Hookless Fastener Co. v. G. E. Prentice Mfg. Co.

75 F.2d 264, 24 U.S.P.Q. (BNA) 397, 1935 U.S. App. LEXIS 2907
CourtCourt of Appeals for the Second Circuit
DecidedFebruary 4, 1935
DocketNo. 164
StatusPublished
Cited by9 cases

This text of 75 F.2d 264 (Hookless Fastener Co. v. G. E. Prentice Mfg. Co.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Second Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Hookless Fastener Co. v. G. E. Prentice Mfg. Co., 75 F.2d 264, 24 U.S.P.Q. (BNA) 397, 1935 U.S. App. LEXIS 2907 (2d Cir. 1935).

Opinions

MANTON, Circuit Judge.

This suit is for infringement of claims 7 and 10 of the Sundback slider patent, No. 1,661,144, relating to fastener sliders, granted to plaintiff’s assignor on February 28, 1928; application filed January 27, 1925. It is used to mesh and unmesh the interlocking units arranged along the sides of a slide fastener. Claim 7 is for “a separable fastener slider comprising overlying spaced wings having inturned edges and having an internal reinforcing connection of deformed wing material extending longitudinally along the axis of said slider between said edges.” Claim 10 differs, and has “means for guiding' interlocking members, a bend directly connecting said wings, and integral longitudinal stiffening means within said bend shaped to maintain the wings in spaced relation independently of any other wing holding means and extending from said bend down to about a transverse line joining the outer wing corners.”

The second patent in suit is Sundback, No. 1,813,433, for separable bottom stops which enable slide fasteners to be used on coats and other articles in which the two halves of the fastener must be completely separated. Claim 13 was held valid and infringed. Claims 5 and 6 were held invalid, and have since been disclaimed.

The one-piece slider of the first patent, here considered, has an integral reinforcing connection, or neck, of deformed wing material. The patent discloses the method of making such a slider to be a process known as “coining” for making the neck of deformed wing material. The neck portion serves the double function of supporting the wings and constituting the inner edges of the diverging channels. In discharging this latter function, it acts as a wedge to separate the interlocked stringers when the slider is moved down to open the fastener. The [265]*265ends of the interlocking members or scoops run against the sides of the neck. The patent points out that the slider is subjected to severe operating stresses tending to spread it, as when closed under strain, and also often tending to contract it, as in a wringer when used on washable goods, and, if the fastener is to be serviceable, the slider must be rigid. The requirement for rigidity was pointed out by the defendant’s president in his patent. Advantages are claimed apart from the method of manufacture. It displaced the yoke and rivet sliders, and it has met with very considerable commercial success since its introduction in the trade.

In its manufacture this sheet metal slider is provided with integral stiffening means which can be either inside or outside of the bend, and is preferably inside. It is made short by eliminating the bent neck in favor of a bent thickened reinforce integral with the wings and directly between them; this reinforce connection preferably being V-shaped to provide inner guide surfaces for the divergent channels. This stiffens the slider against both expansion and contraction in a compact manner without a special rivet because of bringing the distorting moments closest to the center of the slider. This permits the minimum of metal to be used with maximum strength without any added strengthening part. The slider surface is smooth and free from projections and external stiffening means because the reinforce to prevent distortion of the wings is located within the bend and between the wings, is integral with the wings, and extends longitudinally from the bend to a transverse line connecting the outer wing corners. Thus the entire length of the slider is stiffened. The interlocked stringers pass through a wide channel at the bottom of the slider and the separated stringers pass through separated diverging channels at the top. This is the method of operation.

Although the desirability of a one-piece slider was known and appreciated, one was not found to achieve the desired result until this one appeared. It is made cheaply of sheet metal and still, because of its hardened internal reinforcing connection of deformed wing material, it meets the requirements of strength, rigidity, and durability.

The prior patents to which we are referred (Judson, Nos. 504,037 and 557,207) were die cast sliders; the neck portions do not consist of deformed wing material. The Kuhn-Moos British patent, No. 14,358, was described by defendant’s president as a slider made by die-casting process in accordance with which the wings and reinforcing element were made of unitary or integral construction. We think they were properly found below not to be anticipatory. They were clumsy and uneconomical to manufacture. The neck did not have the deformed wing material.

This slider was an improvement over the prior art, for it was made of one piece from sheet metal and without yoke or rivet; it had the necessary strength for commercial use and met with commercial success which speaks its inventive thought.

Claim 10 is narrower than claim 7 because it contains a limitation that “the integral longitudinal stiffening means” between the two wings of the slider shall extend a specific distance down into the slider, while claim 7 merely specifies the integral reinforcing connection extending longitudinally into the slider without specifying exactly how far it must extend. Claim 10 we think invalid, as found below, for it is not limited to deformed wing material.

Claim 7 is infringed, for the defendant’s slider is made of deformed wing material. The method by which it is made is disclosed. It is described in the defendant’s Prentice patent, No. 1,900,949. A blank is cut out of a strip of sheet metal; the edges of the wings are then turned up to form flanges, and the wings are then bent into parallelism. The neck is bent in this step so that it is slightly concave on the outside by means of a die. The cross-hatched arc-shaped sections are cross-sections of the neck at this stage of manufacture. The slider is then placed in a die, and a narrow punch is forced down against the top of the neck. The concave end of the punch pushes the neck down. Due to the form of the punch with the concave slot surface, the metal of the wings is forced inward by the bevel concave surface; as it moves down, that metal is fed down the concave surface progressively as the punch proceeds in, so that it is caused to flow from the wings down into the throat of the neck portion, and at the same time the wing portion on the side, because of the shape of the punch and due to pressing in of the two sides of the wings, is caused to flow down into the sides of the neck, and as a consequence the whole distribution of the metal in the wings and the metal originally in the neck has been changed, and has been caused to flow around and to take entirely new positions in relation to its original position, so that ultimately there is obtained a cross-[266]*266section which has depth and without appreciably thinning down the metal. Thus the deformed wing material of the plaintiff’s invention is copied. The outer edges of the neck are rounded in somewhat, and the end of the pull piece attachment which is passed throtiglfcthe opening in the neck is clinched in place. Not only is the defendant’s reinforcing connection made of deformed wing material, but the material is distributed longitudinally for the purpose of obtaining strength against the separation or compression of the wings in the same manner that the patent in suit distributes it.

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Bluebook (online)
75 F.2d 264, 24 U.S.P.Q. (BNA) 397, 1935 U.S. App. LEXIS 2907, Counsel Stack Legal Research, https://law.counselstack.com/opinion/hookless-fastener-co-v-g-e-prentice-mfg-co-ca2-1935.