JPS6448667A - Production of honeycomb structure - Google Patents
Production of honeycomb structureInfo
- Publication number
- JPS6448667A JPS6448667A JP20615087A JP20615087A JPS6448667A JP S6448667 A JPS6448667 A JP S6448667A JP 20615087 A JP20615087 A JP 20615087A JP 20615087 A JP20615087 A JP 20615087A JP S6448667 A JPS6448667 A JP S6448667A
- Authority
- JP
- Japan
- Prior art keywords
- plate
- thermal spraying
- coating layer
- brazing
- filler metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Laminated Bodies (AREA)
Abstract
PURPOSE:To reinforce the adhesive strength with a plate without any defect at the joining part which is compact and thin in the thickness, and to eliminate the need for tacking by executing the thermal spray of the powder of a brazing filler metal at high speed and high heat by a plasma thermal spraying device and executing brazing by forming the coating layer thereof. CONSTITUTION:The powder of a brazing filler metal A is subjected to thermal spraying to plate-like or currugated sheet-like plate 2 or 3 by the thermal spraying gun 4 of a plasma thermal spraying device 1 to form the coating layer of the brazing filler metal A at the specified part. Since the coating layer is formed by the high speed and high heat thermal spray, the need for tacking is eliminated, no org. solvent is contaminated, the thickness can be thinned and the adhesive strength with the plate 2 or 3 becomes stronger. Then after abutting the plate 2 or 3 to other plate 2 or 3, both are partially joined by heating at brazing stage. The honeycomb structure 15 like a corrugated tube thus manufactured is remarkably improved in its quality and performance aspects of the uniformity, strength, stability, etc., of the cell.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62206150A JP2514043B2 (en) | 1987-08-18 | 1987-08-18 | Method for manufacturing honeycomb structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62206150A JP2514043B2 (en) | 1987-08-18 | 1987-08-18 | Method for manufacturing honeycomb structure |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6448667A true JPS6448667A (en) | 1989-02-23 |
JP2514043B2 JP2514043B2 (en) | 1996-07-10 |
Family
ID=16518624
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62206150A Expired - Lifetime JP2514043B2 (en) | 1987-08-18 | 1987-08-18 | Method for manufacturing honeycomb structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2514043B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5316997A (en) * | 1989-08-04 | 1994-05-31 | Showa Aircraft Industry Co., Ltd. | Heat resisting structure |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101916848B1 (en) * | 2017-07-25 | 2018-11-08 | 티아이엘씨 주식회사 | Improved panel and manufacturing method thereof |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62230474A (en) * | 1986-03-31 | 1987-10-09 | Sumitomo Precision Prod Co Ltd | Heat exchanger |
JPS6448697A (en) * | 1987-08-17 | 1989-02-23 | Showa Aircraft Ind | Production of honeycomb core |
-
1987
- 1987-08-18 JP JP62206150A patent/JP2514043B2/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62230474A (en) * | 1986-03-31 | 1987-10-09 | Sumitomo Precision Prod Co Ltd | Heat exchanger |
JPS6448697A (en) * | 1987-08-17 | 1989-02-23 | Showa Aircraft Ind | Production of honeycomb core |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5316997A (en) * | 1989-08-04 | 1994-05-31 | Showa Aircraft Industry Co., Ltd. | Heat resisting structure |
Also Published As
Publication number | Publication date |
---|---|
JP2514043B2 (en) | 1996-07-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3072225A (en) | Honeycomb sandwich structure | |
US4318965A (en) | Bi-metallic thermo-barrier material and method of welding | |
ATE12219T1 (en) | METAL-CERAMIC COMPONENT AND PROCESS FOR ITS MANUFACTURE. | |
SE8604949L (en) | TITANIUM COMPOSITION WITH POROS SURFACE AND PROCEDURES FOR MANUFACTURE ME | |
DE69635519D1 (en) | METHOD FOR PRODUCING A SOLAR-SENSITIVE SURFACE COATING | |
ATE2756T1 (en) | THERMAL SPRAYING PROCESS FOR THE MANUFACTURE OF POROUS BOILING SURFACES FROM ALUMINUM. | |
FR2430311A1 (en) | METHOD FOR MANUFACTURING A HEAT RESISTANT COMPOSITE PLATE | |
JPS6448667A (en) | Production of honeycomb structure | |
JPS6448671A (en) | Production of honeycomb structure | |
SE7905255L (en) | PROCEDURE FOR PREPARING A COMPOUND MATERIAL | |
JPS61144287A (en) | Production of aluminum base composite plate material | |
JPS5653886A (en) | Micro-strain pressure welding device of metals and ceramics and its method | |
JPS60244490A (en) | Production of clad steel plate | |
JPH04126355A (en) | Negative electrode for lithium cell and manufacture thereof | |
SU1106825A1 (en) | Method of gluing together heat-resistant materials | |
JPS6418574A (en) | Joining method for metal interposing thermal spray film | |
JPS56125228A (en) | Bonding between metal and glass | |
JPH02128832A (en) | Honeycomb structure | |
JPH04361841A (en) | Composite honeycomb structural material | |
JPS5671590A (en) | Diffusion welding method of ti and steel | |
SU825294A1 (en) | Multilayer panel production method | |
JP2606519B2 (en) | Method for manufacturing aluminum honeycomb panel | |
JPS61103580A (en) | Coating process of deal | |
JPH0475730A (en) | Manufacture of brazed honeycomb panel | |
JPS58125383A (en) | Eutectic pressure welding method |