← Back to Patent Explorer
US4529341A Expired / Lapsed US ⏱️ 0.0 years remaining

Drill bit for Kevlar laminates

Assignee: Boeing Co
•
Filing: 1982-09-29
•
Granted: 1985-07-16
•
Expires: 2002-09-29
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An improved drill bit for drilling Kevlar laminates or the like, has a pair of helical edges each terminating in an outer cutting point; a center point; and concavely curved cutting edges extending between the center point and each of the outer cutting point. The cutting edges curve back sharply from the cutting points in a plane transverse to the longitudinal drill bit axis and in a direction opposite to normal rotation of said drill bit so as to draw material served by the cutting points radially inwardly from the edge of a bore. A method is disclosed for modifying a conventional drill point to the novel configuration by grinding on a grinding wheel.

Inventors

  • 👤 Eddie A. Greene

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 00:28
CPC Classifications
B; B23; B23B; B23B51/00; B23B51/02; B23B2251/00; B23B2251/18; B23B2251/185; Y; Y10; Y10T; Y10T408/00; Y10T408/89; Y10T408/899; Y10T408/90; Y10T408/909; Y10T408/9095; Y10T408/9097

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 150 words
An improved drill bit for drilling Kevlar laminates or the like, said drill bit having a pair of helical leading edges each terminating in an outer cutting point; a center point; and concavely curved cutting edges extending between said center point and each said outer cutting point, said cutting edges curving back sharply from said cutting points as viewed along the longitudinal drill bit axis and in a direction opposite to normal rotation of said drill bit so as to draw material severed by said cutting points radially inwardly from the edge of a bore, said helical leading edges having a reduced rake angle along a leading edge segment adjacent to said cutting points relative to the rake angle of said leading edges along portions removed from said outer cutting points to thereby increase the shearing effect of said edges and minimize lifting of workpiece material by said leading edges.
Claim 2
Dependent Claim 150 words
An improved drill bit for drilling Kevlar laminates or the like, said drill bit having a pair of helical leading edges each terminating in an outer cutting point; a center point; and concavely curved cutting edges extending between said center point and each said outer cutting point, said cutting edges curving back sharply from said cutting points as viewed along the longitudinal drill bit axis and in a direction opposite to normal rotation of said drill bit so as to draw material severed by said cutting points radially inwardly from the edge of a bore, said helical leading edges having a reduced rake angle along a leading edge segment adjacent to said cutting points relative to the rake angle of said leading edges along portions removed from said outer cutting points to thereby increase the shearing effect of said edges and minimize lifting of workpiece material by said leading edges.
Claim 3
Dependent Claim 43 words
The drill bit of claim 1 wherein each of said cutting edge in the immediate vicinity of said outer cutting point forms an angle of less than 65 degrees with a line tangent to the drill bit circumference at said outer cutting point.
Claim 4
Dependent Claim 25 words
The drill bit of claim 1, wherein said reduced rake angle is less than 25 degrees relative to the longitudinal axis of the drill bit.
Claim 5
Dependent Claim 27 words
The drill bit of claim 1, wherein said reduced rake angle is between 4 degrees and 15 degrees relative to the longitudinal axis of the drill bit.
Claim 6
Dependent Claim 36 words
The drill bit of claim 1, wherein said outer cutting points extend in the direction of rotation of said drill bit and lead said cutting edges in a plane transverse to the drill bit longitudinal axis.
Claim 7
Dependent Claim 21 words
The drill bit of claim 5, wherein said segments of reduced rake angle are leading edges of said outer cutting points.
Claim 8
Dependent Claim 15 words
The drill bit of claim 1, further comprising parabolic flutes defined between said helical edges.
Claim 9
Dependent Claim 22 words
The drill bit of claim 1, wherein said center point is slightly higher than said outer cutting points in an axial direction.
Claim 10
Dependent Claim 21 words
The drill bit of claim 1, wherein said cutting edges also recede from said outer cutting points in an axial direction.

References Cited (Backward Citations)

US228421A Cited
FR944587A Cited
US2600286A Cited
US2613710A Cited
US4209275A Cited
US4285620A Cited
US4330229A Cited
JPS57132908A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-07-15 1989-01-14 1989-07-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-07-15 1993-01-14 1993-07-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-07-15 1997-01-14 1997-07-16 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag