US2484485A - Die cast terminal fittings and method of making the same - Google Patents
Die cast terminal fittings and method of making the same Download PDFInfo
- Publication number
- US2484485A US2484485A US571918A US57191845A US2484485A US 2484485 A US2484485 A US 2484485A US 571918 A US571918 A US 571918A US 57191845 A US57191845 A US 57191845A US 2484485 A US2484485 A US 2484485A
- Authority
- US
- United States
- Prior art keywords
- fitting
- making
- terminal fittings
- same
- wire
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/14—Casting in, on, or around objects which form part of the product the objects being filamentary or particulate in form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
- F16C1/10—Means for transmitting linear movement in a flexible sheathing, e.g. "Bowden-mechanisms"
- F16C1/12—Arrangements for transmitting movement to or from the flexible member
- F16C1/14—Construction of the end-piece of the flexible member; Attachment thereof to the flexible member
- F16C1/145—Attachment of the end-piece to the flexible member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2220/00—Shaping
- F16C2220/02—Shaping by casting
- F16C2220/04—Shaping by casting by injection-moulding
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/4989—Assembling or joining with spreading of cable strands
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49988—Metal casting
Definitions
- This invention relates to die cast terminal fittings and the method of making the same, and more particularly to such fittings for stranded wire structures.
- terminal fittings to small fiexible wire strands are by cold swaging.
- the design of these terminal fittings to fit screw machine production is desirable, but forging and drilling is the most common practice used to produce such fittings.
- Small flexible wire strands and necessary terminal fittings are used extensively on aircraft. In this use the wire strength must not be impaired and the strength oi the terminal fitting must be comparable to that of low carbon steels.
- Another object is to produce such fittings by die casting.
- Fig. 7 shows the completed terminal fitting of the second embodiment.
- the numeral 2 indicates a stranded wire structure to which a terminal fitting is to be attached.
- a length of the wire is prepared to receive the cast metal by brooming it to form a bulb portion 4 and an end portion 6, as shown in Fig. 2.
- Aluminum bronze is one common type of die casting metals having the Wear and strength characteristics required for a terminal fitting. However, the fiuid casting heat of these metals is between 1900 F. and 2300 F., and casting a terminal to the broomed end of a stranded wire structure by the insert method will bring about a heating of the wire so as to cause a marked drop in its wear and strength values.
- an intermediate fitting 8 made of a low melting point metal is cast around the broomed portion of the wire in any suitable manner, such as die casting, or by sprayng the molten metal on the metal, it only being necessary that the metal be applied to the wire in molten condition in order that it be fused thereto.
- the fitting 8 may be made of a zinc alloy which bonds to steel and which is suited for die casting at a temperature of about 715 F.
- the terminal fitting l0 made of aluminum bronze or a similar high strength material, is die cast directly onto the structure shown in Fig. 3.
- the design of the fittings, fusingand shrinkage of the metals as they cool are components which produce the tensile requirements.
- the zinc fitting hastens chilling and insulates the wires from any destruction from the high casting heat of the terminal fitting I0.
- Figs. 6 and 7 show a second embodiment of the t I invention.
- a ball type fitting I2 is cast directly onto the ball portion 4 of the wire structure, leaving the broomed end 6 extending therefrom.
- the fitting i2 has the same purpose and is made of the same material as the fitting 8.
- the terminal fitting I4 is cast directly onto the fitting i2 and the broomed end 6.
- the fitting l2 insulates the wire in the vicinity of the fatigue point and the high strength die metal is bonded with the extreme broomed end of the wire structure to develop the required assembled strength.
- a connector for stranded wire structure 3 comprising a cast metal layer surrounding and in intimate contact with said wire structure, said metal layer'having a relatively low melting point, and a second cast metal layer surrounding and merging with said first metal layer, said second layer having a relatively high melting point.
