US1520131A - Oblong drop projectile - Google Patents
Oblong drop projectile Download PDFInfo
- Publication number
- US1520131A US1520131A US496953A US49695321A US1520131A US 1520131 A US1520131 A US 1520131A US 496953 A US496953 A US 496953A US 49695321 A US49695321 A US 49695321A US 1520131 A US1520131 A US 1520131A
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- Prior art keywords
- steering
- tail
- projectile
- drop
- shaped
- 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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- 239000002360 explosive Substances 0.000 description 21
- 239000002184 metal Substances 0.000 description 16
- 238000010276 construction Methods 0.000 description 7
- 238000004880 explosion Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000010282 Emodin Substances 0.000 description 1
- 235000014443 Pyrus communis Nutrition 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- RHMXXJGYXNZAPX-UHFFFAOYSA-N emodin Chemical compound C1=C(O)C=C2C(=O)C3=CC(C)=CC(O)=C3C(=O)C2=C1O RHMXXJGYXNZAPX-UHFFFAOYSA-N 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
Images
Classifications
-
- 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
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B25/00—Fall bombs
Definitions
- the present invention relates to the construction of ion shaped drop projectiles and has for its 0 ject to ensure stability of the projectile in its trajectory and at the same time best utilization of the material,
- the projectile is given a lancet-shaped longitudinal section, the steering-tail being formed by a hollow coneshaped sheet-metal shell.
- This construction allows concentration of the main part of the mass of the projectile within the body of the projectile without accumulation of dead material, while the air-resistance centre is located as far as possible back within the range of the light sheet-metal steering shell.
- Figs. 1 and 2 illustrate the principles of construction and shape of the projectile in longitudinal section and a plan view thereto.
- Figs. 3 and 4 are longitudinal sections of two different constructlons of the projec from the steering-surfaces a lancet-shaped' longitudinal section in which any protruding edge and any break in the curve of STAT. I, 1318.)
- the dropping projectile may develop a rotarf; velocity in its descent sufficient to release a centrifugal safety device for its fuse, it is necessa to impart to the steering-surfaces attache to the steeringtail a screw-shaped twist.
- Such steering surfaces can easily be made by constructing the hollow cone-shaped sheet-metal rear rudder of several parts, ,the edges of which are bent out of the cone-surfaces so that they form by themselves steering-surfaces upon the cone.
- the bordered edges can particularl be so shaped, that they form steeringsu aces for the projectile.
- Arched steering surfaces made of thin sheet metal can only with difliculty be so constructed and connected :that they are adapted to. resist to the air pressure and to centrifugal forces without undergoing deformation.
- These diificulties can considerably be reduced by making the steering-surfaces out of sheet-metal strips, level at the rear end projecting beyond the cone-shaped steering-tail and arranged oblique to each other and the cone axis thus that their joints form the outline of a pyramid, while those of the cone surfaces of the steering tail run parallel to the axis and whereby the transition from the level part of the steering-surfaces to the edge of the joint on the steering tail is eifected by a corresponding arching of such surfaces.
- 1 designates the strong-walled chamber for the explosive.
- This explosive chamber is .at its forward end provided with a ,fuse which on the drawing is only diagrammatically illustrated and designated with the numeral 2 and at its rear end with a cap for charging the projectile with explosives.
- 4 is the hollow coneshaped rear rudder or tail and 5 are the steering-surfaces of which three are provided as illustrated. The drawing shows that the transition of the arched surface of the explosive chamber 1 to the cone-shaped surface 4 of the steering-tail is effected with out any break in the outline or a shoulder, so
- scent can flow along the wall of the tail 4 between the steering-surfaces 5 without resistance.
- the projectile according to Fig. 3 differs ,from the one shown in Figs. 1 and 2 in that the explosive chamber is composed of two separate chambers 6, 7 each of cup shape and connected with each other in proximity of the largest diameter of the projectile.
- the fuse forming the point of the projectile has again been marked 2.
- the cap 3 of the explosive chamber has been omitted and charging has to be effected from the point end of the projectile.
- the steering-tail 4 has again been fastened to the explosive chamber 6 without any break or shoulder.
- the explosive chamber is like in Fig. 3 composed of two cup-shaped sections 6, 7 placed opposite each other with their widest opening, the cup-part 6 being however open at its bottom end and closed by a separate bottom cap 8.
