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Publication numberUS3570280 A
Publication typeGrant
Publication dateMar 16, 1971
Filing dateNov 6, 1968
Priority dateNov 6, 1968
Publication numberUS 3570280 A, US 3570280A, US-A-3570280, US3570280 A, US3570280A
InventorsAske Robert L
Original AssigneeHoneywell Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Control apparatus
US 3570280 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

March 16, 1971 R. L. ASKE CONTROL APPARATUS 2 Sheets-Sheet 1 Filed Nov. 6. 1968 FIG. 2

INVENTOR. ROBERT L. ASKE ATTORNEY March 16, 1971 Filed NOV. 6. 1968 R. L. ASKE CONTROL APPARATUS FIG. 4

2 Sheets-Sheet 2 HOURS i'NVENTOR. ROBERT L. ASKE ATTORNEY United States Patent Ofiice 3,570,280 Patented Mar. 16, 1971 ABSTRACT OF THE DISCLOSURE A composite material comprising an elastic material in contiguous relationship with a material having the property of creep under stress. The material is contemplaced for use in various configurations to serve a time delay function.

BACKGROUND OF THE INVENTION Field of the invention The present invention pertains to composite metals and their use as time delay devices.

Description of the prior art Numerous timing devices are well-known in the prior art wherein spring action is retarded by a damper. A common example is the spring-shock absorber combination used on vehicles. In this case, the normally fast action of the spring is retarded by the shock absorber characterlstics.

Timing devices utilizing a spring-powered clock escapement are also well-known in the art. Again the stored energy of the spring is dissipated at a controlled rate dependent on the clock escapement.

Numerous devices wherein normally fast spring forces are retarded come to mind; however, each have the disadvantage of requiring two separate components: the spring and a damping device.

It is an object of the present invention to provide a composite material having applicability to time delay devices.

SUMMARY OF THE INVENTION The present invention pertains to the use of a composite material to provide various timing characteristics in a spring device. The invention is concerned with a single component to replace spring-damper combinations of the prior art.

The delay spring of the present invention comprises a material of elastic properties coated with a material having the property of creep under stress. The property of creep is well-known in metallurgy and is exhibited by materials such as lead, copper, and tin. The particular configuration of the device may be varied to satisfy different requirements. The inner core is made from a suitable spring material which provides the necessary stress to allow creep to take place in the outer coating. The time delay characteristics are controllable by varying a number of parameters such as creep material composition and diameter, core material composition and diameter, length (for linear motion) or number of turn (for rotational motion), or spring mean diameter.

The invention is contemplated for use with ordnance devices to replace temperature sensitive chemical timers. A bimetal inner core is contemplated to provide tempera ture compensation.

The delay spring is desirable over chemical timers in that it may be used more than once. Further, the delay spring will do useful work while providing its delay action, as may be required in an ordnance device for mechanical arming of a munition.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a top view of a timing device utilizing the material of the present invention.

FIG. 2 is a vertical sectional view through the timing device of FIG. 1.

FIG. 3 is a section of the delay spring material of the present invention as used in the embodiment of FIGS. 1 and 2.

FIG. 4 is a graph representing the performance of a successful embodiment of the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENT Referring to FIG. 2, a rotor 2 is rotatably mounted on a shaft 3 which is part of a base 1. The rotor 2 is secured to the shaft 3 by a C-ring 4. A cam disk 5 is secured to the top of rotor 2..

Referring to FIG. 1, a top view of the device shown in section view in FIG. 2, a pivoted arm 6 engages a notch in the perimeter of cam disk 5. A second pivoted arm 7 rides on the edge of cam disk 5.

In operation, the rotor 2 is turned in a counterclockwise direction to a starting point where it is held by engaging pivoted arm 6 with the notch in the perimeter of the disk 5. At the initiation of the timing sequence, pivoted arm 6 is pivoted away from the cam disk 5 and the disk 5 and rotor 2 are free to turn. The rotor 2 turns in a clockwise direction at a speed determined by the delay spring characteristics until the disk turns approximately one-half a revolution and the pivoted arm 7 engages the notch, causing a desired response, such as release of a striker to initiate an explosive detonator.

FIG. 3 illustrates a section of the composite material of the present invention as employed in the embodiment of FIGS. 1 and 2. An elastic material 10 is contiguously surrounded by a material 11 having the property of creep under stress. Material 10 of FIG. 3 is suitable spring material to provide stress to allow creep to take place in the material 11. Examples of suitable metals for creep material 11 are lead, tin, solder and copper.

A successful embodiment of the present invention was constructed with an inner core material of .008 inch music wire 7.5 inches in length. The outer creep mate rial 11 was Kester solder alloy Sn60, .062 inch in diameter and 7.5 inches in length. The spring material was wound in a coil having an outside diameter of .374 inch with an inside diameter of .250 inch. The original number of turns was 7% and the original free length was .508 inch.

Operation of the spring is shown in the graph of FIG. 4. The curve presented is the number of turns in the delay spring as a function of time. Data was taken at +35 degrees Fahrenheit.

The delay spring will tend to return to its original configuration as long as deformation is within the elastic limits of the inner core material and the elastic material exerts enough stress on the creep material.

The properties of the delay spring of the present invention can be realized by many different configurations. It is understood, therefore, that the specific embodiments of my invention shown here are for the purpose of illustration only, and that my invention i limited only by the scope of the appended claims.

What is claimed is:

1. Timing apparatus, comprising:

a deformable composite material of an elastic material in contiguous relationship with a creep material, having a preferred configuration; and

means in operative combination with said composite material for indicating the configuration of said com .4 posite material, whereby said composite material, creep material is chosen from the group consisting of after deformation within the elastic limits of said lead, tin, copper, and combinations thereof. elastic material, returns to said preferred configuration after a predetermined time interval. References Cited if 5 UNITED STATES PATENTS a ase mem er avlng a s a tt ereon;

a rotor rotatably mounted on said shaft; 3283591 11/1966 Green 74 3'5 a delay spring of an elastic material contiguously re- FOREIGN PATENTS lated to a Creep material; and 71, 37 1959 France 2 7 1g2 means engaging said spring to said base and said rotor 10 whereby as said rotor is rotated about said base OTHER REFERENCES said spring is stressed and said spring tends to return German printed application; Stranmann et aL; 1,154; to its unstressed position after a predetermined time Sept 26, 1963. mterval- German printed application; Seiler et 211.; 1,179,051;

3. The apparatus of claim 2 where said rotor has a 15 Oct 7, 1964 cavity therein and said delay spring is located within said cavity a d around a Shaft MILTON KAUFMAN, Primary Examiner 4. The timing device of claim 3 wherein said first elastle material is a spring metal. US. Cl. X.R.

5. The timing device of claim 3 wherein said second 267-182; l0282

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US5500122 *May 11, 1994Mar 19, 1996UopStacked fluid-separation membrane disk module assemblies
US5520807 *May 11, 1994May 28, 1996UopStacked fluid-separation membrane disk module assemblies
US5536405 *May 11, 1994Jul 16, 1996UopStacked membrane disk assemblies for fluid separations
Classifications
U.S. Classification74/3.5, 102/255, 267/182
International ClassificationF42C9/02, F42C9/00, F42C15/00, F42C9/08
Cooperative ClassificationF42C9/02, F42C15/00, F42C9/08
European ClassificationF42C9/08, F42C9/02, F42C15/00