US3570280A - Control apparatus - Google Patents
Control apparatus Download PDFInfo
- Publication number
- US3570280A US3570280A US773714A US3570280DA US3570280A US 3570280 A US3570280 A US 3570280A US 773714 A US773714 A US 773714A US 3570280D A US3570280D A US 3570280DA US 3570280 A US3570280 A US 3570280A
- Authority
- US
- United States
- Prior art keywords
- spring
- creep
- delay
- rotor
- elastic
- 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.)
- Expired - Lifetime
Links
- 239000000463 material Substances 0.000 abstract description 24
- 239000002131 composite material Substances 0.000 abstract description 9
- 239000013013 elastic material Substances 0.000 abstract description 7
- 239000011162 core material Substances 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 229910052718 tin Inorganic materials 0.000 description 3
- 239000006096 absorbing agent Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 102100026459 POU domain, class 3, transcription factor 2 Human genes 0.000 description 1
- 101710133394 POU domain, class 3, transcription factor 2 Proteins 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/02—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/08—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by chemical action, e.g. of acids
-
- 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
- Y10T74/00—Machine element or mechanism
- Y10T74/11—Tripping mechanism
- Y10T74/114—Retarded
Definitions
- the present invention pertains to composite metals and their use as time delay devices.
- 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.
- 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.
- 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.
- 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.
- 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..
- 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.
- 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.
- 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.
- 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.
- Timing apparatus comprising:
- 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;
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Springs (AREA)
Abstract
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.
Description
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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77371468A | 1968-11-06 | 1968-11-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3570280A true US3570280A (en) | 1971-03-16 |
Family
ID=25099091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US773714A Expired - Lifetime US3570280A (en) | 1968-11-06 | 1968-11-06 | Control apparatus |
Country Status (1)
Country | Link |
---|---|
US (1) | US3570280A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5500122A (en) * | 1994-05-11 | 1996-03-19 | Uop | Stacked fluid-separation membrane disk module assemblies |
US5520807A (en) * | 1994-05-11 | 1996-05-28 | Uop | Stacked fluid-separation membrane disk module assemblies |
US5536405A (en) * | 1994-05-11 | 1996-07-16 | Uop | Stacked membrane disk assemblies for fluid separations |
-
1968
- 1968-11-06 US US773714A patent/US3570280A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5500122A (en) * | 1994-05-11 | 1996-03-19 | Uop | Stacked fluid-separation membrane disk module assemblies |
US5520807A (en) * | 1994-05-11 | 1996-05-28 | Uop | Stacked fluid-separation membrane disk module assemblies |
US5536405A (en) * | 1994-05-11 | 1996-07-16 | Uop | Stacked membrane disk assemblies for fluid separations |
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