[go: up one dir, main page]

US20050112964A1 - Extruded strut, fuselage and front wing assembly for towable hydrofoil - Google Patents

Extruded strut, fuselage and front wing assembly for towable hydrofoil Download PDF

Info

Publication number
US20050112964A1
US20050112964A1 US10/897,363 US89736304A US2005112964A1 US 20050112964 A1 US20050112964 A1 US 20050112964A1 US 89736304 A US89736304 A US 89736304A US 2005112964 A1 US2005112964 A1 US 2005112964A1
Authority
US
United States
Prior art keywords
fuselage
strut
board
water sports
sports device
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.)
Abandoned
Application number
US10/897,363
Inventor
Michael Murphy
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US10/897,363 priority Critical patent/US20050112964A1/en
Publication of US20050112964A1 publication Critical patent/US20050112964A1/en
Priority to US11/186,356 priority patent/US7980191B2/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B32/00Water sports boards; Accessories therefor
    • B63B32/60Board appendages, e.g. fins, hydrofoils or centre boards
    • B63B32/62Board appendages, e.g. fins, hydrofoils or centre boards characterised by the material, e.g. laminated materials; characterised by their manufacturing process
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B34/00Vessels specially adapted for water sports or leisure; Body-supporting devices specially adapted for water sports or leisure
    • B63B34/60Arrangements for towing, e.g. for use with water-skis or wakeboards

