[go: up one dir, main page]

US1299744A - War-balloon. - Google Patents

War-balloon. Download PDF

Info

Publication number
US1299744A
US1299744A US23014218A US23014218A US1299744A US 1299744 A US1299744 A US 1299744A US 23014218 A US23014218 A US 23014218A US 23014218 A US23014218 A US 23014218A US 1299744 A US1299744 A US 1299744A
Authority
US
United States
Prior art keywords
bomb
balloon
war
fuse
chamber
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
US23014218A
Inventor
George Lotysiewicz
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 US23014218A priority Critical patent/US1299744A/en
Application granted granted Critical
Publication of US1299744A publication Critical patent/US1299744A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/56Range-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

  • This invention relates to improvements 1n bomb carrying structures of the balloon type and has as its special object the provlsion of means whereby a carried bomb may be the accompanying drawings, forming a material part of this disclosure, and in which Figure 1 is a side elevational view of the invention and indicating its operation, and
  • Fig. 2 is a vertical sectional view drawn to an enlarged scale of the disruptable chamber, the section being taken on line 2--2 of Fig. 1.
  • the numeral 10 designates a gas filled sac such as is commonly used in lighter than air devices'of the balloon type, and which may be inflated by the usual means with hydrogen or like gases, materially lighter than ordinary air.
  • a nettin 11 Surrounding the sac is a nettin 11, terminating in a ring 12, all of the oregoing parts being of the usual type of construction.
  • cords 14 attached to eyes 15, aiixed in the upper head 16, of a hollow cylindrical chamber 18, preferably made of combustible material, and provided with a lower head 19. Secured centrally in the lower head by means of a bolt 20, held in position by a nut 21,'and having an eye 22, in a depending hook 23, by means of which the bomb 25, is suspended centrally of the balloon as can best be seen in Fig. 1.
  • the bomb 25 is provided with laterally extending elements 26 which act as detonators, as does also the spur shaped element 27, pending centrally downward, so that ⁇ whenever the elements 26 or 27,- come into forcible contact with a fixed object the charge within the bomb is caused to be explOded.
  • an internal annular band 30 Arranged within the cylindrical combustible chamber 18, is an internal annular band 30, having a circular cross section and adapted to contain a charge of powder 31, the band being held in place by clips 32, and having engaged with it ya fuse 33, which will burn at a known rate of speed so that the length of the fuse regulates the time of explosion of the powder charge within the band 30, and hence the disruption of the cylinder 18, permitting the bomb 25 to drop.
  • the sac 10 having been in- Hated and the powder filled ring 28 being in position in the cylindrical chamber 18, a bomb may be readily engaged with the hook element 23, and the distance calculated from the point of release to the point where the bomb is to be discharged, the length of the fuse 33 corresponding to the time estimated it will take for the iiight of the balloon in a well known manner, and it will be clearly understood that when the spark within the fuse 33, reaches the powder charge 31, the cylinder 18 becomes disrupted, permitting the bomb to drop by gravity and upon striking the surface of the earth will explode by its contact.
  • an aerial bomb carrying device the combination with a balloon and a bomb carried thereby, of a chamber intervening between said balloon and said bomb, a hollow band supported centrally in said chamber, said hollow band carrying a powder charge adapted to disrupt said cylinder, and a time fuse engaged with said hollow band.
  • an aerial bomb carrier the combination with a balloon and an explosive bomb pendant therefrom, of a disruptable cylin der xed in the connections between said bomb and said balloon, a hollow annular element arranged centrally within said disruptable cylinder, said element carrying a powder charge, means for supporting said annular element therewithin, and a time fuse for conducting a spark to the powder charge whereby theV supporting connection of said bomb is disrupted.

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)