- FIG. 5 and 6 corresponds to the one of Fig. 4 with the exception of a special arrangement for fitting the steering-tail 4 upon the bottom cap 8 of the explosive chamber 6, 7.
- the bottom cap 8 is as illustrated by the enlarged scale drawing of Fig. 6 provided with a tapered recess 9 into which material of the sheetmetal part 4 has been pressed.
- Fig. 7 shows one way of constructing the drop pro ectile especially adapted for heavy mines.
- the explosive chamber consists in this case of a strong walled forward section 11, which again receives the fuse 2 at its pomt and extends to the rear into a conslderably thinner sheet-metal casing 12 closed by a bottom cap 13.
- This bottom cap carries the thin sheet-metal steeringtail 4 with the steering-surfaces 5.
- the combination of the explosive chamber of one strong walled resistible head-piece 11 and one considerably thinner part 12 corresponds to the purpose and strain of a mine shell supposed to contain as much explosive as possible and at the same time capable of entering a resisting target.
- Figs. 1-7 do not show special means for connecting the steering-cone with the steering-surfaces 5. How this connection may effectively be performed has been illustrated in Figs. 8-11.
- the steeringsurfaces are made in screw shape, the joints running likewise out upon the casing surface of the steering tail in screw lines.
- the difiiculty of shaping and retaining the shape during transport and descent has been overcome thereby, that the hollow coneshaped steering-tail of sheet-metal is composed of several separate parts 14-according to the showing of the drawing three in number-the edges running out in screw shape and are bent out of the cone-surface. These bent out surfaces form a safe support for the steering-surfaces.
- both edges of the steering-tail sec tions are bent out of the cone surface and one edge is so far broadened, that it forms a steering surface in itself.
- the steering-surfaces formed by one edge of the sections 14 of the steering-tail are marked 15, the edges of the sections 14 contacting therewith are marked 16.
- the steering-surfaces accordings to Figs. 10 and 11 are shaped substantially level.
- the effect of screw-surfaces is in this case obtained thereby that the sheet-metal plates forming the steering-sur faces are thus inclined toward each other in their part 17 protruding beyond the rear end of the steering-tail 4 and arranged in respect to the axis of the cone 4 that their joiningedges 18 form the edges of a pyramid. (According to the drawing a three cornered pyramid.)
- edges 19 of the steering-surfaces together with the cone-surfaces of the steering-tail 4 run out parallel to the cone axis.
- T he steering-surfaces with'their level sections 17 act in this case mainly as screw-surfaces, while the arched surfaces between the lines 20 and 19 do not participate in the screw effect.
- the steering-surfaces can be bent over at of the steering-surfaces commencing the outer corners of the level sections 17, viz. at the point 21 in the sense of an increasing pitch of the screw-surface.
- a drop projectile comprising a strong walled explosive chamber and a hollow coneshaped steering tail of sheet metal, these elements forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
- a drop projectile comprising a strong walled explosive chamber decreasing in diameter towards both its ends and a hollow cone-shaped steering tail of sheet metal, these elements forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
- a drop projectile comprising a three part strong walled explosive chamber, the two end portions of which are in the form of hollow caps and a hollow cone-shaped steering tail of sheet metal mounted on the rear cap of the explosive chamber the explosive chamber with the steering tail forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
- a drop projectile having a lancet shaped longitudinal section comprising a strong walled explosive chamber, and a hollow cone-shaped steering tail of sheet metal forming the pointed rear end of the lancetshaped body, the steering tail being fixed to the explosive chamber by metal of the steering tail being pressed into suitable recesses within the wall of the explosive chamber.
- a drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail forming the pointed .rear end of the lancet-shaped body provided with steering surfaces consisting of sheet metal strips the joint edges of which running in screw lines on the tail surface.
- a drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail provided with steering surfaces, the steering tail composed of several sections with screw shaped running joining edges bent out from the cone-shaped surface of the steering tail, said bent out edges forming abutments for the steering surfaces provided on the steering tail.
- a drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail, the steering tail composed of several sections with screw shaped joining edges bent out from the cone-shaped surface of the steering tail, pairs of joining edges comprising one edge of width sufficient to make such edge itself a steering surface.
- a drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail provided with sheet metal steering surfaces protruding over the rear end of the hollow steering-tail, the portions of the steering surfaces protruding over the end of the steering-tail being so positioned with relation to each other and connected with each other that the con nected portions form a steering-tail rein forcing pyramid.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Toys (AREA)
Description
H. JACOB OBLONG DROP PROJECTILE Filed Aug. 30, 1921 2 Sheets-Sheet 1 lnvmiur: A M gf l? Dec, 23, 1924!.
H. JACOB OBLONG DROP PROJECTILL Filed Aug. 50, 1921 2 Sheets-Sheet 2 Fig :10.
' specification.
Patented Dec. 1924.
HEINRICH JACOB, OF FRIEDENAU, GERMANY, ASSIGNOR T0 F 2:.
ANSTALT C. P. GOEBZ ATKIENGESEL OBLONG DROP PBOJECTILE.
application filed August 30, 1921. Serial No. 496,953.
(GRANTED UNDER T PROVISIONS OF THE ACT OF MARCH 3, 1921, 41
To allwhom it may concern:
Be it known that I, HEINRICH JACOB, a citizen of the German Republic, and resident of F riedenau, near Berlin, Germany, have invented certain new and useful Improvements in and Relating to Oblong Drop Projectiles, of 'which the following is a The present invention relates to the construction of ion shaped drop projectiles and has for its 0 ject to ensure stability of the projectile in its trajectory and at the same time best utilization of the material,
easy production and protection of the lightly constructed steering elements against destructive influences of arising centrifugalforces. i
For these purposes the projectile is given a lancet-shaped longitudinal section, the steering-tail being formed by a hollow coneshaped sheet-metal shell. This construction allows concentration of the main part of the mass of the projectile within the body of the projectile without accumulation of dead material, while the air-resistance centre is located as far as possible back within the range of the light sheet-metal steering shell. Other features of the invention will a pear from the following specification, wit reference to the drawings.
Figs. 1 and 2 illustrate the principles of construction and shape of the projectile in longitudinal section and a plan view thereto.
Figs. 3 and 4 are longitudinal sections of two different constructlons of the projec from the steering-surfaces a lancet-shaped' longitudinal section in which any protruding edge and any break in the curve of STAT. I, 1318.)
the outer demarcation lines has been avoided carefully contrary to hitherto known con- *means simultaneously shifted far away from the centre of gravity of the projectile, thus producing favorable stabilizing conditions in the air during descent.
In order that the dropping projectile may develop a rotarf; velocity in its descent sufficient to release a centrifugal safety device for its fuse, it is necessa to impart to the steering-surfaces attache to the steeringtail a screw-shaped twist. Such steering surfaces can easily be made by constructing the hollow cone-shaped sheet-metal rear rudder of several parts, ,the edges of which are bent out of the cone-surfaces so that they form by themselves steering-surfaces upon the cone. The bordered edges can particularl be so shaped, that they form steeringsu aces for the projectile.
Arched steering surfaces made of thin sheet metal can only with difliculty be so constructed and connected :that they are adapted to. resist to the air pressure and to centrifugal forces without undergoing deformation. These diificulties can considerably be reduced by making the steering-surfaces out of sheet-metal strips, level at the rear end projecting beyond the cone-shaped steering-tail and arranged oblique to each other and the cone axis thus that their joints form the outline of a pyramid, while those of the cone surfaces of the steering tail run parallel to the axis and whereby the transition from the level part of the steering-surfaces to the edge of the joint on the steering tail is eifected by a corresponding arching of such surfaces.
In the construction according to Figs. 1 and 2 of the drawings, 1 designates the strong-walled chamber for the explosive. This explosive chamber is .at its forward end provided with a ,fuse which on the drawing is only diagrammatically illustrated and designated with the numeral 2 and at its rear end with a cap for charging the projectile with explosives. 4 is the hollow coneshaped rear rudder or tail and 5 are the steering-surfaces of which three are provided as illustrated. The drawing shows that the transition of the arched surface of the explosive chamber 1 to the cone-shaped surface 4 of the steering-tail is effected with out any break in the outline or a shoulder, so
that the air passing the body 1 during de-.
scent can flow along the wall of the tail 4 between the steering-surfaces 5 without resistance.
The projectile according to Fig. 3 differs ,from the one shown in Figs. 1 and 2 in that the explosive chamber is composed of two separate chambers 6, 7 each of cup shape and connected with each other in proximity of the largest diameter of the projectile.
The fuse forming the point of the projectile has again been marked 2. In this construction the cap 3 of the explosive chamber has been omitted and charging has to be effected from the point end of the projectile. The steering-tail 4 has again been fastened to the explosive chamber 6 without any break or shoulder.
According to the illustration of Fig. 4 the explosive chamber is like in Fig. 3 composed of two cup- shaped sections 6, 7 placed opposite each other with their widest opening, the cup-part 6 being however open at its bottom end and closed by a separate bottom cap 8.
This development of the rear end of the explosive chamber facilitates'assembling of the steering-tail and enables inserting of a smoke-set very important for shooting practice especially for exercising purposes. The construction according to Figs. 5 and 6 corresponds to the one of Fig. 4 with the exception of a special arrangement for fitting the steering-tail 4 upon the bottom cap 8 of the explosive chamber 6, 7. The bottom cap 8 is as illustrated by the enlarged scale drawing of Fig. 6 provided with a tapered recess 9 into which material of the sheetmetal part 4 has been pressed.
According to the illustration, displacement from the recessis prevented by screws or rivets 10, but both are not indispensable for this mode of fastening.
Fig. 7 shows one way of constructing the drop pro ectile especially adapted for heavy mines. The explosive chamber consists in this case of a strong walled forward section 11, which again receives the fuse 2 at its pomt and extends to the rear into a conslderably thinner sheet-metal casing 12 closed by a bottom cap 13. This bottom cap carries the thin sheet-metal steeringtail 4 with the steering-surfaces 5.
The combination of the explosive chamber of one strong walled resistible head-piece 11 and one considerably thinner part 12 corresponds to the purpose and strain of a mine shell supposed to contain as much explosive as possible and at the same time capable of entering a resisting target.
Figs. 1-7 do not show special means for connecting the steering-cone with the steering-surfaces 5. How this connection may effectively be performed has been illustrated in Figs. 8-11.
According to Figs. 8 and 9 the steeringsurfaces are made in screw shape, the joints running likewise out upon the casing surface of the steering tail in screw lines. The difiiculty of shaping and retaining the shape during transport and descent has been overcome thereby, that the hollow coneshaped steering-tail of sheet-metal is composed of several separate parts 14-according to the showing of the drawing three in number-the edges running out in screw shape and are bent out of the cone-surface. These bent out surfaces form a safe support for the steering-surfaces. According to the drawing both edges of the steering-tail sec tions are bent out of the cone surface and one edge is so far broadened, that it forms a steering surface in itself. The steering-surfaces formed by one edge of the sections 14 of the steering-tail are marked 15, the edges of the sections 14 contacting therewith are marked 16.
Differing from the construction according to Figs. 8 and 9, the steering-surfaces accordings to Figs. 10 and 11 are shaped substantially level. The effect of screw-surfaces is in this case obtained thereby that the sheet-metal plates forming the steering-sur faces are thus inclined toward each other in their part 17 protruding beyond the rear end of the steering-tail 4 and arranged in respect to the axis of the cone 4 that their joiningedges 18 form the edges of a pyramid. (According to the drawing a three cornered pyramid.)
.The edges 19 of the steering-surfaces together with the cone-surfaces of the steering-tail 4 run out parallel to the cone axis.'
The transition of the level section 17 of the steering-surfaces into the edges 19 of the cone-surface of the steering-tail 4 is obtained by corresponding archin ab ut at the line 20 and continuing gradually towards the edge 19.
T he steering-surfaces with'their level sections 17 act in this case mainly as screw-surfaces, while the arched surfaces between the lines 20 and 19 do not participate in the screw effect.
The steering-surfaces can be bent over at of the steering-surfaces commencing the outer corners of the level sections 17, viz. at the point 21 in the sense of an increasing pitch of the screw-surface.
What I claim is:
1. A drop projectile comprising a strong walled explosive chamber and a hollow coneshaped steering tail of sheet metal, these elements forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
2-. A drop projectile comprising a strong walled explosive chamber decreasing in diameter towards both its ends and a hollow cone-shaped steering tail of sheet metal, these elements forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
3. A drop projectile comprising a three part strong walled explosive chamber, the two end portions of which are in the form of hollow caps and a hollow cone-shaped steering tail of sheet metal mounted on the rear cap of the explosive chamber the explosive chamber with the steering tail forming together a lancet shaped body with a substantially smooth outer surface having a pointed rear end.
4. A drop projectile having a lancet shaped longitudinal section comprising a strong walled explosive chamber, and a hollow cone-shaped steering tail of sheet metal forming the pointed rear end of the lancetshaped body, the steering tail being fixed to the explosive chamber by metal of the steering tail being pressed into suitable recesses within the wall of the explosive chamber.
5. A drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail forming the pointed .rear end of the lancet-shaped body provided with steering surfaces consisting of sheet metal strips the joint edges of which running in screw lines on the tail surface.
6. A drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail provided with steering surfaces, the steering tail composed of several sections with screw shaped running joining edges bent out from the cone-shaped surface of the steering tail, said bent out edges forming abutments for the steering surfaces provided on the steering tail.
7. A drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail, the steering tail composed of several sections with screw shaped joining edges bent out from the cone-shaped surface of the steering tail, pairs of joining edges comprising one edge of width sufficient to make such edge itself a steering surface.
8. A drop projectile of lancet shaped longitudinal section comprising a strong walled explosion chamber and a hollow coneshaped steering tail provided with sheet metal steering surfaces protruding over the rear end of the hollow steering-tail, the portions of the steering surfaces protruding over the end of the steering-tail being so positioned with relation to each other and connected with each other that the con nected portions form a steering-tail rein forcing pyramid.
In testimony whereof I have signed this specification in the presence of two subscribing witnesses.
HEINRICH JACOB. Witnesses:
HERMAN REISING J ULEs HUMBRECHT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US496953A US1520131A (en) | 1921-08-30 | 1921-08-30 | Oblong drop projectile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US496953A US1520131A (en) | 1921-08-30 | 1921-08-30 | Oblong drop projectile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1520131A true US1520131A (en) | 1924-12-23 |
Family
ID=23974865
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US496953A Expired - Lifetime US1520131A (en) | 1921-08-30 | 1921-08-30 | Oblong drop projectile |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1520131A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2725233A (en) * | 1951-02-24 | 1955-11-29 | Gen Motors Corp | Finned tail-piece |
| US2922365A (en) * | 1955-11-28 | 1960-01-26 | Cook Electric Co | Aerial missile |
| WO1986006828A1 (en) * | 1985-05-11 | 1986-11-20 | Rheinmetall Gmbh | Undercalibrated projectile |
| US5807198A (en) * | 1997-02-27 | 1998-09-15 | Oddzon Products, Inc. | Tossable game-ball device |
| US5833897A (en) * | 1997-02-27 | 1998-11-10 | Oddzon Products, Inc. | Method of forming tossable device including game-ball unit |
| US6010419A (en) * | 1997-09-10 | 2000-01-04 | Oddzon, Inc, | Throwing toy with non-spinning tail |
| US6042494A (en) * | 1997-09-10 | 2000-03-28 | Rappaport; Mark J. | Throwing toy with retractable tail |
| US6220918B1 (en) | 1998-06-12 | 2001-04-24 | Oddzon, Inc. | Tossable ring airfoil projectile |
-
1921
- 1921-08-30 US US496953A patent/US1520131A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2725233A (en) * | 1951-02-24 | 1955-11-29 | Gen Motors Corp | Finned tail-piece |
| US2922365A (en) * | 1955-11-28 | 1960-01-26 | Cook Electric Co | Aerial missile |
| WO1986006828A1 (en) * | 1985-05-11 | 1986-11-20 | Rheinmetall Gmbh | Undercalibrated projectile |
| US4730561A (en) * | 1985-05-11 | 1988-03-15 | Rheinmetall Gmbh | Subcaliber projectile |
| US5807198A (en) * | 1997-02-27 | 1998-09-15 | Oddzon Products, Inc. | Tossable game-ball device |
| US5833897A (en) * | 1997-02-27 | 1998-11-10 | Oddzon Products, Inc. | Method of forming tossable device including game-ball unit |
| US6010419A (en) * | 1997-09-10 | 2000-01-04 | Oddzon, Inc, | Throwing toy with non-spinning tail |
| US6042494A (en) * | 1997-09-10 | 2000-03-28 | Rappaport; Mark J. | Throwing toy with retractable tail |
| US6220918B1 (en) | 1998-06-12 | 2001-04-24 | Oddzon, Inc. | Tossable ring airfoil projectile |
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