US2051927A - Discharger for pyrotechnic cartridges - Google Patents

Discharger for pyrotechnic cartridges Download PDF

Info

Publication number
US2051927A
US2051927A US714939A US71493934A US2051927A US 2051927 A US2051927 A US 2051927A US 714939 A US714939 A US 714939A US 71493934 A US71493934 A US 71493934A US 2051927 A US2051927 A US 2051927A
Authority
US
United States
Prior art keywords
barrel
discharger
plate
back plate
detent
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
Application number
US714939A
Inventor
Wiley Samuel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US714939A priority Critical patent/US2051927A/en
Application granted granted Critical
Publication of US2051927A publication Critical patent/US2051927A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
    • F41F1/06Mortars

Definitions

  • This invention relates to a discharger for pyrotechnic cartridges.
  • the principal object of the invention is to provide a discharger which is capable of firing a large cartridge carrying a heavy propellant charge and which may be conveniently mounted on the side wall of aircraft.
  • FIG. 1 is a view in rear elevation and partly in section of the improved discharger.
  • Fig. 2 is a view in side elevation.
  • Fig. 3 is a sectional view on the line 3--3 of Fig. 1.
  • Fig. 4 is a fragmentary view in side elevation showing the barrel in firing position.
  • Fig. 5 is a longitudinal sectional view of the barrel with a firing pin in retracted position.
  • Fig. 9 is a view in side elevation of the wall of the aircraft.
  • Fig. 10 is a plan view of the discharger of Fig. 8.
  • the discharger comprises a barrel 5 having its rear end closed by a breech 8 wihch is attached to the barrel by the threaded connection I.
  • the breech 6 is formed with a conical projection 8 for centering a cartridge (not shown) carrying its own propelling charge.
  • a reduced stem 9 on the breech and coaxial with the barrel houses a firing pin I whose point II is adapted to pass through an aperture [2 in the conical projection 8.
  • a lever l3 pivotally mounted on a pin 14 carried by ears l-l5 on the stem extends through an aperture IS in the stem and has its inner end disposed in a slot I! in the firing pin.
  • a lanyard I8 is attached to the outer end of the lever and serves to rotate the lever and drive the firing pin forward.
  • the extremity of the stem 9 is provided with a pair of trunnions
  • a frame for mounting the barrel consists of a bottom plate 20, side plates 2l-2l and relatively short front and back plates respectively 22 and 23.
  • the side plates are formed with opposite guideways or channels 24-24 on their inner faces.
  • the channels are open at the upper edge of the side plates and are closed adjacent the bottom plate. This arrangement provides for entry of the trunnions l9 between the plates and the closed ends constitute bearings or seats for the trunnions as clearly shown in Fig. 1.
  • One of the trunnions is provided with a wheel or annular head 25 positioned between the side plates and having peripheral notches or recesses 26 for receiving a beveled lug 21 on a detent 28.
  • the detent is pivotally mounted on a pin 29 carried by ears 3U--3ll fast on the back plate 23.
  • acting on the detent normally moves it towards the back plate and causes the lug 21 to project through an aperture 32 in the back plate and into one of the recesses 26.
  • the wall 33 may be the body of an aircraft.
  • the wall is provided with an opening 35 through which the barrel may be moved as shown in Fig. 8.
  • the opening is normally closed by a panel 36 mounted on spring-actuated hinges 31.
  • the barrel is then tilted either outwardly or in wardly as indicated in dotted lines '1 apd thecartridge falls out of the barrel.
  • the lug -21 on the" detent reengages' in one og the 'regesses 23 holds the barrelin place.
  • discharger is illustrated as mounted on a wall 33 it is to be understood that it may I the side plates and extending above the seats of the g'uidewaya'a barrel including a reduced stem be carried by any suitable support. 7
  • abarrel including a reduced stem having trunnions adapted to ride in the guideways and be: supported on the seats thereof, an annular head on one trunnion provided with a series of peripheral recesses, a detent'carried by the back plate andsele'ctively' engageable in the recesses to hold theb'arrel in position or angular adjustment; and the stem oi the barrel engageable with the front or back plate when the' detent is in the end recesses.
  • a' frame including spaced side plates, the'inside face of each plate having a guideway open at the upper edge of the plate and providing a seat adjacent the bottom of the plate, a front plate and a back plate connecting the side plates, a barrel including a reduced stem having trunnions adapted to ride in the guideways and be supported on the seat thereof, an an ul hea o one t unnion.
  • rovi ed wi h a series of peripheral recesses, a detent carried by the back plate and selectively engageable in the recesses to hold the barrel in position of angular adjustment, and the stem of the barrel engage- ;algle with the front or back plate when the detent is the end recesses.
  • a frame including spaced side plates, the e face of each plate having a guideway open at the upper edge of the plate and providing a seat adjacent the bottom of the plate, a trgnt plateand a back plate connecting having-:trunnions' adaptedto ride in the guideways and be supported-on the seats thereof, an annular head'on one trunnion provided with a series of peripheral recesses, a detent carried byJthe back plate; and'sel'ectively engage'able'in therecesses to hold the barrel in position of angular adjust ment.

