which cooling fluid is supplied to effect said impingement cooling of the liner.
In another embodiment of the invention the structure is designed as an acoustic liner for a wall. In this case the structure may be made from metallic strips where the wall is exposed to high temperatures. Alternatively the structure may be made from plastic resinous or fiber re-inforced composite materials which are moulded into the rectangular wave-form. The structure is attached by one surface to the wall and the other surface is perforated. Sound pressure waves impinging on the wall therefore pass through the perforations and are attenuated in the chambers between the surfaces of the structure.
The wave-form of each strip is preferably square so that the chambers formed in the woven structure are square, otherwise strips of different widths would have to be used if chambers having sides of unequal length were required.
The word rectangular in this context should be taken to include the special case of a square, which is a rectangle having sides of equal length.
The invention will now be more particularly described, merely by way of example, with reference to the accompanying drawings in which:
FIG. 1 is an exploded pictorial view of the parts of the structure and a backing plate.
FIG. 2 is a pictorial view of a structure assembled onto a hollow backing structure for use as an impingement cooled liner.
FIG. 3 is a pictorial view of a structure mounted on a single backing member and perforated for use as an acoustic liner.
Referring now to FIG. 1 there is shown a backing plate 1 in which are formed a plurality of holes 2 for rivets (not shown), and three metal strips 3 and 4 which are bent into a square wave form. The strips 3 and 4 are woven, in a manner very similar to cloth weaving, and are eventually disposed at right angles with the tops of the waves of one strip 3 corresponding with the bottoms of the waves of another strip 4, so that in the assembledform the strips form two substantially continuous, opposing surfaces with individual chambers in between (see FIG. 2).
Simultaneously with the weaving process the strips are riveted to the backing plate 1.
The method of weaving is to start with two strips (3 and 4) which are to form the two edges of an assembly, and to rivet the strip 3 at the rivet hole 2a. The adjacent strips 3 and 4 are then positioned and riveted at the holes 2b and 2c and the process continued until the whole structure has been built up. A structure made in this way is capable of withstanding temperature differentials of up to 400C without buckling since the folded strips are capable of expansion without affecting the backing plate.
Turning now to FIG. 2 there is shown an embodiment of the invention in which the structure forms a liner for an outer wall 10 and is cooled so that it can withstand even higher differentials. The backing plate 1 forms one side ofthe outer wall 10 which itself is a sandwich construction having surfaces 1 and 11 spaced apart by a plurality of webs 12 which define passages for the flow of cooling air therebetween.
The metal strips 3 and 4 are perforated with cooling air holes 15 and rivet holes 16 prior to bending so that when they are bent into the correct form the perforations all lie on the same side of the wave form. When the structure is woven from the strips therefore it presents a perforated surface and an unperforated surface.
The backing sheet is also perforated with corresponding cooling air holes and rivet holes and the strips are woven and attached to the backing plate so that the perforated surfaces are in contact and the perforations aligned.
In use, cooling fluid is passed along the spaces between the webs 12 in the outer wall, and passes through the perforations so that jets of cooling fluid impinge on the inside of the unperforated surface which is exposed to a high temperature.
An application for such a structure is as a liner for a jet pipe or exhaust cone of a gas turbine engine. By impingement cooling the surface which is exposed to the exhaust gases the temperature difference across the liner can be brought down to the region of 400C, which the liner can withstand without distortion.
The hollow outer wall may be replaced by a honeycomb structure as long as apertures are provided for passing cooling air to the perforations in the liner.
Where the opposite side of the base plate is accessible the method of attachment may be by blind rivetting or spot welding, otherwise explosive rivets may be used.
Another embodiment of the invention is shown in FIG. 3 wherein the structure is adapted to act as a sound absorbing structure.
As in the previous embodiments metal strips 3 and 4 are woven together and attached by rivets to a backing plate 1 but in this case perforations are formed in the opposite side of the wave to the rivet holes so that the perforated surface is exposed to a gas stream in use. The perforations should cover approximately one quarter of the surface area of the surface of the liner.
The chambers formed between the surfaces of the liner have metallic walls and the energy in sound waves entering the chambers through the perforations is destroyed by reflection from the walls and turbulence in the chamber.
A liner constructed from folded metal strips has the capability of withstanding thermal gradients across it as described above and can therefore be used as an acoustic liner for jet pipes of gas turbine engines.
In cases where there is no temperature gradient to resist, the liner may be formed from moulded plastic strips or fiber reinforced resin materials which can be bonded to a backing plate.
We claim:
1. A hollow structure comprising a plurality of Iongitudinally and transversely arranged and interwoven strips of relatively rigid material, said strips being of the same width and each strip being of a rectangular waveform so that each strip has successive top and bottom portions lying in spaced apart parallel planes and interconnected by vertical web portions, the longitudinal strips and the transverse strips being interwoven in such a manner that the top portions of any one longitudinal strip overlie aligned bottom portions of adjacent transverse strips, and the bottom portions of said longitudinal strip are overlaid by top portions of said adjacent transverse strips, each top portion of any strip being congruent with the bottom portion overlaid by it, and all of the vertical web portions being of the same height, said interwoven strips forming substantially closed chambers in which each web forms a common wall for two adjacent chambers, and all the top and bottom portions of the strips being contiguous with the top and bottom portions respectively of the adjacent longitudinal and transverse strips to form two continuous surfaces in spaced apart parallel planes.
2. A hollow structure according to claim 1 and wherein one of said surfaces is attached to a backing member which is in the form of a ducting and the other one of which presents a smooth surface to a flow of fluid in the ducting.
3. A hollow structure according to claim 2 and wherein the strips are metallic and are rivetted onto a backing plate.
4. A hollow structure according to claim 2 and wherein means are provided defining perforations in both the backing member and in one of the surfaces formed by the strips and the strips are attached to the backing member so that said one perforated surface contacts the backing member with the perforations in the surface aligned with those in the backing member for the passage therethrough of a cooling fluid.
5. A hollow structure according to claim 4 and wherein the backing member comprises two spaced apart walls with passages therebetween for the supply of a cooling fluid to the perforations.
6. A hollow structure according to claim 1 and wherein means are provided defining perforations in one of the surfaces formed by the strips, and a backing member attached to the other of the surfaces formed by the strip.
7. A hollow structure according to claim 6 and wherein the areas of the perforations total substantially one quarter of the area of the surface.
8. A hollow structure as claimed in claim 6 and in which the strips are made from a non-metallic material.