- a connector for stranded wire structure comprising a cast metal layer surrounding and in intimate contact with said wire structure a short distance from one end thereof, said metal layer having a relatively low melting point, and a second cast metal layer surrounding and merging with said first metal layer and also surrounding and in intimate contact with the exposed end oi said wire structure, said second layer havl6 ing a relatively high melting point.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Wire Processing (AREA)
Description
0a. 11,- 1949. E. BRICKMAN 2,484,485
7 Y DIE C TERMINAL F. TINGS AND MET OF MAKING .SAIE
ed Jan. 8, 1945 Patented Oct. 11, 1949 UNITED STATES PATENT OFFICE DIE CAST TERMINAL FITTINGS AND METHOD OF MAKING THE SAME 4 Claims.
This invention relates to die cast terminal fittings and the method of making the same, and more particularly to such fittings for stranded wire structures.
The present method of attaching terminal fittings to small fiexible wire strands is by cold swaging. The design of these terminal fittings to fit screw machine production is desirable, but forging and drilling is the most common practice used to produce such fittings. Small flexible wire strands and necessary terminal fittings are used extensively on aircraft. In this use the wire strength must not be impaired and the strength oi the terminal fitting must be comparable to that of low carbon steels.
It is an object of this invention to produce and attach terminal fittings faster and cheaper than at present.
Another object is to produce such fittings by die casting.
These and other objects will be more apparent after referring to the attached drawings, in
invention showing an intermediate fitting cast in place;
Fig. 7 shows the completed terminal fitting of the second embodiment.
Referring more particularly to the drawings, the numeral 2 indicates a stranded wire structure to which a terminal fitting is to be attached. A length of the wire is prepared to receive the cast metal by brooming it to form a bulb portion 4 and an end portion 6, as shown in Fig. 2. Aluminum bronze is one common type of die casting metals having the Wear and strength characteristics required for a terminal fitting. However, the fiuid casting heat of these metals is between 1900 F. and 2300 F., and casting a terminal to the broomed end of a stranded wire structure by the insert method will bring about a heating of the wire so as to cause a marked drop in its wear and strength values. To protect the wire from such damage an intermediate fitting 8 made of a low melting point metal is cast around the broomed portion of the wire in any suitable manner, such as die casting, or by sprayng the molten metal on the metal, it only being necessary that the metal be applied to the wire in molten condition in order that it be fused thereto. The fitting 8 may be made of a zinc alloy which bonds to steel and which is suited for die casting at a temperature of about 715 F. Such fittings, applied to broomed stranded wire structures by die casting and employing water-cooled dies, will not aifect the physical properties of the stranded wires commonly used in the aircraft industry. The terminal fitting l0, made of aluminum bronze or a similar high strength material, is die cast directly onto the structure shown in Fig. 3. The design of the fittings, fusingand shrinkage of the metals as they cool are components which produce the tensile requirements. The zinc fitting hastens chilling and insulates the wires from any destruction from the high casting heat of the terminal fitting I0.
Figs. 6 and 7 show a second embodiment of the t I invention. A ball type fitting I2 is cast directly onto the ball portion 4 of the wire structure, leaving the broomed end 6 extending therefrom.
The fitting i2 has the same purpose and is made of the same material as the fitting 8. The terminal fitting I4 is cast directly onto the fitting i2 and the broomed end 6. The fitting l2 insulates the wire in the vicinity of the fatigue point and the high strength die metal is bonded with the extreme broomed end of the wire structure to develop the required assembled strength.
While two embodiments of the invention have been shown and described, it will be apparent that other modifications and adaptations may be made without departing from the scope of the attached claims.
I claim:
1. The method of making a terminal fitting for stranded wire structure, which comprises brooming a length of the stranded wire adjacent one end thereof, casting a zinc alloy fitting to that part of the broomed length adjacent the wound stranded wire, and then casting a high strength terminal fitting directly around said first named fitting and the remainder of the broomed length.
2. The method of making a terminal fitting for stranded wire structure which comprises brooming a length of the stranded wire adjacent one end thereof, casting a low melting point metal fitting to that part of the broomed length adjacent the wound stranded wire, and then casting a high strength terminal fitting directly around said first named fitting and the remainder of the broomed length.
