Multiple-layer wall for a hollow body and method for manufacturing same

• US 4,511,612 A
• Filed: 08/20/1982
• Issued: 04/16/1985
• Est. Priority Date: 08/21/1981
• Status: Expired due to Fees

• Current Assignee: MTU Motoren- und Turbinen-Union Muenchen GmbH (MTU)
• Original Assignee: MTU Motoren- und Turbinen-Union Muenchen GmbH (MTU)
• Inventors: Rossmann, Axel, Huther, Werner
• Primary Examiner(s): McCamish, Marion E.
• Assistant Examiner(s): NOT, DEFINED
• Application Number:
  US06/410,059
• Time in Patent Office: 970 Days
• Field of Search: 428/426, 428/489, 428/498, 428/428, 428/698, 428/701, 428/312.6, 428/312.8, 428/313.9, 428/314.2, 428/367, 428/450, 428/469, 428/697, 428/36, 501/95, 501/88, 501/98, 123/270, 123/271, 123/272, 123/193 R, 123/668, 123/669, 123/285, 264/60, 264/61
• US Class Current: 428/34.5
• CPC Class Codes: B22F 2998/00 Supplementary information concerning processes or compositions relating to powder metallurgy
• CPC Class Codes: B22F 7/062 involving the connection or repairing of preformed parts
• CPC Class Codes: B22F 7/08 with one or more parts not made from powder B22F7/062 takes precedence
• CPC Class Codes: C23C 28/00 Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
• CPC Class Codes: F02B 3/06 with compression ignition compression ignition engines using air or gas for blowing fuel into compressed air in cylinder F02B13/02
• CPC Class Codes: F02B 77/11 Thermal or acoustic insulation
• CPC Class Codes: F05C 2201/021 Aluminium
• CPC Class Codes: F05C 2201/0448 Steel
• CPC Class Codes: Y10T 29/49984 and casting
• CPC Class Codes: Y10T 428/1314 Contains fabric, fiber particle, or filament made of glass, ceramic, or sintered, fused, fired, or calcined metal oxide, or metal carbide or other inorganic compound [e.g., fiber glass, mineral fiber, sand, etc.]
• CPC Class Codes: Y10T 428/1317 Multilayer [continuous layer]
• CPC Class Codes: Y10T 428/2918 including free carbon or carbide or therewith [not as steel]

Abstract

A multiple-layer wall is provided for a hollow body to sustain high thermal and mechanical loads and to afford adequate thermal insulation. The wall has, on the inside, a heat and/or wear resistant ceramic inner layer and, surrounding it, a preferably prestressed retaining layer of fiber reinforced plastic. An intermediate layer of a thermally insulating ceramic material can also be provided. The wall can also have a retaining layer of metal. At least the retaining layer is shrink-fitted. The retaining layer of metal and/or the intermediate layer moreover can be deposited by a sintering process. Prestressing is achieved also by the shrinkage resulting from the sintering process. As a result of prestressing, the inner layer, when under internal pressure, comes under substantially no circumferential tension or under circumferential compression only. The wall is used especially with precombustion chambers of Diesel engines or with cylinder barrels or internal combustion engines.

Claims

1. A casing subjected to hot gases such as combustion gases of an engine and comprising a hollow body including a three-layer composite wall having a load side, said wall including a ceramic inner layer bounding said load side and an outer retaining layer of fiber-reinforced material or metal confining said inner layer, and further comprising an intermediate layer of thermally insulating ceramic material between said inner and retaining layers, said intermediate layer being shrinkfitted or sintered on to the inner layer, said retaining layer compressively prestressing said inner layer.

2. A casing as claimed in claim 1 wherein said ceramic inner layer is of silicon carbide or silicon nitride.

3. A casing as claimed in claim 1 or 2 wherein said retaining layer is a carbon fiber reinforced graphite.

4. A casing as claimed in claim 1 wherein said retaining layer is of highly heat-resistant steel.

5. A casing as claimed in claim 1 or 4 wherein said thermally insulating ceramic intermediate layer is lithium aluminum silicate, magnesium aluminum silicate, aluminum titanate or pyrolitic boron nitride.

6. A method for manufacturing a multiple-layer wall as claimed in claim 5 wherein the insulating ceramic intermediate layer is prepared by depositing a layer of sinterable insulating ceramic powder on the inner layer by isostatic pressing or by transfer molding and sintering the same.

7. A method as claimed in claim 6 wherein said outer retaining layer of metal is prepared by pouring the metal around the composite structure consisting of said inner and intermediate layers in a mold.

8. A method as claimed in claim 6 wherein said outer retaining layer of metal is prepared by depositing a layer of sinterable metal powder on the composite structure consisting of said inner and intermediate layers and sintering said powder.

9. A casing as claimed in claim 1 wherein said wall constitutes a pre-combustion chamber for a Diesel engine.

10. A casing as claimed in claim 9 wherein said multiple sections include inverse conical sections and a pelvis shaped section in abutting serial relationship.

11. A casing as claimed in claim 1 wherein said wall constitutes a cylinder barrel for an internal combustion engine.

12. A casing as claimed in claim 1 wherein said wall is divided into multiple sections along parallel planes.

13. A method for manufacturing a multiple-layer wall as claimed in claim 1 wherein said retaining layer is shrink-fitted on the assembly consisting of said inner and intermediate layers.

14. A casing as claimed in claim 1 wherein said ceramic inner layer has heat corrosion resistance at elevated temperatures and said intermediate ceramic layer is heat insulative to prevent heat loss.

15. A casing as claimed in claim 14 wherein said ceramic inner layer has low tensile strength and high compressive strength whereby the prestress of the retaining layer enables said ceramic inner layer to resist high internal pressures in said casing.