Definitions

  • These towable water sports devices have a strut, fuselage and front and rear wings or blades which are made by casting a molten aluminum alloy.
  • This process requires pouring molten aluminum into a sand or steel mold.
  • the alloy used in this process is a 356A aluminum which is then heat-treated to T-6 hardness.
  • the casting is then ground or sanded down to eliminate all entry gates, all venting gates and the receiving canals. This requires a lot of grinding, sanding and machining of the cast part after it has been taken out of the mold. Cutting and grounding a part from a rolled or pressed aluminum billet wastes material and requires a lot of machine time.
  • Another disadvantage in manufacturing using the cast process is that the metal as it cures releases or gives off gases, resulting in the production of many small voids. This porosity in the part results in a poor finish.
  • the primary disadvantage of a part cast from 356A aluminum is that it does not have the ability to flex which can result in a catastrophic failure or breakage of the part. There is a large rejection rate when casting an aluminum part due to the temperature of the mold, the outside temperature, and the amount of the metal as it is poured into the mold.
  • the temperature of the mold has to be compatible with the heat of the material poured into the mold and this changes on a daily basis.
  • the porosity of the cast part is present on the surface of the part.
  • the surface porosity of the cast part adds drag to the foil assembly, which hinders the performance of the hydrofoil assembly.
  • the porosity of the cast part also is not compatible with and does not accept the anodizing process.
  • the anodizing is, however, desirable in that it offers a protective, maintenance free and corrosion-resistant finish.
  • a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said
  • the invention uses an extruded aluminum out of a AA6061 alloy heat-treated to T-6 in advance of the extrusion.
  • the 6061 heat-treated aluminum is one of the alloys to be used, but it is not the only one suitable for use in this manufacturing process.
  • suitable aluminum alloys include the M 6000 series which are disclosed in Park U.S. Pat. No. 4,589,932, and Wade et al U.S. Patent No. 5,503,690, the disclosures of which are expressly incorporated herein by reference. This eliminates the need to take the casting from the foundry to a separate location for the heat-treating process. Extrusion does not involve the pouring of metal. The metal is billet or rolled aluminum is pushed or pulled through a pre-cut die.
  • This grain allows the running of the grain in the long dimension of the part for added strength.
  • This process eliminates the porosity (that offers no strength) and gives the part more strength with completely different characteristics.
  • the extruded part can bend or flex with a memory that allows it to retain its original shape.
  • the extruded part is less brittle which avoids breakage while under stress in use and danger to the rider. Eliminating the porosity on the exterior surface of the part gives it: a)more visibly aesthetics; 2) polishes up nicely; 3) less drag due to little or no porosity; and 4) it is compatible with the anodizing protective coating.
  • the surface anodizing of aluminum extrusions described, for example, in Fukagawa et al U.S. Pat. No. 5,911,845.
  • extruded aluminum is applicable to the strut, fuselage, front and rear blade or wing comprising the foil assembly used in a towable hydrofoil.
  • FIG. 1 is a perspective view of the water sport device of this invention with the rider seated and being towed through the water by a power boat (not shown).
  • FIG. 2 shows at the left a top plan view of the fuselage and front and rear planing blades, and at the right, a side view of the strut, the parts being unassembled.
  • FIG. 3 shows the strut being inserted into the opening provided in the fuselage, the fuselage and planing blades being shown in longitudinal section.
  • FIG. 4 shows the strut fully in place in the fuselage and welded to the fuselage.
  • FIG. 5 depicts a die through which aluminum alloy is extruded to make the parts from which the strut, fuselage and planing blades are ultimately formed.
  • the water sports device of this invention has a seat 10 for the rider 11 which is affixed to the curved board 12 , the strut 14 projects downwardly from board 12 in a generally perpendicular fashion.
  • the lower end of strut 14 is received in opening 16 of fuselage 18 .
  • the fuselage 18 carries the front planing blade 20 and rear planing blade 22 .
  • a further feature of this invention concerns the combination of parts.
  • the castings for the foil assembly were three different parts: 1) a t-bar consisting of strut and fuselage as a single component; 2) front wing; and 3) rear wing.
  • the new means of manufacturing includes four parts: 1) the rear wing 22 ; 2) front wing 20 ; 3) the strut 14 ; and 4) the fuselage 18 .
  • the strut 14 and the fuselage 18 are heliarced (a means of welding aluminum) together to form the t-bar as shown in FIG. 4 .
  • the extruded strut 14 fits into the fuselage slot 24 as shown in the drawings and heliarced 26 as depicted in the drawing.
  • the extrusion process also provides the capability of including the front wing 20 and rear wing 22 within the extruded fuselage 18 as a single unit, thus reducing the number of parts to two.
  • the fuselage 18 and front wing 20 and rear wing 22 can be cut to the desired shape from a single aluminum extrusion using a programmable milling machine which is available in the marketplace. This reduces assembly time since the wings do not have to be joined to the fuselage in separate operations.
  • the extrusions are formed by drawing hot formable aluminum through a die such as die 28 .
  • the extrusion is then quenched and heat treated.
  • the strut can be extruded through a die of appropriate cross section, cut to length and used as such without further working. This process conforms generally to FIG. 1 of Wakabayashi U.S. Pat. No. 5,321,967.
  • the slot 24 is cut into the fuselage.
  • the fuselage, wings and strut in the desired configuration are polished smooth.
  • the resultant surface is quite slick and well adapted to anodizing which provides an esthetically pleasing appearance which is highly resistant to corrosion.
  • the avoidance of corrosion is an important benefit of this invention in that the strut, fuselage and blades or wings remain smooth and do not acquire or build up added drag in the water over time due to oxidation and mineral build-up.
  • the heliarc process is an oxygen gas mix and can be used for the welding of the extruded parts and it represents one option to be used for welding aluminum parts, but is not the only one available for this method of manufacturing.
  • Other techniques for welding or joining pre-formed aluminum parts are known to those skilled in the art.
  • the benefits of this invention include a less expensive part, stronger part, more consistent part and a part with less drag, increased performance, and fewer warranty problems. Extrusion has been used in other industries such as screen doors, window frames and others.
  • the present invention is a completely new concept in the manufacturing of hydrofoils for water sport devices and it provides results which are not manifested in prior extruded parts.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Forging (AREA)

Abstract

A towable water sports device having a hydrofoil assembly including a strut, fuselage and front and rear blades carried by the fuselage wherein said parts are extruded aluminum.