3. A connector for stranded wire structure 3 comprising a cast metal layer surrounding and in intimate contact with said wire structure, said metal layer'having a relatively low melting point, and a second cast metal layer surrounding and merging with said first metal layer, said second layer having a relatively high melting point.
4. A connector for stranded wire structure comprising a cast metal layer surrounding and in intimate contact with said wire structure a short distance from one end thereof, said metal layer having a relatively low melting point, and a second cast metal layer surrounding and merging with said first metal layer and also surrounding and in intimate contact with the exposed end oi said wire structure, said second layer havl6 ing a relatively high melting point.
" ALAN E. BRICKMAN.
REFERENCES crran The following references are of record in the file of this patent:
UNITED STATE PATENTS Number Name Date 906,827 Holley et al Dec. 15, 1908 974,7 9 Stevenson Nov. 1, 1910 10 1,043,831 Heinkel et a1 Nov. 12, 1912 1,214,709 Orr Feb. 6, 1917 1,719,963 Brady July 9, 1929 1,748,879 Vamey Feb. 11, 1930 1,931,176 Baird Oct. 17, 1933 2,0 6,856 Fiege Oct. 8, 1935 2,238,926 Caldwell Apr. 22, 1941
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US571918A US2484485A (en) | 1945-01-08 | 1945-01-08 | Die cast terminal fittings and method of making the same |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US571918A US2484485A (en) | 1945-01-08 | 1945-01-08 | Die cast terminal fittings and method of making the same |
Publications (1)
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US2484485A true US2484485A (en) | 1949-10-11 |
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US571918A Expired - Lifetime US2484485A (en) | 1945-01-08 | 1945-01-08 | Die cast terminal fittings and method of making the same |
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Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2649652A (en) * | 1948-05-24 | 1953-08-25 | Mattel Creations Inc | Method of making melody combs |
US2687278A (en) * | 1948-05-26 | 1954-08-24 | Chrysler Corp | Article with passages |
US2719742A (en) * | 1951-11-19 | 1955-10-04 | Univ California | Ball and socket joint |
US2905977A (en) * | 1956-10-24 | 1959-09-29 | Bouligny Inc R H | Cradle pin for textile fiber drafting apparatus |
US3032846A (en) * | 1955-04-04 | 1962-05-08 | Jones & Laughlin Steel Corp | Wire rope fitting |
US3086741A (en) * | 1958-12-08 | 1963-04-23 | Cramer Posture Chair Company I | Cast base for chair legs and method of making same |
US3402461A (en) * | 1963-03-25 | 1968-09-24 | Western Electric Co | Capacitor termination |
US3665587A (en) * | 1968-12-05 | 1972-05-30 | Global Marine Inc | Process for fabricating a dead end of the spelter socket type for wire cables |
US4043690A (en) * | 1975-08-28 | 1977-08-23 | York Engineering, Inc. | Wire rope termination |
FR2418688A1 (en) * | 1978-03-03 | 1979-09-28 | Z Nezhinselmash | Machine reinforcing rope with cast pieces - has axially movable clamp spreading rope strands within mould for self-reinforcement |
FR2424775A1 (en) * | 1978-05-05 | 1979-11-30 | Philips Nv | PROCESS FOR SHAPING HEADS FOR HANGING TO TRACTION SPRINGS, AND TRACTION SPRING OBTAINED FROM THE KIND. |
US5027497A (en) * | 1989-04-06 | 1991-07-02 | Tokyo Rope Mfg. Co., Ltd. | Method for forming fixing end portion of composite rope and composite rope |
