Self-Advancing Step-Tap Drill Bit
For reduced fatigue, improved safety, and greater efficiency
NASA’s Johnson Space Center invites interested companies to license its patented self-advancing, step-tap drill bit. Originally developed for Space Shuttle repair (it now flies on every Shuttle mission), this novel, stepped drill bit features a cutting edge that concurrently enlarges a hole as it cuts threadsa feature not available in other stepped drill bits. The drill bit advances itself into the work material similar to a screw, eliminating the need to apply external axial force. This unique technology greatly improves the safety and efficiency of handheld drilling while reducing operator fatigue, making it ideal for high-volume and heavy-duty construction applications and home shop use.
Additional technical details are presented below. For more information about this licensing and joint development opportunity, please contact us by phone or email: (919) 249-0327,
- Reduced fatigue: Features a unique self-advancing component that eliminates the need for continuous axial force, decreasing physical work effort
- Improved safety: Reduces the risk of the work piece tearing or spinning in the operator’s hand because the drill bit does not grab the work piece
- Greater efficiency: Allows operators to work more quickly and productively without the need to change drill bits and taps when drilling different sized holes
- Drilling holes larger than 0.5 inch
- Drilling vertically oriented holes
- Repetitive drilling
- Overhead drilling
The self-advancing, step-tap drill bit uses a cutting edge to simultaneously enlarge a hole and cut threads. The drill bit is stepped, enabling an increase in the diameter of the hole with each step. To prevent the threads from stripping caused by the required cutting forces between the drill bit and the work material, the thread pitch (number of threads per inch) and diameter increase for each step are adjusted for the material type and thickness. The diameters of the steps are in increments of 0.0300.060 inch (0.81.5 mm). The tip typically has a diameter of 1/83/16 inch (3.24.8 mm).
The thickness of the work piece to be drilled and tapped determines the length of the pilot-drill section chosen, so that the pilot hole is completed before engagement of the first tap section. If the cutting-edge geometry of the drill bit is optimized for the material to be drilled, only a relatively small axial force (typically a few pounds) must be applied when drilling the pilot hole. Once the first tap section engages the pilot hole, no additional axial force is necessary because the thread engagement between the tap and the work piece provides the axial force, seamlessly advancing the drill bit. A stop-lip or shoulder at the shank end of the widest tap section prevents further passage of the drill bit through the hole.
Applied axial drilling forces for handheld drills can be quite large, often as much as 75 lb (about 330 N) when drilling holes up to approximately 1 inch (25 mm) in diameter. With non-self-advancing drills, an operator often must bear down with near full body weight to facilitate downward drilling. When using such non-self-advancing drills, vertical, overhead, and repetitive drilling is extremely fatiguing and limits worker productivity. In addition, applying a large axial force with a hand-held drill can be dangerous because the drill bit can grab the work piece, causing the work piece to spin or tear the drill and work piece from the operator’s hand.
Other drilling technologies include drill bits that make a single-sized hole, step drills that enable hole enlargement, taps that thread one size of a pre-existing hole, and a simple combination of a single-sized drill and a tap (for tapping after a hole has been drilled). Combining any of these technologies will not result in a functional, self-advancing, step-tap drill. Rather, the innovation developed at Johnson Space Center is a precise combination of step size, cutting angle, thread advance, and flute design, producing a drill bit that all but eliminates the need to apply external axial force while concurrently cutting and threading a hole. This significantly reduces operator fatigue, increases safety and efficiency, and enables drilling larger holes in thinner materials with a standard, commercially available drill.
Partners licensing and commercializing this innovative technology can manufacture and market the drill bits in several optimized designs and sizes for purchase individually or as a set. Marketable variations include:
- A set designed to leave a tapped hole for threading standard-sized fasteners
- A set to leave a hole through which to pass the shank of standard-sized fasteners
- A set for large holes
- Sets optimized for metal, plastic, and brittle ceramics
Johnson Space Center has received patent protection for this technology: U.S. Patent No. 7,357,606 (link opens new browser window)
- What makes this drill bit different from others available today?
- What makes the drill bit self-advancing?
- What are the best applications for this drill bit?
- What materials are best suited to drilling with this type of bit?
- Can the drill bit be used on harder materials such as titanium and stainless steel?
- How many revolutions per minute (RPMs) can the drill bit support?
- What materials and/or coatings are appropriate for the drill bit?
- What are the design specifications for the drill bits?
- What diameters are available?
- Can very small versions of the drill be made, for example, with a maximum step size of 0.3 inch or smaller?
- What is the overall length of the drill bit? They look quite large in some of your photos.
- Can the drill bits be made without the threading capability?
- How do you manage the drilling process to avoid running up against the stop lip with excessive force and possibly damaging the work material?
- Do you have to reverse the drill bit out of the hole?
- How deep can you drill before the bit gets clogged with burrs?
- Can we test the drill bit before licensing?
The unique aspect of this drill bit is its self-advancing feature. Once the pilot drill section has started advancing (which requires only about 3-4 pounds axial force) the drill bit requires no additional axial loading, even when drilling holes larger than 1 inch, due to its self-advancing feature. While common drill bits require high axial loads and feature low torques, this drill bit requires minimal axial load and features higher torques.
This self-advancing feature forms the foundation for the patent granted to NASA: U.S. patent no. 7,357,606 (link opens new browser window) .
The drill bit simultaneously cuts threads as it enlarges the hole, enabling the drill bit to advance on its own (or “self-advance”), similar to a screw. This eliminates the need to apply large axial force to the hand-held drill.
Drilling the pilot section is the only time an axial force is required, which is typically less than 4 pounds, generally for less than 20 seconds.
- Drilling high-cost items, particularly advanced composite materials
- Repetitive hand-held drilling and tapping
- Drilling holes larger than 1⁄2 inch
- Drilling vertically oriented holes
- Overhead drilling
This drill bit is best suited to drilling in thin and medium-thin (less than 3/8-inch) materials. It is especially useful when drilling high-cost, advanced composite materials, because the unique self-advancing aspect of the drill bit leaves a clean-cut hole with minimal breakout damage. The self-advancing feature eliminates de-lamination of composite layers, particularly back-side breakout, because the threading action places the drilled material in compression. Materials well-suited to this drill bit include:
- Thin-skinned foam cored composites
- Epoxy graphite
- Other honeycombed composites with thin bonded skins
- Coated materials
- Aluminum sheeting
- Galvanized sheet metal
The drill bit has not been tested on these types of materials, and therefore cannot be recommended for hardened materials at this time.
The drill bit is designed for lower speeds. Due to the self-advancement being dictated by the thread pitch, fast RPMs with coarse thread pitches advance the cutting edge at too great of rate. For the NASA-developed drill bits with 18 threads per inch (TPI), about 200 RPM is about the maximum useful rate when drilling advanced composites. For use during a space walk for repair of the space shuttle leading edge, the maximum speed of the space-rated drill driver is 60 RPM, thus that is the maximum planned NASA speed.
With an 18 TPI bit, testers were able to successfully control speed by partially depressing the power trigger on a commercially available drill set at low range.
The drill bit can be made of typical materials such as oil hardened tool steel, cobalt steel, high speed steel, or carbide. Coatings such as diamond, titanium nitride, titanium aluminum nitride, titanium carbon nitride, and others can be added to extend the life of the bit and provide heat resistance and lubrication.
The point consists of a small pilot drill 1/8- to 3/16-inch diameter with two flutes and a cutting point 115° to 135°. The cutting edge relief-web is ground to be about 0.050-inch wide to increase the cutting tip pressure for a given applied axial load. The rake on the cutting edge is best from 0° to +20° for non-metals. The pilot drill bit section is made about 0.3-inch long so that the pilot hole is completed before the engagement of the step-tap section. Drilling the pilot section of the self-advancing step-tap drill bit is the only time an axial force is required on the hand-held drill and is less than 4 lbs force with the correct drill-bit-cutting-edge geometry. The time to drill the pilot section through the reinforced carbon-carbon (RCC) is less than 20 seconds. All the forces applied by a crewmember in an extravehicular mobility unit (EMU) for the pilot hole are within the allowed limits.
The detailed description that follows applies to the first step-tap section past the pilot drill bit as well as to all subsequent step-tap enlargements. The first step-tap section engages the pilot hole and increases the diameter by 0.030- to 0.060-inch, as does each subsequent step-tap. It was determined that as the step diameters become greater than 1/2 inch, the step diameter increase is best reduced to 0.030-inch. For step diameters less than 1/2 inch, 0.050 to 0.060 inch diameter increase is acceptable. The length of each step is chosen so that one complete step is cut before the next sized step begins engagement. For space shuttle RCC, step lengths of 0.3 inch were used. The transition between step-tap sections includes a cutting edge with a transition angle between adjacent step-tap diameters of 25° to 50°. A cutting edge rake from 0° to +20° works best for space shuttle RCC. The thread-tap can start at the step diameter or it can spiral through the transition angle between adjacent steps. It is more difficult to machine a drill bit with a spiral increase in thread-tap diameter versus machining a constant thread tap diameter on each step. We found that for holes less than 3/8-inch, having the threaded-tap only on the constant diameter steps was satisfactory. Engagement and hole enlargement between steps self advanced with no issues. For holes wider than 3/8 inch, the transition angle should be threaded with a spirally increasing thread-tap to aid the self-advancement and prevent the threads from becoming stripped due to the large forces between the cutting surfaces and the material being drilled. Step diameter increases for holes larger than 1/2 inch may need to be kept smaller than that which works well for holes less than this.