Description

  • This patent application claims the benefit of Provisional Patent Application Ser. No. 60/524,657, filed Nov. 25, 2003.
  • BACKGROUND OF INVENTION
  • Towable hydrofoil water sports devices for supporting a human rider are described in U.S. Pat. No. 5,100,354, granted March 31, 1992, U.S. Pat. No. 5,249,998, granted Oct. 5, 1993, U.S. Pat. No. 6,179,676, Jan. 30, 2001, and U.S. Pat. No. 6,551,158, granted Apr. 22, 2003
  • These towable water sports devices have a strut, fuselage and front and rear wings or blades which are made by casting a molten aluminum alloy. This process requires pouring molten aluminum into a sand or steel mold. The alloy used in this process is a 356A aluminum which is then heat-treated to T-6 hardness. The casting is then ground or sanded down to eliminate all entry gates, all venting gates and the receiving canals. This requires a lot of grinding, sanding and machining of the cast part after it has been taken out of the mold. Cutting and grounding a part from a rolled or pressed aluminum billet wastes material and requires a lot of machine time. Another disadvantage in manufacturing using the cast process is that the metal as it cures releases or gives off gases, resulting in the production of many small voids. This porosity in the part results in a poor finish. In addition as the casting comes out of the mold, there is shrinkage and the extent of the shrinkage is variable due to the nature of the alloy and weather conditions during the curing process. The primary disadvantage of a part cast from 356A aluminum is that it does not have the ability to flex which can result in a catastrophic failure or breakage of the part. There is a large rejection rate when casting an aluminum part due to the temperature of the mold, the outside temperature, and the amount of the metal as it is poured into the mold. The temperature of the mold has to be compatible with the heat of the material poured into the mold and this changes on a daily basis. There is a lack of overall consistency in the parts. The porosity of the cast part is present on the surface of the part. The surface porosity of the cast part adds drag to the foil assembly, which hinders the performance of the hydrofoil assembly. The porosity of the cast part also is not compatible with and does not accept the anodizing process. The anodizing is, however, desirable in that it offers a protective, maintenance free and corrosion-resistant finish.
  • SUMMARY OF INVENTION
  • In a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said support, generally parallel to said board, wherein said rearward planing wing or blade has a generally flat upper face and a generally flat lower face;
      • the improvement wherein at least said strut and fuselage are made of extruded aluminum alloy.
    DESCRIPTION OF PREFERRED EMBODIMENTS
  • The invention uses an extruded aluminum out of a AA6061 alloy heat-treated to T-6 in advance of the extrusion. The 6061 heat-treated aluminum is one of the alloys to be used, but it is not the only one suitable for use in this manufacturing process. For example, suitable aluminum alloys include the M 6000 series which are disclosed in Park U.S. Pat. No. 4,589,932, and Wade et al U.S. Patent No. 5,503,690, the disclosures of which are expressly incorporated herein by reference. This eliminates the need to take the casting from the foundry to a separate location for the heat-treating process. Extrusion does not involve the pouring of metal. The metal is billet or rolled aluminum is pushed or pulled through a pre-cut die. This gives the material a grain as opposed to a porosity as in a part made by the cast process. This grain allows the running of the grain in the long dimension of the part for added strength. This process eliminates the porosity (that offers no strength) and gives the part more strength with completely different characteristics. The extruded part can bend or flex with a memory that allows it to retain its original shape. The extruded part is less brittle which avoids breakage while under stress in use and danger to the rider. Eliminating the porosity on the exterior surface of the part gives it: a)more visibly aesthetics; 2) polishes up nicely; 3) less drag due to little or no porosity; and 4) it is compatible with the anodizing protective coating. The surface anodizing of aluminum extrusions described, for example, in Fukagawa et al U.S. Pat. No. 5,911,845.
  • The advantages of extruded aluminum are applicable to the strut, fuselage, front and rear blade or wing comprising the foil assembly used in a towable hydrofoil.
  • THE DRAWINGS
  • Turning to the drawings:
  • FIG. 1 is a perspective view of the water sport device of this invention with the rider seated and being towed through the water by a power boat (not shown).
  • FIG. 2 shows at the left a top plan view of the fuselage and front and rear planing blades, and at the right, a side view of the strut, the parts being unassembled.
  • FIG. 3 shows the strut being inserted into the opening provided in the fuselage, the fuselage and planing blades being shown in longitudinal section.
  • FIG. 4 shows the strut fully in place in the fuselage and welded to the fuselage.
  • FIG. 5 depicts a die through which aluminum alloy is extruded to make the parts from which the strut, fuselage and planing blades are ultimately formed.
  • Turning to the drawings in more detail, the water sports device of this invention has a seat 10 for the rider 11 which is affixed to the curved board 12, the strut 14 projects downwardly from board 12 in a generally perpendicular fashion. The lower end of strut 14 is received in opening 16 of fuselage 18. The fuselage 18 carries the front planing blade 20 and rear planing blade 22.
  • A further feature of this invention concerns the combination of parts. In the past the castings for the foil assembly were three different parts: 1) a t-bar consisting of strut and fuselage as a single component; 2) front wing; and 3) rear wing. The new means of manufacturing includes four parts: 1) the rear wing 22; 2) front wing 20; 3) the strut 14; and 4) the fuselage 18. The strut 14 and the fuselage 18 are heliarced (a means of welding aluminum) together to form the t-bar as shown in FIG. 4. The extruded strut 14 fits into the fuselage slot 24 as shown in the drawings and heliarced 26 as depicted in the drawing. This process is completely new from the previous method of manufacturing in the past. The extrusion process also provides the capability of including the front wing 20 and rear wing 22 within the extruded fuselage 18 as a single unit, thus reducing the number of parts to two. For example, the fuselage 18 and front wing 20 and rear wing 22 can be cut to the desired shape from a single aluminum extrusion using a programmable milling machine which is available in the marketplace. This reduces assembly time since the wings do not have to be joined to the fuselage in separate operations.
  • The extrusions are formed by drawing hot formable aluminum through a die such as die 28. The extrusion is then quenched and heat treated. The strut can be extruded through a die of appropriate cross section, cut to length and used as such without further working. This process conforms generally to FIG. 1 of Wakabayashi U.S. Pat. No. 5,321,967. The slot 24 is cut into the fuselage. The fuselage, wings and strut in the desired configuration are polished smooth. The resultant surface is quite slick and well adapted to anodizing which provides an esthetically pleasing appearance which is highly resistant to corrosion. The avoidance of corrosion is an important benefit of this invention in that the strut, fuselage and blades or wings remain smooth and do not acquire or build up added drag in the water over time due to oxidation and mineral build-up.
  • The heliarc process is an oxygen gas mix and can be used for the welding of the extruded parts and it represents one option to be used for welding aluminum parts, but is not the only one available for this method of manufacturing. Other techniques for welding or joining pre-formed aluminum parts are known to those skilled in the art.
  • The benefits of this invention include a less expensive part, stronger part, more consistent part and a part with less drag, increased performance, and fewer warranty problems. Extrusion has been used in other industries such as screen doors, window frames and others. The present invention is a completely new concept in the manufacturing of hydrofoils for water sport devices and it provides results which are not manifested in prior extruded parts.