US5211500A (en) * | 1989-04-06 | 1993-05-18 | Tokyo Rope Mfg. Co., Ltd. | Composite rope having molded-on fixing member at end portion thereof |
US5337621A (en) * | 1993-11-18 | 1994-08-16 | Teleflex Incorporated | Cable end fitting retainer and method for making same |
US5730262A (en) * | 1995-02-03 | 1998-03-24 | Fichtel & Sachs Ag | Shock absorber or vibration damper and a hinge eye for a vibration damper or shock absorber |
US20070289217A1 (en) * | 2006-05-18 | 2007-12-20 | Arrow Tru-Line, Inc | Overhead door cable assembly with molded cable stop |
US20080211202A1 (en) * | 2005-05-23 | 2008-09-04 | John Belding | Stabilizer Link Assembly |
WO2011101105A1 (en) * | 2010-02-17 | 2011-08-25 | Gemo D. G. Moritz Gmbh & Co. Kg | Rising cable with stabilized driver |
WO2011101104A1 (en) * | 2010-02-17 | 2011-08-25 | Gemo D. G. Moritz Gmbh & Co. Kg | Pitched cable with play-tolerant driver |
DE102010011792A1 (en) * | 2010-03-17 | 2011-09-22 | Universität Stuttgart | cable end |
WO2012084082A1 (en) * | 2010-12-23 | 2012-06-28 | Gemo D. G. Moritz Gmbh & Co. Kg | Pitched cable having a flexible core around which a coil is wrapped |
US20180223896A1 (en) * | 2017-02-07 | 2018-08-09 | Yuan-Hung WEN | End cap device for bicycle cables |
DE102019203969A1 (en) * | 2019-03-22 | 2020-09-24 | Brose Fahrzeugteile Se & Co. Kommanditgesellschaft, Bamberg | Pull rope for a power transmission device in a vehicle |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US906627A (en) * | 1908-02-29 | 1908-12-15 | Bristol Brass Company | Process of uniting metals. |
US974719A (en) * | 1910-03-30 | 1910-11-01 | Charles Stevenson | Wire cable, socket, and coupling. |
US1043831A (en) * | 1909-11-12 | 1912-11-12 | Christian F Heinkel | Method of uniting materials. |
US1214709A (en) * | 1916-02-17 | 1917-02-06 | Arthur Orr | Means for and method of fastening cable ends. |
US1719963A (en) * | 1926-03-29 | 1929-07-09 | Albert C Henry | Composite electrical brush or contact and method of producing same |
US1746879A (en) * | 1925-05-21 | 1930-02-11 | Aluminum Co Of America | Dead-end fixture for cables |
US1931176A (en) * | 1930-08-30 | 1933-10-17 | John W Bair | Cable socket applying tool and method |
US2016856A (en) * | 1934-05-07 | 1935-10-08 | Henry C Fiege | Cable clamp |
US2238926A (en) * | 1936-10-22 | 1941-04-22 | Electric Railway Improvement Co | Welding |
-
1945
- 1945-01-08 US US571918A patent/US2484485A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US906627A (en) * | 1908-02-29 | 1908-12-15 | Bristol Brass Company | Process of uniting metals. |
US1043831A (en) * | 1909-11-12 | 1912-11-12 | Christian F Heinkel | Method of uniting materials. |
US974719A (en) * | 1910-03-30 | 1910-11-01 | Charles Stevenson | Wire cable, socket, and coupling. |
US1214709A (en) * | 1916-02-17 | 1917-02-06 | Arthur Orr | Means for and method of fastening cable ends. |
US1746879A (en) * | 1925-05-21 | 1930-02-11 | Aluminum Co Of America | Dead-end fixture for cables |
US1719963A (en) * | 1926-03-29 | 1929-07-09 | Albert C Henry | Composite electrical brush or contact and method of producing same |
US1931176A (en) * | 1930-08-30 | 1933-10-17 | John W Bair | Cable socket applying tool and method |
US2016856A (en) * | 1934-05-07 | 1935-10-08 | Henry C Fiege | Cable clamp |
