US2513157A - Nose structure for projectiles - Google Patents
Nose structure for projectiles Download PDFInfo
- Publication number
- US2513157A US2513157A US479516A US47951643A US2513157A US 2513157 A US2513157 A US 2513157A US 479516 A US479516 A US 479516A US 47951643 A US47951643 A US 47951643A US 2513157 A US2513157 A US 2513157A
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- United States
- Prior art keywords
- antenna
- container
- projectile
- insulating member
- casing
- 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
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-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
Definitions
- This invention relates to nose structures for projectiles and more particularly to a novel structure of this character for use in a radio-controlled projectile, which includes an antenna.
- Radio apparatus in the casing is used as a control means for the projectile, as, for example, to steer it in its flight or tocause detonation of an explosive charge therein when the projectile is in proximity to a target.
- a radio apparatus in the casing is used as a control means for the projectile, as, for example, to steer it in its flight or tocause detonation of an explosive charge therein when the projectile is in proximity to a target.
- considerable difiiculty has beenencountered in mounting the antenna of the radio apparatus on the projectile casing. More particularly, the mechanical shock to which projectiles are commonly subjected, as in handling, loading and firing, tend to displace or distort the antenna on the projectile, with the result that operation of the radio apparatus is impaired.
- One object of the present invention resides in the provision of a novel antenna unit included in the nose structure of a projectile,
- a nose structure made in accordance with the present invention comprises a generally conical antenna in the form of a projectile nose, and means for connectingthe antenna to the casing of the projectile.
- the antenna is provided with a dish-shaped base which fits closely against a member having a complementary shape and connected to the projectile casing, whereby the antenna is held securely against lateral movement on the casing.
- Another object of the invention is to provide a nose structure for projectiles which includes an antenna and a container connected to the antenna for receiving part of a radio apparatus.
- the container is generally cup-shaped and has an insulating member mounted over its open end between the container and the antenna, the insulating member having a passage for wiring between the antenna and the container.
- FIG. 1 is an axial sectional view of part of a projectile having one form of the new nose structure
- Figs. 2 to 5, inclusive are perspective views of parts of the structure shown in Fig. l.
- Fig. 6 is a sectional view on the plane 66 in Fig. 1.
- the nose structure of the present invention is shown mounted on a projectile comprising a hollow casing l0 having an internally threaded portion H adjacent its forward end.
- a cylindrical container I2 is secured in the forward end of the casing by means of threads mating with the threaded portion II, the container extending rearwardly in the casing for a substantial distance.
- the container is designed to receive parts of a radio apparatus (not shown) for controlling the projectile, as illustrated, for example, in a copending application of M. A. Tuve, et a1., Serial No. 471,388, filed January 6, 1943.
- the container In front of the threaded portion H, the container is enlarged to form an external shoulder l3 engaging the end of the projectile casing.
- the side wall M of the enlargement is generally frusto-conical so that it conforms to and provides a continuation of the tapered contour of the front end portion of the casing.
- the container I2 is open at its forward end where it receives an inner, cupshaped container IS, the bottom of which is disposed intermediate the ends of the container l2.
- the inner container I5 is provided, with an outwardly extending peripheral flange l6 seated on the forward end of the enlargement of the outer container.
- a generally dish-shaped plate 3 is seated on the flange IS in front of the containers and receives an insulating member l9 having a central passage 20 extending through the member.
- the front face of the insulating member I!) is concave, and closely fitted therein is the convex base 2
- the antenna is spun or otherwise made in a conical shape so as to form the nose of the projectile.
- Bolts 23 extend through the base of the antenna, the insulating member l9, plate i8 and flange I6 and are threaded in the enlargement of the outer container 12 to hold the parts in position.
- the bolts 23 are suitably insulated from the antenna 22, as .by means of insulating washers 24.
- the antenna 22 as shown, comprises a generally frusto-conical part 25 integral with the base 2
- the plug 26 may be secured in any suitable manner, as by bifurcating its rear end portion to form a pair of diverging spring legs 21 extending into the end of the hollow part 25.
- a screw 28 is mounted on the base 2
- the nose structure of the invention is compact and rugged and is suitable for manufacture at low cost.
- the bolts 23 secure the parts against relative movement and connect the nose structure to the projectile casing through the outer container II.
- the plate II, the insulating member I! and the antenna base II of concave-convex form and litting them closely together, the parts eilectively resist lateral movement on the casing due to the usual shocks to which projectiles are subjected.
- the plate ll serves as an electrical shield between the radio parts in the-container l5 and the antenna 22 and insulating member l3.
- a cup-shaped container adapted to flt in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an opening therethrough, an insulating member on the plate andhaving a wiring passage communicating with said opening, an antenna on said member, and attaching means for jointly connecting the antenna, insulating member and plate to said flange.
- a cup-shaped container adapted to fit in a projectile casing and having a chmnber for receiving part of radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an opening therethrough, an insulating member on the plate and having a wiring passage communicating with said opening, a generally conical antenna in the form of a projectile nose and having a base, a connecting bolt extending through said base, insulating member, plate and flange, and means for insulating the bolt from the antenna.
- a container adapted to lit in a projectile casing and having a chamber for receiving part 01' a radio apparatus, an antenna, an insulating member between the container and the antenna, an electrical shield between the container and the antenna and insulating member,
- a container designed to fit in a projectile casing and having a chamber for receiving part of a radio apparatus, a frustoconical hollow antenna, an insulating member between the container and the antenna, said antenna having a portion projecting inwardly at its base, and means passing through said portion, and said insulating member and secured to said container, to hold the antenna in place.
- a cup-shaped container designed to fit in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flang around its open end, a hollow antenna having a base, an insulating member between said base and the flange of the container, and securing means insulated from the base but extending through said base, said insulating member and said flange, to hold the antenna in place while keeping it electrically insulated from the projectile casing.
- a cup-shaped container designed to flt in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an .opening therethrough, an insulating member on the plate and having a wiring passage communicating with said opening, a generally frusto-conlcal antenna forming an open-end projectile nose and having a base, a connecting bolt extending through said base, insulating member, plate and flange, means for insulating the bolt froin the antenna, access to said -bolt being provided.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Details Of Aerials (AREA)
Description
June 27, 1950 R0. FERRIS ETAL.
NOSE STRUCTURE FOR PROJECTILES Filed March 17, 1943 IIWENTORS ROBERT 6. BY SH?!) Patented June 27, 1950 F KC NOSE STRUCTURE FOR PROJECTIILES retary of the Navy Application March 17, 1943, Serial N0. 479,516
6 Claims.
This invention relates to nose structures for projectiles and more particularly to a novel structure of this character for use in a radio-controlled projectile, which includes an antenna.
- Projectiles have been devised heretofore wherein a. radio apparatus in the casing is used as a control means for the projectile, as, for example, to steer it in its flight or tocause detonation of an explosive charge therein when the projectile is in proximity to a target. In such projectiles, considerable difiiculty has beenencountered in mounting the antenna of the radio apparatus on the projectile casing. More particularly, the mechanical shock to which projectiles are commonly subjected, as in handling, loading and firing, tend to displace or distort the antenna on the projectile, with the result that operation of the radio apparatus is impaired.
One object of the present invention, therefore, resides in the provision of a novel antenna unit included in the nose structure of a projectile,
which is of rugged construction so that it is suitable to withstand the usual stresses to which projectiles are subjected, without displacement of the antenna. A nose structure made in accordance with the present invention comprises a generally conical antenna in the form of a projectile nose, and means for connectingthe antenna to the casing of the projectile. Preferably, the antenna is provided with a dish-shaped base which fits closely against a member having a complementary shape and connected to the projectile casing, whereby the antenna is held securely against lateral movement on the casing.
Another object of the invention is to provide a nose structure for projectiles which includes an antenna and a container connected to the antenna for receiving part of a radio apparatus. In the preferred construction, the container is generally cup-shaped and has an insulating member mounted over its open end between the container and the antenna, the insulating member having a passage for wiring between the antenna and the container.
These and other objects of the invention may be understood by reference to the accompanying drawing. in which Fig. 1 is an axial sectional view of part of a projectile having one form of the new nose structure;
Figs. 2 to 5, inclusive, are perspective views of parts of the structure shown in Fig. l, and
Fig. 6 is a sectional view on the plane 66 in Fig. 1.
The nose structure of the present invention is shown mounted on a projectile comprising a hollow casing l0 having an internally threaded portion H adjacent its forward end. A cylindrical container I2 is secured in the forward end of the casing by means of threads mating with the threaded portion II, the container extending rearwardly in the casing for a substantial distance. The container is designed to receive parts of a radio apparatus (not shown) for controlling the projectile, as illustrated, for example, in a copending application of M. A. Tuve, et a1., Serial No. 471,388, filed January 6, 1943. In front of the threaded portion H, the container is enlarged to form an external shoulder l3 engaging the end of the projectile casing. The side wall M of the enlargement is generally frusto-conical so that it conforms to and provides a continuation of the tapered contour of the front end portion of the casing. The container I2 is open at its forward end where it receives an inner, cupshaped container IS, the bottom of which is disposed intermediate the ends of the container l2. At its open end, the inner container I5 is provided, with an outwardly extending peripheral flange l6 seated on the forward end of the enlargement of the outer container.
A generally dish-shaped plate 3 is seated on the flange IS in front of the containers and receives an insulating member l9 having a central passage 20 extending through the member. The front face of the insulating member I!) is concave, and closely fitted therein is the convex base 2| of a metal antenna 22. The antenna is spun or otherwise made in a conical shape so as to form the nose of the projectile. Bolts 23 extend through the base of the antenna, the insulating member l9, plate i8 and flange I6 and are threaded in the enlargement of the outer container 12 to hold the parts in position. The bolts 23 are suitably insulated from the antenna 22, as .by means of insulating washers 24.
The antenna 22, as shown, comprises a generally frusto-conical part 25 integral with the base 2|, and a conical plug 26 mounted on the reduced end of the part 25. The plug 26 may be secured in any suitable manner, as by bifurcating its rear end portion to form a pair of diverging spring legs 21 extending into the end of the hollow part 25. A screw 28 is mounted on the base 2| of the antenna and provides a terminal for electrical connection through the passage 20 and an alined opening 29 in plate l8 to part of the radio apparatus (not shown) in the container l5.
It will be evident that the nose structure of the invention is compact and rugged and is suitable for manufacture at low cost. The bolts 23 secure the parts against relative movement and connect the nose structure to the projectile casing through the outer container II. By making the plate II, the insulating member I! and the antenna base II of concave-convex form and litting them closely together, the parts eilectively resist lateral movement on the casing due to the usual shocks to which projectiles are subjected. The plate ll serves as an electrical shield between the radio parts in the-container l5 and the antenna 22 and insulating member l3.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. In combination, a cup-shaped container adapted to flt in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an opening therethrough, an insulating member on the plate andhaving a wiring passage communicating with said opening, an antenna on said member, and attaching means for jointly connecting the antenna, insulating member and plate to said flange.
2. In combination, a cup-shaped container adapted to fit in a projectile casing and having a chmnber for receiving part of radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an opening therethrough, an insulating member on the plate and having a wiring passage communicating with said opening, a generally conical antenna in the form of a projectile nose and having a base, a connecting bolt extending through said base, insulating member, plate and flange, and means for insulating the bolt from the antenna.
3. In combination, a container adapted to lit in a projectile casing and having a chamber for receiving part 01' a radio apparatus, an antenna, an insulating member between the container and the antenna, an electrical shield between the container and the antenna and insulating member,
and means for connecting the container, insulating member, antenna and shield to a projectile casing.
4. In combination, a container designed to fit in a projectile casing and having a chamber for receiving part of a radio apparatus, a frustoconical hollow antenna, an insulating member between the container and the antenna, said antenna having a portion projecting inwardly at its base, and means passing through said portion, and said insulating member and secured to said container, to hold the antenna in place.
5. In combination, a cup-shaped container \designed to fit in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flang around its open end, a hollow antenna having a base, an insulating member between said base and the flange of the container, and securing means insulated from the base but extending through said base, said insulating member and said flange, to hold the antenna in place while keeping it electrically insulated from the projectile casing.
6. In combination, a cup-shaped container designed to flt in a projectile casing and having a chamber for receiving part of a radio apparatus, the container having a flange around its open end, a plate seated on the flange and having an .opening therethrough, an insulating member on the plate and having a wiring passage communicating with said opening, a generally frusto-conlcal antenna forming an open-end projectile nose and having a base, a connecting bolt extending through said base, insulating member, plate and flange, means for insulating the bolt froin the antenna, access to said -bolt being provided.
through the said open end, and a substantially conical removable tip for closing said open end.
ROBERT G. FERRIS.
SHELDON H. DIKE.
REFERENCES CITED The following references are of record Sweden Dec. 22, 1937
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US479516A US2513157A (en) | 1943-03-17 | 1943-03-17 | Nose structure for projectiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US479516A US2513157A (en) | 1943-03-17 | 1943-03-17 | Nose structure for projectiles |
Publications (1)
Publication Number | Publication Date |
---|---|
US2513157A true US2513157A (en) | 1950-06-27 |
Family
ID=23904351
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US479516A Expired - Lifetime US2513157A (en) | 1943-03-17 | 1943-03-17 | Nose structure for projectiles |
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US (1) | US2513157A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2700112A (en) * | 1949-03-07 | 1955-01-18 | Alford Andrew | Antenna structure |
US2828413A (en) * | 1956-06-21 | 1958-03-25 | Bell Telephone Labor Inc | Self-contained antenna-radio system in which a split conductive container forms a dipole antenna |
US3000310A (en) * | 1956-07-13 | 1961-09-19 | Walter C Power | Fuse housing |
US3127609A (en) * | 1960-03-30 | 1964-03-31 | Frederick L Wentworth | Antenna having ring waveguide two wavelengths long for feeding two slots in diametrically opposed portions thereof |
US4371875A (en) * | 1974-10-22 | 1983-02-01 | Licentia Patent-Verwaltungs-Gmbh | Projectile antenna |
US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US49326A (en) * | 1865-08-08 | Improvement in explosive shells for ordnance | ||
US1074111A (en) * | 1913-01-09 | 1913-09-30 | Crucible Steel Co America | Projectile. |
FR476375A (en) * | 1914-10-23 | 1915-07-29 | Ets Delaunay Belleville Sa | Smoke shell |
US2356227A (en) * | 1940-08-27 | 1944-08-22 | Diehl Elias Stanley | Projectile |
-
1943
- 1943-03-17 US US479516A patent/US2513157A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US49326A (en) * | 1865-08-08 | Improvement in explosive shells for ordnance | ||
US1074111A (en) * | 1913-01-09 | 1913-09-30 | Crucible Steel Co America | Projectile. |
FR476375A (en) * | 1914-10-23 | 1915-07-29 | Ets Delaunay Belleville Sa | Smoke shell |
US2356227A (en) * | 1940-08-27 | 1944-08-22 | Diehl Elias Stanley | Projectile |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2700112A (en) * | 1949-03-07 | 1955-01-18 | Alford Andrew | Antenna structure |
US2828413A (en) * | 1956-06-21 | 1958-03-25 | Bell Telephone Labor Inc | Self-contained antenna-radio system in which a split conductive container forms a dipole antenna |
US3000310A (en) * | 1956-07-13 | 1961-09-19 | Walter C Power | Fuse housing |
US3127609A (en) * | 1960-03-30 | 1964-03-31 | Frederick L Wentworth | Antenna having ring waveguide two wavelengths long for feeding two slots in diametrically opposed portions thereof |
US4371875A (en) * | 1974-10-22 | 1983-02-01 | Licentia Patent-Verwaltungs-Gmbh | Projectile antenna |
US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
US12055375B2 (en) | 2020-07-02 | 2024-08-06 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
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