Claims (7)

1. In a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said support, generally parallel to said board, wherein said rearward planing wing or blade has a generally flat upper face and a generally flat lower face;
the improvement wherein at least said strut and fuselage are made of extruded aluminum alloy.
2. The water sports device of claim 1 wherein the strut, fuselage and front and rear planing wings are made of extruded aluminum.
3. The water sports device of claim 2 wherein the strut, fuselage and front rear planing wings are provided with an anodized surface.
4. The water sports device of claim 1 wherein the strut has a lower end which is received in an opening in the fuselage.
5. The water sports device of claim 4 wherein the strut is heliarc welded to the fuselage.
6. The water sports device of claim 1 wherein the extruded aluminum is an M 6000 series.
7. The water sports device of claim 6 wherein the extruded aluminum is M 6061.
US10/897,363 2003-11-25 2004-07-21 Extruded strut, fuselage and front wing assembly for towable hydrofoil Abandoned US20050112964A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US10/897,363 US20050112964A1 (en) 2003-11-25 2004-07-21 Extruded strut, fuselage and front wing assembly for towable hydrofoil
US11/186,356 US7980191B2 (en) 2003-11-25 2005-07-20 Extruded strut, fuselage and front wing assembly for towable hydrofoil

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US52465703P 2003-11-25 2003-11-25
US10/897,363 US20050112964A1 (en) 2003-11-25 2004-07-21 Extruded strut, fuselage and front wing assembly for towable hydrofoil

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US11/186,356 Continuation-In-Part US7980191B2 (en) 2003-11-25 2005-07-20 Extruded strut, fuselage and front wing assembly for towable hydrofoil

Publications (1)

Publication Number Publication Date
US20050112964A1 true US20050112964A1 (en) 2005-05-26

Family

ID=34595160

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/897,363 Abandoned US20050112964A1 (en) 2003-11-25 2004-07-21 Extruded strut, fuselage and front wing assembly for towable hydrofoil

