US2614781A - Aircraft seat leg release means - Google Patents

Aircraft seat leg release means Download PDF

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Publication number
US2614781A
US2614781A US9950549A US2614781A US 2614781 A US2614781 A US 2614781A US 9950549 A US9950549 A US 9950549A US 2614781 A US2614781 A US 2614781A
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United States
Prior art keywords
leg
catch
standard
sleeve
floor
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Expired - Lifetime
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William A Engel
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Individual
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Classifications

    • AHUMAN NECESSITIES
    • A47FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47BTABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
    • A47B91/00Feet for furniture in general
    • A47B91/08Feet for furniture in general connected to the floor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0639Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0696Means for fastening seats to floors, e.g. to floor rails
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60NSEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/24Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles for particular purposes or particular vehicles
    • B60N2/30Non-dismountable or dismountable seats storable in a non-use position, e.g. foldable spare seats
    • B60N2/3038Cushion movements
    • B60N2/304Cushion movements by rotation only
    • B60N2/3045Cushion movements by rotation only about transversal axis
    • B60N2/3047Cushion movements by rotation only about transversal axis the cushion being hinged at the back-rest
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T279/00Chucks or sockets
    • Y10T279/17Socket type
    • Y10T279/17231Pivoted jaws
    • Y10T279/17239Moving-cam actuator
    • Y10T279/17256Reciprocating cam sleeve
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T279/00Chucks or sockets
    • Y10T279/17Socket type
    • Y10T279/17863Shouldered-tang holding
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T279/00Chucks or sockets
    • Y10T279/18Pivoted jaw
    • Y10T279/182Cam-sleeve actuated
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/42Rigid engaging means
    • Y10T292/444Swinging catch
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/46Rod end to transverse side of member
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/57Distinct end coupler
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/59Manually releaseable latch type
    • Y10T403/591Manually releaseable latch type having operating mechanism
    • Y10T403/595Lever
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/60Biased catch or latch
    • Y10T403/602Biased catch or latch by separate spring
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/60Biased catch or latch
    • Y10T403/608Pivoted

Definitions

  • This invention relates particularly to folding seat legs, and refers especially to easily releasable means for fixedly attaching the legs of such seats to the floor structurewhen the seats are in set-up usable position.
  • the object of the invention is the provision of a leg of the character described which is adapted to have releasable engagement with a fixed floor member, and is easily and quickly operable from a point adjacent to the supported seat by a person sitting thereon to effect release of the floor connection and permit a folding of the seat.
  • FIG. 1 is a perspective elevation in usable setup position of a folding-seat of a type commonly used in aircraft and equipped with legs embodying the invention
  • Fig. 2 is a similar view of the seat and its legs in folded position
  • Fig. 3 is an enlarged longitudinal section of a leg embodying the invention in engagement with its floor lock
  • Fig. 4 is a side elevation of the leg and its locking means, with parts broken away and with the locking parts moved to releasing position
  • Fig. 5 is a different side elevation of the leg as shown in Fig. 4
  • Fig. 6 is an enlarged central longitudinal section of the foot member of the leg that carries the releasable catch members
  • Figs. 7 and 8 are cross-sections on the lines '!-'I and 8-8, respectively, in Fig. 4.
  • l designates a folding-seat such as used in aircraft and which, in the present instance, has a front frame bar 2 supported in usable position by legs 3. These legs are hinged at their inner ends to the bar 2 to be folded lengthwise thereagainst, as shown in Fig. 4.
  • Each leg 3, in which the invention resides, comprises a standard 4 preferably of tubular form that is pivotally connected at its upper end to a hinge member 5 mounted on the bar 2 to permit folding against the bar.
  • a foot-piece 6 is attached to the lower end of the standard 4 preferably by inserting the lower end of the standard into a socket 1 in the top of the footpiece and connecting them by a pin 8.
  • the lower end of the foot-piece is adapted to seat on a floor plate 9 secured to the adjacent fioor structure and is provided with a central recess ID for fitting over a lock button H that is fixed to and projects above the floor plate.
  • each catch finger has a spur IT at its upper end projecting outwardly therefrom beyond the side ofthe footpiece 6 and forming a downwardly facing cam surface I8 at its outer side for the purpose hereinafter described.
  • a trip sleeve 20 Fitted around the leg standard 4 for longitudinal sliding movements thereon is a trip sleeve 20 having an enlargement 2
  • a coiled expansion spring 23 is disposed in the space between the standard 4 and sleeve enlargement 2
  • the lower sleeve enlargement 22 slidingly fits down around the foot-piece 6 and has opposing side slots 25 therein into which the respective catch finger spurs IT project.
  • the lower end walls of these slots are adapted to engage the cam surfaces l8 of the finger spurs and to coact therewith to force the upper ends of the catch fingers inward when the sleeve 20 is moved upward on the leg standard. This movement of the fingers effect a release of their hooked ends from an engaged catch button ll.
  • the trip sleeve When the trip sleeve is moved downward on the standard from a rest position, its lower end may act on the outer sides of the catch end portions of the fingers to force them into catch engagement with the lock button when the foot-piece 6 of the leg standard is resting on the floor plate, thus serving to augment the action of the spring Hi.
  • the lower end of the sleeve enlargement 22 is slotted, as at 26, to
  • a leg standard a floor-lock member adapted to have interengagement with the lower end of the leg when the latter is in usable position
  • catch means normally operable to have releasable catch engagement with the floor member when the standard and floor member are in predetermined interengaged relation
  • said catch means comprising a plurality of catch levers disposed longitudinally of the leg standard and pivoted thereto for rocking movement to release and engage the floor-lock member when in register therewith, spring means acting on the inner ends of said catch levers to normally force them outwardly, each catch lever having an outwardly disposed cam projection on its inner end portion above its fulcrum with the cam surface of the projection facing outward- 1y, a sleeve mounted on the leg standard for movement lengthwise thereof and having openings for receiving the cam projections of the levers whereby an upward movement of the sleeve on the leg standard will cause the outer end walls of said openings to coact with said cam surfaces to eifect a positive release of the catch levers from holding engagement with the