Claims (8)

1. A hollow structure comprising a plurality of longitudinally and transversely arranged and interwoven strips of relatively rigid material, said strips being of the same width and each strip being of a rectangular wave-form so that each strip has successive top and bottom portions lying in spaced apart parallel planes and interconnected by vertical web portions, the longitudinal strips and the transverse strips being interwoven in such a manner that the top portions of any one longitudinal strip overlie aligned bottom portions of adjacent transverse strips, and the bottom portions of said longitudinal strip are overlaid by top portions of said adjacent transverse strips, each top portion of any strip being congruent with the bottom portion overlaid by it, and all of the vertical web portions being of the same height, said interwoven strips forming substantially closed chambers in which each web forms a common wall for two adjacent chambers, and all the top and bottom portions of the strips being contiguous with the top and bottom portions respectively of the adjacent longitudinal and transverse strips to form two continuous surfaces in spaced apart parallel planes.
2. A hollow structure according to claim 1 and wherein one of said surfaces is attached to a backing member which is in the form of a ducting and the other one of which presents a smooth surface to a flow of fluid in the ducting.
3. A hollow structure according to claim 2 and wherein the strips are metallic and are rivetted onto a backing plate.
4. A hollow structure according to claim 2 and wherein means are provided defining perforations in both the backing member and in one of the surfaces formed by the strips and the strips are attached to the backing member so that said one perforated surface contacts the backing member with the perforations in the surface aligned with those in the backing member for the passage therethrough of a cooling fluid.
5. A hollow structure according to claim 4 and wherein the backing member comprises two spaced apart walls with passages therebetween for the supply of a cooling fluid to the perforations.
6. A hollow structure according to claim 1 and wherein means are provided defining perforations in one of the surfaces formed by the strips, and a backing member attached to the other of the surfaces formed by the strip.
7. A hollow structure according to claim 6 and wherein the areas of the perforations total substantially one quarter of the area of the surface.
8. A hollow structure as claimed in claim 6 and in which the strips are made from a non-metallic material.
US60601A 1969-08-18 1970-08-03 Hollow structure with core of interwoven strips Expired - Lifetime US3698145A (en)

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GB41130/69A GB1300409A (en) 1969-08-18 1969-08-18 Improvements in hollow wall structures

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Cited By (12)

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US3808394A (en) * 1972-03-31 1974-04-30 Anjac Plastics Creating holes in flexible members
US3895152A (en) * 1973-12-26 1975-07-15 Continental Oil Co A composite cellular construction
US4011703A (en) * 1974-06-27 1977-03-15 Umberto Tanzilli Building element for making insulating panels and panels assembled therefrom
US4023617A (en) * 1973-12-26 1977-05-17 Continental Oil Company Construction having integral circulatory system
US4317503A (en) * 1978-11-17 1982-03-02 Ingemanssons Ingenjorsbyra Ab Sound insulating building element
US4858401A (en) * 1984-07-08 1989-08-22 Thorp Graham M Cable ducting system
US5800905A (en) * 1990-01-22 1998-09-01 Atd Corporation Pad including heat sink and thermal insulation area
US20030009965A1 (en) * 2000-09-07 2003-01-16 Setuya Matumoto Residential heat insulation construction, and heat insulator to be used
US20050279045A1 (en) * 2003-11-20 2005-12-22 Shannon Jaeger Plurality of tiles
US20090307996A1 (en) * 2005-10-28 2009-12-17 Johann Berger Building Board or the Like, Its Manufacture and Use
WO2012006183A3 (en) * 2010-06-29 2013-08-08 H2Safe, Llc Fluid container
US9650195B2 (en) 2014-10-24 2017-05-16 H2Safe, Llc Fail-safe containment device for containing volatile fluids

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US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall
DE19714147A1 (en) * 1997-04-05 1998-10-08 Albrecht Dr Ing Hille Composite material for erection of walls
CN105043155B (en) * 2015-07-24 2017-01-18 北京航空航天大学 Conical-cylinder type vortex fin

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FR1166394A (en) * 1956-02-18 1958-11-05 Gomma Antivibranti Applic Combination resonator panels for sound absorbing coverings
US3214321A (en) * 1962-11-16 1965-10-26 Harold E Graham Plastic structural member and method of making same
US3318064A (en) * 1963-11-15 1967-05-09 Gen Dynamics Corp Thermal insulation system
DE1484323A1 (en) * 1963-03-08 1969-03-13 Messerschmitt Werke Flugzeug U Rigid, plate-shaped component and method for producing the stiffening layer

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DD28213A (en) *
FR1166394A (en) * 1956-02-18 1958-11-05 Gomma Antivibranti Applic Combination resonator panels for sound absorbing coverings
US3214321A (en) * 1962-11-16 1965-10-26 Harold E Graham Plastic structural member and method of making same
DE1484323A1 (en) * 1963-03-08 1969-03-13 Messerschmitt Werke Flugzeug U Rigid, plate-shaped component and method for producing the stiffening layer
US3318064A (en) * 1963-11-15 1967-05-09 Gen Dynamics Corp Thermal insulation system

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3808394A (en) * 1972-03-31 1974-04-30 Anjac Plastics Creating holes in flexible members
US3895152A (en) * 1973-12-26 1975-07-15 Continental Oil Co A composite cellular construction
US4023617A (en) * 1973-12-26 1977-05-17 Continental Oil Company Construction having integral circulatory system
US4011703A (en) * 1974-06-27 1977-03-15 Umberto Tanzilli Building element for making insulating panels and panels assembled therefrom
US4317503A (en) * 1978-11-17 1982-03-02 Ingemanssons Ingenjorsbyra Ab Sound insulating building element
US4858401A (en) * 1984-07-08 1989-08-22 Thorp Graham M Cable ducting system
US5800905A (en) * 1990-01-22 1998-09-01 Atd Corporation Pad including heat sink and thermal insulation area
US20030009965A1 (en) * 2000-09-07 2003-01-16 Setuya Matumoto Residential heat insulation construction, and heat insulator to be used
US7024832B2 (en) * 2000-09-07 2006-04-11 Matumotokenkou Kabushiki Kaisha Thermal insulation structure of housing and heat shielding member used for same
US20050279045A1 (en) * 2003-11-20 2005-12-22 Shannon Jaeger Plurality of tiles
US20090307996A1 (en) * 2005-10-28 2009-12-17 Johann Berger Building Board or the Like, Its Manufacture and Use
WO2012006183A3 (en) * 2010-06-29 2013-08-08 H2Safe, Llc Fluid container
CN103339461A (en) * 2010-06-29 2013-10-02 H2赛弗有限公司 Fluid container
US10578247B2 (en) 2010-06-29 2020-03-03 H2Safe, Llc Fluid container
US9650195B2 (en) 2014-10-24 2017-05-16 H2Safe, Llc Fail-safe containment device for containing volatile fluids

Also Published As

Publication number Publication date
FR2058342B1 (en) 1974-06-14
FR2058342A1 (en) 1971-05-28
GB1300409A (en) 1972-12-20
DE2040404A1 (en) 1971-02-25
SE361069B (en) 1973-10-15

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