Description

G. LOTYSIEWICZ.
WAR BALLooN.
ION F APPLC 2,1918 y 1 ,299,744. Patented Apr. 8,1919.
3, www
mmnzw i my mw y' www A non/VHS' GEORGE LOTYSIEWICZ, OF IBBOOKING, SASKATCHEWAN, CANADA.
WABPBALLOON.
Specication of Letters Patent.
Patented. Anas, Taio.
Application led April 22, 1918. Serial No. 230,142.
To all whom t may concern Be it known that I, GEORGE Lorrrsrwrcz, a citizen of Poland, resident of Brooking, Province olf Saskatchewan, Dominion of Canada, have invented certainv new and useful Improvements in Vilar-Balloons, of which the following is a specification.
This invention relates to improvements 1n bomb carrying structures of the balloon type and has as its special object the provlsion of means whereby a carried bomb may be the accompanying drawings, forming a material part of this disclosure, and in which Figure 1 is a side elevational view of the invention and indicating its operation, and
Fig. 2 is a vertical sectional view drawn to an enlarged scale of the disruptable chamber, the section being taken on line 2--2 of Fig. 1.
In the drawing the numeral 10, designates a gas filled sac such as is commonly used in lighter than air devices'of the balloon type, and which may be inflated by the usual means with hydrogen or like gases, materially lighter than ordinary air.
Surrounding the sac is a nettin 11, terminating in a ring 12, all of the oregoing parts being of the usual type of construction.
Engaged with the ring 12 are cords 14, attached to eyes 15, aiixed in the upper head 16, of a hollow cylindrical chamber 18, preferably made of combustible material, and provided with a lower head 19. Secured centrally in the lower head by means of a bolt 20, held in position by a nut 21,'and having an eye 22, in a depending hook 23, by means of which the bomb 25, is suspended centrally of the balloon as can best be seen in Fig. 1.
The bomb 25 is provided with laterally extending elements 26 which act as detonators, as does also the spur shaped element 27, pending centrally downward, so that` whenever the elements 26 or 27,- come into forcible contact with a fixed object the charge within the bomb is caused to be explOded.
Arranged within the cylindrical combustible chamber 18, is an internal annular band 30, having a circular cross section and adapted to contain a charge of powder 31, the band being held in place by clips 32, and having engaged with it ya fuse 33, which will burn at a known rate of speed so that the length of the fuse regulates the time of explosion of the powder charge within the band 30, and hence the disruption of the cylinder 18, permitting the bomb 25 to drop.
In operation, the sac 10, having been in- Hated and the powder filled ring 28 being in position in the cylindrical chamber 18, a bomb may be readily engaged with the hook element 23, and the distance calculated from the point of release to the point where the bomb is to be discharged, the length of the fuse 33 corresponding to the time estimated it will take for the iiight of the balloon in a well known manner, and it will be clearly understood that when the spark within the fuse 33, reaches the powder charge 31, the cylinder 18 becomes disrupted, permitting the bomb to drop by gravity and upon striking the surface of the earth will explode by its contact.
I claim:
1. In an aerial bomb carrying device, the combination with a balloon and a bomb carried thereby, of a chamber intervening between said balloon and said bomb, a hollow band supported centrally in said chamber, said hollow band carrying a powder charge adapted to disrupt said cylinder, and a time fuse engaged with said hollow band.
.2. In an aerial bomb carrier, the combination with a balloon and an explosive bomb pendant therefrom, of a disruptable cylin der xed in the connections between said bomb and said balloon, a hollow annular element arranged centrally within said disruptable cylinder, said element carrying a powder charge, means for supporting said annular element therewithin, and a time fuse for conducting a spark to the powder charge whereby theV supporting connection of said bomb is disrupted.
In testimony whereof I have aixed my signature.
GEORGE LOTYSIEWICZ.
US23014218A 1918-04-22 1918-04-22 War-balloon. Expired - Lifetime US1299744A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US23014218A US1299744A (en) 1918-04-22 1918-04-22 War-balloon.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US23014218A US1299744A (en) 1918-04-22 1918-04-22 War-balloon.

Publications (1)

Publication Number Publication Date
US1299744A true US1299744A (en) 1919-04-08

Family

ID=3367286

Family Applications (1)

Application Number Title Priority Date Filing Date
US23014218A Expired - Lifetime US1299744A (en) 1918-04-22 1918-04-22 War-balloon.

Country Status (1)

Country Link
US (1) US1299744A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416877A (en) * 1940-06-10 1947-03-04 Laughlin Myron Penn Aerial mine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416877A (en) * 1940-06-10 1947-03-04 Laughlin Myron Penn Aerial mine

Similar Documents

Publication Publication Date Title
US1300333A (en) Explosive shell.
US1150667A (en) Shell or projectile.
US1299744A (en) War-balloon.
US1175800A (en) Incendiary projectile.
US1289483A (en) Aerial bomb.
US1311785A (en) Aerial torpedo or mine
US1329443A (en) Bomb
US1361286A (en) Aerial torpedo
US1317610A (en) Booster construction for explosive devices
US910942A (en) Explosive mine or projectile.
US1276547A (en) Flying-bomb.
CN212362987U (en) A rocket load restraint release and separation mechanism
US1297273A (en) Aerial torpedo or mine.
US1317608A (en) Lester i
US1343036A (en) Aerial bomb
US1272759A (en) Hand-grenade.
US957210A (en) Rocket.
US1284148A (en) Magazine-projectile.
US2335927A (en) Aerial bomb
US333552A (en) Bomb-lance
US1270072A (en) Explosive bomb.
US1292408A (en) Bomb.
US1317609A (en) Detonator
US1242053A (en) Hand-grenade.
US2654321A (en) Projectile method and means