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chair Legs, Seat Parts, And Backrests (AREA)

Description

5 w. A. ENGEL zfi fim AIRCRAFT SEAT LEG RELEASE MEANS Filed June 16, 1949 2 mm 1 IN VEN TOR. I I iLL AMAENEBL;
WM A
ATTYS.
ZQGM B Oct. 21, 1952 w. A.-E N 5EL AIRCRAFT SEAT LEG RELBA$E MEANS v INVENTORZ WfLLJAM I. ENEEL BY Filed June 16, 1949 ATTYS- Patented Oct. 21, 1952 I UNITED STATES PATENT 1 OFFICE This inventionrelates particularly to folding seat legs, and refers especially to easily releasable means for fixedly attaching the legs of such seats to the floor structurewhen the seats are in set-up usable position.
The object of the invention is the provision of a leg of the character described which is adapted to have releasable engagement with a fixed floor member, and is easily and quickly operable from a point adjacent to the supported seat by a person sitting thereon to effect release of the floor connection and permit a folding of the seat.
Further objects and advantages of the invention will be apparent from the following detailed description, and from the accompanying drawings illustrating one embodiment of the invention, in whichi Fig. 1 is a perspective elevation in usable setup position of a folding-seat of a type commonly used in aircraft and equipped with legs embodying the invention; Fig. 2 is a similar view of the seat and its legs in folded position; Fig. 3 is an enlarged longitudinal section of a leg embodying the invention in engagement with its floor lock; Fig. 4 is a side elevation of the leg and its locking means, with parts broken away and with the locking parts moved to releasing position; Fig. 5 is a different side elevation of the leg as shown in Fig. 4; Fig. 6 is an enlarged central longitudinal section of the foot member of the leg that carries the releasable catch members, and Figs. 7 and 8 are cross-sections on the lines '!-'I and 8-8, respectively, in Fig. 4.
In Figs. 1 and 2, l designates a folding-seat such as used in aircraft and which, in the present instance, has a front frame bar 2 supported in usable position by legs 3. These legs are hinged at their inner ends to the bar 2 to be folded lengthwise thereagainst, as shown in Fig. 4.
Each leg 3, in which the invention resides, comprises a standard 4 preferably of tubular form that is pivotally connected at its upper end to a hinge member 5 mounted on the bar 2 to permit folding against the bar. A foot-piece 6 is attached to the lower end of the standard 4 preferably by inserting the lower end of the standard into a socket 1 in the top of the footpiece and connecting them by a pin 8. The lower end of the foot-piece is adapted to seat on a floor plate 9 secured to the adjacent fioor structure and is provided with a central recess ID for fitting over a lock button H that is fixed to and projects above the floor plate.
the recess l0 and is adapted to engage in the side recess I5 of the lock button ll toretain the leg standard in locked engagement with the foot plate 9. The upper ends of the catch fingers 14 extend above the pivots l3 and enter therespective side portions of the socket I and registering slots in the standard tube 4 and are connected in said recess by a coiled expansion spring I6. This spring acts to yieldingly urge the upper ends of the catch fingers outward so as to force their lower ends into catch engagement with the lock button I l. Each catch finger has a spur IT at its upper end projecting outwardly therefrom beyond the side ofthe footpiece 6 and forming a downwardly facing cam surface I8 at its outer side for the purpose hereinafter described.
Fitted around the leg standard 4 for longitudinal sliding movements thereon is a trip sleeve 20 having an enlargement 2| at its upper end and an enlargement 22 at its lower end. A coiled expansion spring 23 is disposed in the space between the standard 4 and sleeve enlargement 2|, and has one end-thrust against the lower end of said enlargement and its other end-thrust against a sleeve or shoulder part 24 fixed to the upper end portion of the standard within said enlargement (Fig. 4).
The lower sleeve enlargement 22 slidingly fits down around the foot-piece 6 and has opposing side slots 25 therein into which the respective catch finger spurs IT project. The lower end walls of these slots are adapted to engage the cam surfaces l8 of the finger spurs and to coact therewith to force the upper ends of the catch fingers inward when the sleeve 20 is moved upward on the leg standard. This movement of the fingers effect a release of their hooked ends from an engaged catch button ll. When the trip sleeve is moved downward on the standard from a rest position, its lower end may act on the outer sides of the catch end portions of the fingers to force them into catch engagement with the lock button when the foot-piece 6 of the leg standard is resting on the floor plate, thus serving to augment the action of the spring Hi. In the present instance, the lower end of the sleeve enlargement 22 is slotted, as at 26, to
3 receive the lower end portions of the catch fingers.
In aircraft service, it is desirable to employ seats that are firmly locked to the floor when in use and which may be folded against the wall of the aircraft when not in use. It is also desirable to provide floor locking means in connection with the legs, which means can be easily and quickly unlocked by a person sitting on the seat and before rising therefrom. This is accomplished with the present leg construction by the person merely reaching over to enable him to grasp the trip sleeve 20 of a leg and then to move the sleeve upwardly on the leg standard 4 against the tension of the spring 23, and thus effect a release of the catch fingers M from locking engagement with the fioor or look button H. This release of the catch fingers is effected by reason of the lower end walls of the sleeve slots 25 engaging the tapered or cam edges ill of the finger spurs I1 and forcing the upper ends of the fingers inward against the tension of the spring [6. When the catch fingers of a leg havebeen released from the look button, the leg may be raised to disengage the lock button from the recess I in the lower end of the foot-piece 6 and the leg then folded against the front seat bar 2. When setting up a seat in unfolded position, a leg may be easily and quickly engaged with a lock button by forcing the foot-rest recess 10 down over the button while the catch sleeve 29 is held retracted, thus holding the catch fingers in released position.
I wish it understood that my invention is not limited to any specific construction, arrangement or form of the parts, as it is capable of numerous modifications and changes without departing from the spirit of the claim.
Having thus described my invention, what I claim as new, and desire to secure by United States Letters Patent, is:
In combination, a leg standard, a floor-lock member adapted to have interengagement with the lower end of the leg when the latter is in usable position, catch means normally operable to have releasable catch engagement with the floor member when the standard and floor member are in predetermined interengaged relation, said catch means comprising a plurality of catch levers disposed longitudinally of the leg standard and pivoted thereto for rocking movement to release and engage the floor-lock member when in register therewith, spring means acting on the inner ends of said catch levers to normally force them outwardly, each catch lever having an outwardly disposed cam projection on its inner end portion above its fulcrum with the cam surface of the projection facing outward- 1y, a sleeve mounted on the leg standard for movement lengthwise thereof and having openings for receiving the cam projections of the levers whereby an upward movement of the sleeve on the leg standard will cause the outer end walls of said openings to coact with said cam surfaces to eifect a positive release of the catch levers from holding engagement with the floor-lock member, said sleeve extending to near the upper end of the leg standard, and means acting against the sleeve and leg standard to normally hold the sleeve in its downwardly extended position.
WILLIAM A. ENGEL.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US9950549 1949-06-16 1949-06-16 Aircraft seat leg release means Expired - Lifetime US2614781A (en)

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Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699802A (en) * 1951-04-16 1955-01-18 Svenska Maskinverken Ab Device for sealing open tube ends or the like
US2715379A (en) * 1951-01-22 1955-08-16 Russell G Solheim Diving bell
US2834304A (en) * 1954-09-21 1958-05-13 Evans Prod Co Freight loading apparatus
US2851234A (en) * 1952-02-23 1958-09-09 Frederick W Scheifele Fishing rod support
US2890745A (en) * 1956-08-16 1959-06-16 Martin M Pientkewic Mobile frame mounted tire removing device
US2900925A (en) * 1955-01-07 1959-08-25 Evans Prod Co Freight securing bar
US2942897A (en) * 1957-12-10 1960-06-28 Eon Corp Fastening device
US2991830A (en) * 1958-01-09 1961-07-11 Daniels C R Inc Folding leg assembly for airplanes and other usage
US3147018A (en) * 1962-08-01 1964-09-01 Reichert August Self-centering holder for automatic tube filling machines and a jaw member therefor
US3171183A (en) * 1961-06-20 1965-03-02 James R Johnston Utility fastener
US3240520A (en) * 1962-11-16 1966-03-15 North American Aviation Inc Quick releasing high strength connector
US3461933A (en) * 1966-02-15 1969-08-19 Moulinex Sa Rotary blade domestic appliance
US3600999A (en) * 1970-02-16 1971-08-24 Houdaille Industries Inc Punching tool assembly
US4501404A (en) * 1981-07-24 1985-02-26 Textron Inc. Quick disconnect assembly
US4813310A (en) * 1987-10-28 1989-03-21 Moynihan Patrick B Pliers with interchangeable jaws
US6478503B1 (en) * 2001-06-26 2002-11-12 Pao-Hsien Cheng Locking device for a detachable handrest of a stroller
US20100107846A1 (en) * 2008-11-06 2010-05-06 Wilson Tool International Inc. Punch assemblies and methods for modifying
US20100329774A1 (en) * 2007-05-16 2010-12-30 Takeo Komamura Connection device
US20110181005A1 (en) * 2010-01-25 2011-07-28 Jeff Whisenand Remotely controllable rotary switch actuator
US8667663B2 (en) 2008-12-05 2014-03-11 Sikorsky Aircraft Corporation Eccentric fitting assembly
US8707841B2 (en) 2011-11-11 2014-04-29 Wilson Tool International Inc. Punch assemblies and universal punch therefor
US9156652B1 (en) * 2014-01-07 2015-10-13 Alan R. Warboys Speedy winch adapter
US9381023B2 (en) * 2011-04-07 2016-07-05 DePuy Synthes Products, Inc. Surgical drill instrument with motor and locking mechanism to receive an attachment and a cutting burr
US9402638B2 (en) 2011-04-07 2016-08-02 DePuy Synthes Products, Inc. Cutting burr shank configuration
US9409223B2 (en) 2011-11-11 2016-08-09 Wilson Tool International Inc. Punch assemblies and universal punch therefor
US20170234350A1 (en) * 2003-11-17 2017-08-17 Telezygology, Inc. Fasteners and Other Assemblies
USD820328S1 (en) 2015-12-31 2018-06-12 Mate Precision Tooling, Inc. Punch insert
USD822725S1 (en) 2015-12-31 2018-07-10 Mate Precision Tooling, Inc. Punch insert
US20180345351A1 (en) * 2017-05-30 2018-12-06 Dale Natoli Punch Assembly with Quick Release Removable Head
US10265756B2 (en) 2012-02-06 2019-04-23 Mate Precision Tooling, Inc. Punch assembly with steel punch point insert removably secured therein
US10328479B2 (en) 2015-02-09 2019-06-25 Mate Precision Tooling, Inc. Punch assembly with replaceable punch tip secured by coupling pin
US20220313336A1 (en) * 2021-03-31 2022-10-06 Medos International Sárl Orthopedic instrument adapters
US11667051B2 (en) 2020-09-23 2023-06-06 Wilson Tool International Inc. Punch assemblies and toolless systems thereof for tip retention and release

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US938534A (en) * 1909-01-02 1909-11-02 Highland Falls Mfg Company Drill.
US1575149A (en) * 1925-02-11 1926-03-02 James L Craig Screw holder and driver
US2448817A (en) * 1944-11-11 1948-09-07 Reconstruction Finance Corp Fastening device
US2567605A (en) * 1949-08-04 1951-09-11 George W Kean Collet chuck

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US938534A (en) * 1909-01-02 1909-11-02 Highland Falls Mfg Company Drill.
US1575149A (en) * 1925-02-11 1926-03-02 James L Craig Screw holder and driver
US2448817A (en) * 1944-11-11 1948-09-07 Reconstruction Finance Corp Fastening device
US2567605A (en) * 1949-08-04 1951-09-11 George W Kean Collet chuck

Cited By (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2715379A (en) * 1951-01-22 1955-08-16 Russell G Solheim Diving bell
US2699802A (en) * 1951-04-16 1955-01-18 Svenska Maskinverken Ab Device for sealing open tube ends or the like
US2851234A (en) * 1952-02-23 1958-09-09 Frederick W Scheifele Fishing rod support
US2834304A (en) * 1954-09-21 1958-05-13 Evans Prod Co Freight loading apparatus
US2900925A (en) * 1955-01-07 1959-08-25 Evans Prod Co Freight securing bar
US2890745A (en) * 1956-08-16 1959-06-16 Martin M Pientkewic Mobile frame mounted tire removing device
US2942897A (en) * 1957-12-10 1960-06-28 Eon Corp Fastening device
US2991830A (en) * 1958-01-09 1961-07-11 Daniels C R Inc Folding leg assembly for airplanes and other usage
US3171183A (en) * 1961-06-20 1965-03-02 James R Johnston Utility fastener
US3147018A (en) * 1962-08-01 1964-09-01 Reichert August Self-centering holder for automatic tube filling machines and a jaw member therefor
US3240520A (en) * 1962-11-16 1966-03-15 North American Aviation Inc Quick releasing high strength connector
US3461933A (en) * 1966-02-15 1969-08-19 Moulinex Sa Rotary blade domestic appliance
US3600999A (en) * 1970-02-16 1971-08-24 Houdaille Industries Inc Punching tool assembly
US4501404A (en) * 1981-07-24 1985-02-26 Textron Inc. Quick disconnect assembly
US4813310A (en) * 1987-10-28 1989-03-21 Moynihan Patrick B Pliers with interchangeable jaws
US6478503B1 (en) * 2001-06-26 2002-11-12 Pao-Hsien Cheng Locking device for a detachable handrest of a stroller
US20170234350A1 (en) * 2003-11-17 2017-08-17 Telezygology, Inc. Fasteners and Other Assemblies
US20100329774A1 (en) * 2007-05-16 2010-12-30 Takeo Komamura Connection device
US9086082B2 (en) * 2007-05-16 2015-07-21 Sofken Company, Ltd. Connection device
US8327745B2 (en) * 2008-11-06 2012-12-11 Wilson Tool International Inc. Punch assemblies and methods for modifying
US9776337B2 (en) 2008-11-06 2017-10-03 Wilson Tool International Inc. Punch assemblies and methods for modifying
US20100107846A1 (en) * 2008-11-06 2010-05-06 Wilson Tool International Inc. Punch assemblies and methods for modifying
US9687994B2 (en) 2008-11-06 2017-06-27 Wilson Tool International Inc. Punch assemblies and methods for modifying
US8667663B2 (en) 2008-12-05 2014-03-11 Sikorsky Aircraft Corporation Eccentric fitting assembly
US8534676B2 (en) * 2010-01-25 2013-09-17 Jeff Whisenand Remotely controllable rotary switch actuator
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