JPS5318888A - Tapered punching device - Google Patents

Tapered punching device

Info

Publication number
JPS5318888A
JPS5318888A JP9419576A JP9419576A JPS5318888A JP S5318888 A JPS5318888 A JP S5318888A JP 9419576 A JP9419576 A JP 9419576A JP 9419576 A JP9419576 A JP 9419576A JP S5318888 A JPS5318888 A JP S5318888A
Authority
JP
Japan
Prior art keywords
tapered
tip
punching device
reamer portion
reamer
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.)
Pending
Application number
JP9419576A
Other languages
Japanese (ja)
Inventor
Kazuo Hane
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.)
Kubota Corp
Original Assignee
Kubota Corp
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 Kubota Corp filed Critical Kubota Corp
Priority to JP9419576A priority Critical patent/JPS5318888A/en
Publication of JPS5318888A publication Critical patent/JPS5318888A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B51/00Tools for drilling machines
    • B23B51/08Drills combined with tool parts or tools for performing additional working

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Drilling Tools (AREA)

Abstract

PURPOSE:To effectively prevent the breakage at the blade tip of a tapered reamer portion by providing a reamer portion at the tip of a tapered reamer portion maintaining the same diameter, forming the blades of both reamer portions in the form of screw teeth, and providing a drill blade at the tip of the reamer portion of the same diameter, so that the cutting resistance is reduced.
JP9419576A 1976-08-06 1976-08-06 Tapered punching device Pending JPS5318888A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9419576A JPS5318888A (en) 1976-08-06 1976-08-06 Tapered punching device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9419576A JPS5318888A (en) 1976-08-06 1976-08-06 Tapered punching device

Publications (1)

Publication Number Publication Date
JPS5318888A true JPS5318888A (en) 1978-02-21

Family

ID=14103507

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9419576A Pending JPS5318888A (en) 1976-08-06 1976-08-06 Tapered punching device

Country Status (1)

Country Link
JP (1) JPS5318888A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011049095A1 (en) * 2009-10-21 2011-04-28 福井県 Drill for composite material as well as machining method using same and machining apparatus using same
FR2983422A1 (en) * 2011-12-01 2013-06-07 Airbus Operations Sas Bit for use on conical reaming tool used to drill and ream conical opening in skin surface of e.g. fuselage panel of aircraft, has front tip drilling surface, and conical central section and front tip extended in extension of each other
CN114112130A (en) * 2021-09-30 2022-03-01 河海大学 Device and method for repeatedly measuring stress intensity factor of crack tip

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011049095A1 (en) * 2009-10-21 2011-04-28 福井県 Drill for composite material as well as machining method using same and machining apparatus using same
JP2011104766A (en) * 2009-10-21 2011-06-02 Fukui Prefecture Drill for composite material, and machining method and apparatus using the same
CN102574219A (en) * 2009-10-21 2012-07-11 福井县 Drill for composite material as well as machining method using same and machining apparatus using same
FR2983422A1 (en) * 2011-12-01 2013-06-07 Airbus Operations Sas Bit for use on conical reaming tool used to drill and ream conical opening in skin surface of e.g. fuselage panel of aircraft, has front tip drilling surface, and conical central section and front tip extended in extension of each other
CN114112130A (en) * 2021-09-30 2022-03-01 河海大学 Device and method for repeatedly measuring stress intensity factor of crack tip

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