Country Status (1)

Country Link
US (1) US20050112964A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7980191B2 (en) 2003-11-25 2011-07-19 Murphy Michael J Extruded strut, fuselage and front wing assembly for towable hydrofoil

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US261022A (en) * 1882-07-11 Machine for making bolts and rivets
US4027614A (en) * 1975-04-07 1977-06-07 Jones Clyde B Sailboat construction
US4615291A (en) * 1982-08-16 1986-10-07 Jones Clyde B Hydrofoil boat
US5100354A (en) * 1989-02-23 1992-03-31 Woolley Robert C Water sports device
US5211594A (en) * 1992-07-02 1993-05-18 Barrows Michael L Water ski hydrofoil and process
US5249998A (en) * 1989-02-23 1993-10-05 Woolley Robert C Water sports device
US6179676B1 (en) * 1999-03-22 2001-01-30 Jon D. Wilborn Shock tower
US6386932B1 (en) * 2000-06-27 2002-05-14 Michael Murphy Inflatable boat
US6551158B2 (en) * 2001-02-20 2003-04-22 Michael Murphy Adjustable angled rear wing

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US261022A (en) * 1882-07-11 Machine for making bolts and rivets
US4027614A (en) * 1975-04-07 1977-06-07 Jones Clyde B Sailboat construction
US4615291A (en) * 1982-08-16 1986-10-07 Jones Clyde B Hydrofoil boat
US5100354A (en) * 1989-02-23 1992-03-31 Woolley Robert C Water sports device
US5249998A (en) * 1989-02-23 1993-10-05 Woolley Robert C Water sports device
US5211594A (en) * 1992-07-02 1993-05-18 Barrows Michael L Water ski hydrofoil and process
US6179676B1 (en) * 1999-03-22 2001-01-30 Jon D. Wilborn Shock tower
US6386932B1 (en) * 2000-06-27 2002-05-14 Michael Murphy Inflatable boat
US6551158B2 (en) * 2001-02-20 2003-04-22 Michael Murphy Adjustable angled rear wing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7980191B2 (en) 2003-11-25 2011-07-19 Murphy Michael J Extruded strut, fuselage and front wing assembly for towable hydrofoil

Similar Documents

Publication Publication Date Title
US7980191B2 (en) Extruded strut, fuselage and front wing assembly for towable hydrofoil
Emley Continuous casting of aluminium
US20020084007A1 (en) Aluminum alloys having improved cast surface quality
US6334978B1 (en) Cast alloys
US20050112964A1 (en) Extruded strut, fuselage and front wing assembly for towable hydrofoil
Sequeira et al. Effect of section thickness and microstructure on the mechanical properties of high pressure die cast magnesium alloy AZ 91 D
US4356618A (en) Production of rolled products
Epstein et al. Aluminum and its alloys
Decker et al. Progress in thixomolding
US20050245327A1 (en) Extruded golf club head and method of manufacture
Mordike et al. Laser Surface Melting of Aluminum Alloys
GB2033794A (en) Improvements in the production of rolled products
Helling Tanks and Pipes Cast of Aluminum Alloy With Reduced Wall Thickness and Casting Skin Left on Inner Surface
CN114381621A (en) Process for producing aluminum alloy section for ship
Ghomashchi Process control and optimization of near net-shaped aluminum-silicon alloys premium cast products.
Serban et al. Calculation method for general deformations of hull prefabricated units due to welding process.
Vimmer et al. High-speed billet casting with the use of Daimold technology
Roshan et al. Die Temperature Control in Pressure Diecasting
Aliravci et al. Elimination of Shrinkage Microporosity in AZ 91 Alloy Castings
Yamamoto et al. Entrainment of Molten Flux During Continuous Casting of Copper Alloys
Sasaki et al. Effect of solidified structure on mechanical properties of AZ 91 alloy
Webster et al. SHAPING UP FOR SAVING WEIGHT
Il'chenko et al. Investigating the Thermophysical Properties of Heat-Insulating Inserts Used in Pouring Steel
Hemon et al. Feeding Aluminum Die Castings: the Role of Calculation
Belopukhov et al. The Optimum Conditions of Mold Filling During the Die Casting of Magnesium Alloys

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION