JPS6448667A - Production of honeycomb structure - Google Patents

Production of honeycomb structure

Info

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
Application number
JP20615087A
Other languages
Japanese (ja)
Other versions
JP2514043B2 (en
Inventor
Tsutomu Muto
Tetsuo Toyoda
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Showa Aircraft Industry Co Ltd
Original Assignee
Showa Aircraft Industry Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Showa Aircraft Industry Co Ltd filed Critical Showa Aircraft Industry Co Ltd
Priority to JP62206150A priority Critical patent/JP2514043B2/en
Publication of JPS6448667A publication Critical patent/JPS6448667A/en
Application granted granted Critical
Publication of JP2514043B2 publication Critical patent/JP2514043B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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.
JP62206150A 1987-08-18 1987-08-18 Method for manufacturing honeycomb structure Expired - Lifetime JP2514043B2 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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