Description

Aug. 25, 1936. s. WILEY DISCHARGER FOR PYROTECHNIC CARTRIDGES Filed March 10, 1934 2 Sheets-Sheet 1 Inventnr Eamuel Wile 4AL1CIYTLE I I l I ll T I I l l [I- h 1111 l l li--- S. WILEY DISCHARGER FOR PYROTEGHNIC CARTRIDGES Aug. 25, 1936.
Filed March 10, 1934 2 Sheets-Sheet 2 l I l I I I I I I n I .r. 5 FM Ww/E v M w H .1 .A WE m w m 5 Patented Aug. 25, 1936 UNITED STATES PATENT OFFICE msonanenn FOR PYROTECHNIC CARTRIDGES (Granted under the act of March 3. 1883, as amended April 30, 1928; 370 0. G. 757) The invention described herein may; be manufactured and used by or for the Government for governmental purposes, without the payment to me of any royalty thereon.
- This invention relates to a discharger for pyrotechnic cartridges.
The principal object of the invention is to provide a discharger which is capable of firing a large cartridge carrying a heavy propellant charge and which may be conveniently mounted on the side wall of aircraft.
Other objects are to provide a novel means for mounting a barrel in a frame and for locking the barrel in various positions of angular adjustment.
. With the foregoing and other objects in view, the invention resides in the novel arrangement and combination of parts and in the details of construction hereinafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed may be made within the scope of what is claimed without departing from the spirit of the invention;
A practical embodiment of the invention is illustrated in the accompanying drawings, where- Fig. 1 is a view in rear elevation and partly in section of the improved discharger.
Fig. 2 is a view in side elevation.
Fig. 3 is a sectional view on the line 3--3 of Fig. 1.
Fig. 4 is a fragmentary view in side elevation showing the barrel in firing position.
Fig. 5 is a longitudinal sectional view of the barrel with a firing pin in retracted position.
. position.
Fig. 9 is a view in side elevation of the wall of the aircraft.
Fig. 10 is a plan view of the discharger of Fig. 8.
Referring to Figs. 1 to 6 the discharger comprises a barrel 5 having its rear end closed by a breech 8 wihch is attached to the barrel by the threaded connection I. The breech 6 is formed with a conical projection 8 for centering a cartridge (not shown) carrying its own propelling charge.
A reduced stem 9 on the breech and coaxial with the barrel houses a firing pin I whose point II is adapted to pass through an aperture [2 in the conical projection 8. A lever l3 pivotally mounted on a pin 14 carried by ears l-l5 on the stem extends through an aperture IS in the stem and has its inner end disposed in a slot I! in the firing pin. A lanyard I8 is attached to the outer end of the lever and serves to rotate the lever and drive the firing pin forward. The extremity of the stem 9 is provided with a pair of trunnions |9--|9.
A frame for mounting the barrel consists of a bottom plate 20, side plates 2l-2l and relatively short front and back plates respectively 22 and 23. The side plates are formed with opposite guideways or channels 24-24 on their inner faces. The channels are open at the upper edge of the side plates and are closed adjacent the bottom plate. This arrangement provides for entry of the trunnions l9 between the plates and the closed ends constitute bearings or seats for the trunnions as clearly shown in Fig. 1.
One of the trunnions is provided with a wheel or annular head 25 positioned between the side plates and having peripheral notches or recesses 26 for receiving a beveled lug 21 on a detent 28. The detent is pivotally mounted on a pin 29 carried by ears 3U--3ll fast on the back plate 23. A spring 3| acting on the detent normally moves it towards the back plate and causes the lug 21 to project through an aperture 32 in the back plate and into one of the recesses 26.
As shown in Fig. 2 when the lug 21 is engaged in the center recess the barrel is parallel to the frame. When the lug is engaged in the end recesses the stem of the barrel rests on and is additionally supported by the front or back plate as indicated in Figs. 4 and 8.
Referring to Figs. '7 to the discharger is installed on a vertical wall 33 and is supported in any suitable manner, as by the bracket 34. The wall 33, for example, may be the body of an aircraft. The wall is provided with an opening 35 through which the barrel may be moved as shown in Fig. 8. The opening is normally closed by a panel 36 mounted on spring-actuated hinges 31.
When the discharger is not in use it is carried in a vertical position parallel to the wall 33 as seen in Fig. 7. In order to load the discharger from the inside of the aircraft it is moved to the position shown in dotted lines in Fig. 8 and a cartridge is dropped into the muzzle of the barrel. The firing pin it) is in the retracted position due to the action of gravity. The barrel is then pushed through the opening 35 in the wall 33 and locked in the position shown in full lines thebarrel due to a misfire or to a decision not to fire, the barrelis grasped by the hand and pulled upwardly. This action automatically disengages v the detent-J28 and causes the trunnions I9 to -ride upwardly in the channels 24 of the side plates I;
The barrel is then tilted either outwardly or in wardly as indicated in dotted lines '1 apd thecartridge falls out of the barrel. Upon lowers ing the barrel until the trunnions are seated in the bottom of the channels 24 the lug -21 on the" detent reengages' in one og the 'regesses 23 holds the barrelin place.
While the discharger is illustrated as mounted on a wall 33 it is to be understood that it may I the side plates and extending above the seats of the g'uidewaya'a barrel including a reduced stem be carried by any suitable support. 7
-I claim:
'1'. In a discharger; a frameincludingspaced side. plates, the inside face of each plate having a guideway open at the upper edge of the plate and providing a seat adjacent, the bottom of the plate, a front plate andia back plate connecting the side plates and extend-ingabove the seats of the guide- Ways, abarrel including a reduced stem having trunnions adapted to ride in the guideways and be: supported on the seats thereof, an annular head on one trunnion provided with a series of peripheral recesses, a detent'carried by the back plate andsele'ctively' engageable in the recesses to hold theb'arrel in position or angular adjustment; and the stem oi the barrel engageable with the front or back plate when the' detent is in the end recesses.
' 2, In adischarger, a' frame including spaced side plates, the'inside face of each plate having a guideway open at the upper edge of the plate and providing a seat adjacent the bottom of the plate, a front plate and a back plate connecting the side plates, a barrel including a reduced stem having trunnions adapted to ride in the guideways and be supported on the seat thereof, an an ul hea o one t unnion. rovi ed wi h a series of peripheral recesses, a detent carried by the back plate and selectively engageable in the recesses to hold the barrel in position of angular adjustment, and the stem of the barrel engage- ;algle with the front or back plate when the detent is the end recesses.
3. In a discharger, a frame including spaced side plates, the e face of each plate having a guideway open at the upper edge of the plate and providing a seat adjacent the bottom of the plate, a trgnt plateand a back plate connecting having-:trunnions' adaptedto ride in the guideways and be supported-on the seats thereof, an annular head'on one trunnion provided with a series of peripheral recesses, a detent carried byJthe back plate; and'sel'ectively engage'able'in therecesses to hold the barrel in position of angular adjust ment.
4. A support having trunnion seats, barrel holdingmeans oarr-i'edlby the support adjacent the seats a barrel having trunnions engaging the seats when in firing position and held by the holding; means, and vertical trunnion guideways in the support above the seats for receiving the trunnion "W'hen' the barrel is raised mm" engagement with the holding means for the purpose of being tilted an amount greaterthan that perrnitteel by the; holding means,
' SAMUEL WILEY;
US714939A 1934-03-10 1934-03-10 Discharger for pyrotechnic cartridges Expired - Lifetime US2051927A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US714939A US2051927A (en) 1934-03-10 1934-03-10 Discharger for pyrotechnic cartridges

