US2265697A - Ammunition shell - Google Patents
Ammunition shell Download PDFInfo
- Publication number
- US2265697A US2265697A US339112A US33911240A US2265697A US 2265697 A US2265697 A US 2265697A US 339112 A US339112 A US 339112A US 33911240 A US33911240 A US 33911240A US 2265697 A US2265697 A US 2265697A
- Authority
- US
- United States
- Prior art keywords
- shell
- airplane
- parachute
- ammunition shell
- ammunition
- 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
- 239000002360 explosive Substances 0.000 description 3
- 238000004880 explosion Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000009527 percussion Methods 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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type
Definitions
- Our invention refers to explosive shells, and it is particularly adapted as a defense against airplane raids.
- the invention has for its primary object to provide an ammunition shell unit, which may develop a secondary explosion due to striking an airplane or other object, whereby the body of the shell will grapple or engage the object struck and simultaneously discharge a parachute, which is connected'to the shell by a suitable cable, thus putting out of commission the airplane or object struck.
- the invention consists in certain peculiarities of construction and arrangement of parts, as will be hereinafter fully set forth in connecranged to be otherwise movable, whereby it is discharged through the rear end of the jacket.
- a piston-head is loosely mounted near the front end of the jacket, and has attached thereto a coiled cable 8, which cable is also attached to the leaders I of a parachute 8; the same is shown snugly folded within the shell with its crowned end abutting the disc 3.
- a fixed disc 5 Spaced from thepiston-head 5 is a fixed disc 5, which disc carries a percussion cap it, and
- a spring-controlled plunger rod I2 is reciprocatedly mounted in the nose of the shell, and has projecting from said nose a tappet finger l3.
- the rear end of the plunger rod carries a hammer id, adapted to contact and explode the auxiliary charge ii.
- the hammer it is also provided with fingers it, which engage springcontrolled trip arms l6 and pivot grapple hooks II, the said grapple hooks being exterior of and normally closed against the shell I.
- a shell comprising, a jacket, a plunger extend-
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Automotive Seat Belt Assembly (AREA)
Description
DEC. 9, G NEU A N ET AL 2,265,697
AMMUNITION SHELL Filed June 6, 1940 lnventmra FranK Eur-Imelda! George Neurnann and atented fies. 9, 1941 AMMUNITION SHELL George Neufialnn and Frank Schneider,
wankee, Wis.
Application June 6, 1940, Serial No. 339,112-
ICIaim.
Our invention refers to explosive shells, and it is particularly adapted as a defense against airplane raids.
The invention has for its primary object to provide an ammunition shell unit, which may develop a secondary explosion due to striking an airplane or other object, whereby the body of the shell will grapple or engage the object struck and simultaneously discharge a parachute, which is connected'to the shell by a suitable cable, thus putting out of commission the airplane or object struck.
With the above and other minor objects in view, the invention consists in certain peculiarities of construction and arrangement of parts, as will be hereinafter fully set forth in connecranged to be otherwise movable, whereby it is discharged through the rear end of the jacket.
A piston-head is loosely mounted near the front end of the jacket, and has attached thereto a coiled cable 8, which cable is also attached to the leaders I of a parachute 8; the same is shown snugly folded within the shell with its crowned end abutting the disc 3.
Spaced from thepiston-head 5 is a fixed disc 5, which disc carries a percussion cap it, and
between the fixed disc and piston-head is an auxiliary explosive charge II.
A spring-controlled plunger rod I2 is reciprocatedly mounted in the nose of the shell, and has projecting from said nose a tappet finger l3. The rear end of the plunger rod carries a hammer id, adapted to contact and explode the auxiliary charge ii. The hammer it is also provided with fingers it, which engage springcontrolled trip arms l6 and pivot grapple hooks II, the said grapple hooks being exterior of and normally closed against the shell I.
From the foregoing description, it will be noted that when the tappet finger l3 engages, for example, the body 01 an airplane, it will produce a hammer blow upon the cap of the auxiliary charge ll. This explosion of the charge will cause the piston-head to travel rearwardly in the jacket and strip the parachute and associated parts from the shell i.
As shown in Figure 2, in the event that the shell pierces a wing of an airplane, the grapple hooks ll, being expanded or spread out due to action of the hammer blow, will contact with the surfaces of the wing, and, thus, securely lockthe shell into anchor engagement with said wing. Hence, the parachute will ofler a substantial resistance or anchorage element with reference to the airplane, and said plane will be twisted from its course, or checked in speed to such an extent as to put the plane out of action. It will be observed, however, that this same result with reference to the shell and associated parachute will be had in the event that the shell strikes any portion of the plane.
Furthermore, in some instances, we may utilize a time-controlled explosive element associated with the auxiliary charge, whereby the shell may be discharged and function at a pre-determined distance from its point of travel; and, consequently, when so exploded, the cable and parachute will readily entangle a moving object, such as an airplane.
While we have shown and described a shell embodying our invention minutely as to details, it is understood that we may vary the structural features of the shell indefinitely within the scope of the claim to accomplish the desired results.
We claim:
A shell comprising, a jacket, a plunger extend-
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US339112A US2265697A (en) | 1940-06-06 | 1940-06-06 | Ammunition shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US339112A US2265697A (en) | 1940-06-06 | 1940-06-06 | Ammunition shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2265697A true US2265697A (en) | 1941-12-09 |
Family
ID=23327549
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US339112A Expired - Lifetime US2265697A (en) | 1940-06-06 | 1940-06-06 | Ammunition shell |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2265697A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3103889A (en) * | 1961-01-31 | 1963-09-17 | Sr Edward W Keeney | Fragmentation bullet |
| US3859598A (en) * | 1969-04-09 | 1975-01-07 | Texas Instruments Inc | Aerial drop penetration device |
| US20100173734A1 (en) * | 2009-01-07 | 2010-07-08 | Greg Robbins | Concealed Broad Head Arrow Tip and Associated Methods |
| US10408588B1 (en) * | 2017-12-21 | 2019-09-10 | The United States Of America As Represented By The Secretary Of The Army | Over penetration inhibiting and retaining mechanism |
-
1940
- 1940-06-06 US US339112A patent/US2265697A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3103889A (en) * | 1961-01-31 | 1963-09-17 | Sr Edward W Keeney | Fragmentation bullet |
| US3859598A (en) * | 1969-04-09 | 1975-01-07 | Texas Instruments Inc | Aerial drop penetration device |
| US20100173734A1 (en) * | 2009-01-07 | 2010-07-08 | Greg Robbins | Concealed Broad Head Arrow Tip and Associated Methods |
| US10408588B1 (en) * | 2017-12-21 | 2019-09-10 | The United States Of America As Represented By The Secretary Of The Army | Over penetration inhibiting and retaining mechanism |
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