US2238926A (en) * | 1936-10-22 | 1941-04-22 | Electric Railway Improvement Co | Welding |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2649652A (en) * | 1948-05-24 | 1953-08-25 | Mattel Creations Inc | Method of making melody combs |
US2687278A (en) * | 1948-05-26 | 1954-08-24 | Chrysler Corp | Article with passages |
US2719742A (en) * | 1951-11-19 | 1955-10-04 | Univ California | Ball and socket joint |
US3032846A (en) * | 1955-04-04 | 1962-05-08 | Jones & Laughlin Steel Corp | Wire rope fitting |
US2905977A (en) * | 1956-10-24 | 1959-09-29 | Bouligny Inc R H | Cradle pin for textile fiber drafting apparatus |
US3086741A (en) * | 1958-12-08 | 1963-04-23 | Cramer Posture Chair Company I | Cast base for chair legs and method of making same |
US3402461A (en) * | 1963-03-25 | 1968-09-24 | Western Electric Co | Capacitor termination |
US3665587A (en) * | 1968-12-05 | 1972-05-30 | Global Marine Inc | Process for fabricating a dead end of the spelter socket type for wire cables |
US4043690A (en) * | 1975-08-28 | 1977-08-23 | York Engineering, Inc. | Wire rope termination |
FR2418688A1 (en) * | 1978-03-03 | 1979-09-28 | Z Nezhinselmash | Machine reinforcing rope with cast pieces - has axially movable clamp spreading rope strands within mould for self-reinforcement |
FR2424775A1 (en) * | 1978-05-05 | 1979-11-30 | Philips Nv | PROCESS FOR SHAPING HEADS FOR HANGING TO TRACTION SPRINGS, AND TRACTION SPRING OBTAINED FROM THE KIND. |
US4270261A (en) * | 1978-05-05 | 1981-06-02 | U.S. Philips Corporation | Method of forming fixing heads on tension springs and tension springs manufactured by this method |
US5027497A (en) * | 1989-04-06 | 1991-07-02 | Tokyo Rope Mfg. Co., Ltd. | Method for forming fixing end portion of composite rope and composite rope |
US5211500A (en) * | 1989-04-06 | 1993-05-18 | Tokyo Rope Mfg. Co., Ltd. | Composite rope having molded-on fixing member at end portion thereof |
US5337621A (en) * | 1993-11-18 | 1994-08-16 | Teleflex Incorporated | Cable end fitting retainer and method for making same |
US5730262A (en) * | 1995-02-03 | 1998-03-24 | Fichtel & Sachs Ag | Shock absorber or vibration damper and a hinge eye for a vibration damper or shock absorber |
US20080211202A1 (en) * | 2005-05-23 | 2008-09-04 | John Belding | Stabilizer Link Assembly |
US20070289217A1 (en) * | 2006-05-18 | 2007-12-20 | Arrow Tru-Line, Inc | Overhead door cable assembly with molded cable stop |
WO2011101105A1 (en) * | 2010-02-17 | 2011-08-25 | Gemo D. G. Moritz Gmbh & Co. Kg | Rising cable with stabilized driver |
WO2011101104A1 (en) * | 2010-02-17 | 2011-08-25 | Gemo D. G. Moritz Gmbh & Co. Kg | Pitched cable with play-tolerant driver |
DE102010011792A1 (en) * | 2010-03-17 | 2011-09-22 | Universität Stuttgart | cable end |
WO2012084082A1 (en) * | 2010-12-23 | 2012-06-28 | Gemo D. G. Moritz Gmbh & Co. Kg | Pitched cable having a flexible core around which a coil is wrapped |
US9140330B2 (en) | 2010-12-23 | 2015-09-22 | Gemo D. G. Moritz Gmbh & Co. | Pitched cable having a flexible core around which a coil is wrapped |
US20180223896A1 (en) * | 2017-02-07 | 2018-08-09 | Yuan-Hung WEN | End cap device for bicycle cables |
DE102019203969A1 (en) * | 2019-03-22 | 2020-09-24 | Brose Fahrzeugteile Se & Co. Kommanditgesellschaft, Bamberg | Pull rope for a power transmission device in a vehicle |
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