Thread pitch of 13 to 18 threads per inch (TPI) works well. For non-metals, a coarser thread pitch is required to make for sufficient thread depth to hold and thus prevent stripping. For metals, a finer thread pitch may be desirable. The step-tap drill bit can be made with one constant thread pitch over all steps or a variable thread pitch where each step has a different TPI. The transition angle can have its own TPI, which might be different than that of each step section. A finer TPI on the transition angle is helpful to ensure self-advancement between steps particularly for diameters above 1/2 inch.
A stop-lip is placed after the largest step-tap section to prevent the drill bit from passing through the hole. A three faceted drive shank of 3/8-inch diameter allows for use in standard drill chucks.
The operation of this drill bit is not highly dependent on the number of flutes. Drill bits with one to four flutes work well. We tended to use two-flute drill bits simply for ease of machining. Drill bit speeds of rotation work best at less than 60 revolutions per minute (RPM) for holes up to 1/2 inch. For holes wider than 1/2 inch, 30 RPM works best.
Several construction materials for the drill bit were tried. Air-hardened steel was used for fast production of engineering prototypes where only a few dozen test holes were drilled. Oil-hardened tool steel or cobalt tool steel is a good material for final construction. The end use for on-orbit space shuttle RCC repair does not require extended tool life and normal tool steels keep their cutting edge for dozens of holes in RCC. More exotic materials such as tungsten-carbide and diamond coatings were tested and determined that their advantages were not needed.
The diameter range for the step-tap drill bit is a user-specified criterion. For a step enlargement of 0.030- to 0.060-inch per step with a step length of 0.3-inch, the diameter range then determines the drill bit’s overall length. The inventors chose to divide their required diameter range between two drill bits, one from pilot hole to 0.5-inch, the second from 0.5 to 1.0625-inch. The 1.0625-inch step-tap created a clear hole 1 inch in diameter. Each of these drill bits were less than 6 inches long, including the drive shank.
There are two basic designs for the choice of step-tap hole diameters and choice of TPI. One is to leave a threaded hole in which to screw a threaded fastener with TPI that matches standard screws and bolts. This requires a different TPI pitch on the steps that match standard-sized fasteners (e.g., 1/420, 5/1618, 3/816, 1/213, etc.). The other is to create a clearance hole, even though threaded, sufficient to pass the shank of standard fasteners. This type of drill bit can have a constant TPI pitch chosen to optimize the self-advancement of this drill bit.
Yes, the drill bit can be made for any user-selected diameter.
The length of the drill bit is determined by the thread pitch, step enlargement, and desired maximum step size. If very large diameters are needed and the drill bit operates in tight, enclosed areas, the diameter range can be split across two drill bits, allowing each bit to be shorter in length. The space-flight rated drill bits are 6 inches long. One drill features bits from a diameter of 0.25 to 0.5 inch, the second from 0.5 to 1.0625 inch.
No, the self-advancing aspect of the drill bit is achieved by concurrently cutting threads as the hole is enlarged. Eliminating the threading would eliminate the self-advancing feature.
For applications requiring only a through hole, the through hole will have the threaded profile. This can be an advantage when drilling composite materials for repair. When a damaged area is drilled out and a patch is installed over the drilled out area, the threaded profile can act as a high-surface-area zone to which the composited repair compound can bond.
Because of the slower speed of operation, a stop lip is not typically necessary. NASA initially included stop lips on prototypes but found them unnecessary and removed them for the final production version.
Yes, because the drill bit leaves a threaded hole, you must reverse it out through the last step to avoid damaging the threads.
Clogging is not an issue, as step-type drill bits are typically used with thinner materials. Each new step starts with a fresh drill bit section. The chips tend to be pushed forward and accumulate in the flutes of the previous steps, rather than clogging the bit. As noted above, coatings can be applied to provide heat resistance, if needed.
Qualified, interested parties can execute a no-cost Prototype License which allows for limited manufacturing for prototype and testing purposes. Please contact
for more information.
- "Tools in Space (link opens new browser window) ," by Alan Richter, published in Cutting Tool Engineering Magazine, April 2007
- "Self-Advancing Step-Tap Drills: It is not necessary to apply axial drilling forces,(link opens new browser windo" published in NASA Tech Briefs, Thursday, February 01 2007
- Technical Support Package (TSP) for Self-Advancing Step-Tap Drills (link opens new browser window)
- Demonstration of the Self-Advancing Step-Tap Drill Bit drilling hole of 1/2" diameter
- Demonstration of the Self-Advancing Step-Tap Drill Bit drilling 1" hole in reinforced carbon-carbon composite material
This technology is part of NASA’s Innovative Partnerships Program, which seeks to transfer technology into and out of NASA to benefit the space program and U.S. industry. NASA invites companies to inquire about the licensing possibilities for the Self-Advancing Step-Tap Drill Bit (MSC-23954-1) for commercial applications.
If you would like more information about this technology, please contact us by phone or e-mail: (919) 249-0327,
For information about other technology licensing opportunities, please visit:
Advanced Planning Office
NASA's Johnson Space Space Center