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US714939A US2051927A (en) 1934-03-10 1934-03-10 Discharger for pyrotechnic cartridges

Publications (1)

Publication Number Publication Date
US2051927A true US2051927A (en) 1936-08-25

Family

ID=24872086

Family Applications (1)

Application Number Title Priority Date Filing Date
US714939A Expired - Lifetime US2051927A (en) 1934-03-10 1934-03-10 Discharger for pyrotechnic cartridges

Country Status (1)

Country Link
US (1) US2051927A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2502470A (en) * 1946-08-31 1950-04-04 Martin James Ejecting means for chair stabilizing drogue parachutes
US4709614A (en) * 1985-09-19 1987-12-01 Rheinmetall Gmbh Throwing device for firing incandescent bodies

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2502470A (en) * 1946-08-31 1950-04-04 Martin James Ejecting means for chair stabilizing drogue parachutes
US4709614A (en) * 1985-09-19 1987-12-01 Rheinmetall Gmbh Throwing device for firing incandescent bodies

Similar Documents

Publication Publication Date Title
US2391864A (en) Repeating rocket gun
US3318033A (en) Grenade launching arrangement
US2051927A (en) Discharger for pyrotechnic cartridges
US1850034A (en) Bomb-thrower divisible in two parts adapted to be carried on man's back
US2415153A (en) Mount and spent ammunition retriever for flexibly mounted guns
US2371059A (en) Toy gun
US2466725A (en) Vehicle mounted gun and periscope mounting therefor
US1779770A (en) Collapsible firearm
US1931262A (en) Firearm
US2307009A (en) Discharger for pyrotechnic cartridges
US2066326A (en) Turret gun mount
US1874815A (en) Firearm
US2208475A (en) Pistol, gun, or the like for firing and projecting rockets or projectiles for use in throwing lines
US1948511A (en) Discharger
US1845381A (en) Holder for pyrotechnic cartridges
US2069221A (en) Grenade
US1827031A (en) Mechanical loader for muzzle-loading mortars
US1402407A (en) Gun mounting
US2248970A (en) Firearm
US1483129A (en) Line-throwing gun
US1845242A (en) Bolt operating mechanism for machine guns
US2210538A (en) Machine gun mount
US2230328A (en) Automatic gun
US1713723A (en) Combination mount for machine guns
US1789530A (en) Manually-supported mortar