US1274207A - Balloon construction. - Google Patents
Balloon construction. Download PDFInfo
- Publication number
- US1274207A US1274207A US20553617A US20553617A US1274207A US 1274207 A US1274207 A US 1274207A US 20553617 A US20553617 A US 20553617A US 20553617 A US20553617 A US 20553617A US 1274207 A US1274207 A US 1274207A
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- United States
- Prior art keywords
- parachute
- post
- balloon
- block
- bag
- 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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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
Definitions
- the primary object of the invention is the provision of a balloon adapted for carrying passengers such as soldiers detailed for dropping bombs upon. the enemy, arrangement being made for preserving the lives of 'the occupants in the event of damage to the elevating member.
- a further object of the invention is the provision of a compact' arrangement of parachute carried by a balloon adapted for instant use when the balloonis damaged but occupying only a small space when the parachute is not in use.
- a still further object of the device is to provide a balloon especially adapted for war purposes'in dropping bombs and other explosives, the device being arranged with a Steering means and with a parachute adapted for opening automatically in the event of an accident to the balloon.
- Figure 1 is a side elevation of the device with the parachute in its open arrangement.
- Fig. 2 is a vertical central sectional view thereof with parts broken away.
- Fig. 3 is a view similar to Fig. 2 with the parachute in its inclosed i folded arrangemeit, and portions of ⁇ the device omitted an Fig. 4 is an enlarged transverse sectional view taken upon line IV-IV of Fig. 2.
- my invention broa ly consists in a parachute 10 of umbrella form carried by a balloon 11 of substantially the usual appearance in such a manner as to be completely inclosed when not in use but automatically projected and opened for use when the occasion requires.
- the balloon 11 has an inverted pearshaped gas bag 12 adapted for inflation for causing the device to rise in the air, a basket 13 beingsuspended therefrom by means of a tubular post ⁇ 14 extending through the bag 12 and secured to the top thereof as at 15.
- a telescope or sighting apparatus 16 is mounted in the basket 13 for looking downwardly through the bottom 17 of the basket for assisting the "soldiers operating the balloon to correctly aim the bombs 18 upon the nellpy when dropping the same out of the as et.
- the basket 13 is i also connected with the bag 12 by the usual arrangement of suspending cables 19, and a sail 20 is carried at one side of the balloon for assisting the occupants in steering the device in its movements through the air.
- Upper and lo-wer supporting frames 21 and 22 carry the sail 20, and cords 23 are provided for lifting the sail when found desirable.
- the parachute 10 being in the form lof an umbrella, has a central pole or stick 24 having a cap 25 upon the upper end thereof, and a ring 26 is slidably arranged upon the pole 24 connected to the ribs ofthe parachute 10 by means of bows 27, whereby,r as will be apparent, the parachute may -be opened or closed, by elevating or lowering the ring 26.
- a reduced lower extension 28 is provided for the pole 24 mounted upon a disk or block 29 arranged within the post 14 in the manner of a piston.
- a spring'30 encircles the extension 28 and bars between the ringA 26 and block 29, and a cord 31 is attached to the ring 26 and passes through the post 14 to a suitable winding mechanismarf ranged within the basket 13.' By operating the winding mechanism the cord 31 pulls down on the ring 26, compressing the spring 30 and closing the parachute. It will be un- ⁇ derstood that when so compressed, a releasing of the ring 26 permits the spring 30 to automatically open the parachute 10 unless the same is otherwise restrained.
- a helical spring 32 is arranged within the post 14 being mounted at lts lower end upon an inner shoulder 33 of the post, and bearing at its upper end against the block 29.
- a cord 34 is arranged within the post 14 having its upper end attached to the block 29 and its other end connected to a winding mechanism 35 within the basket 13. It will be seen that when the parachute 10 has been compactly folded by pulling downwardly upon the cord 31, the parachute may be drawn inwardly of the post 14 by ranging the parachute in 'its normal inoperative position within the balloonI bag 12 as illustrated in Fig. 3 of the drawings.
- the parachute l0 is normally inclosed within the post 14, and the bag l2 being lilled with a suitable gas, the balloon will rise to the desired altitude ⁇ :tor viewing the enemy through the telescope 16 and dropping the bombs 18, while the rudder or sail 20 .slightly assists in steering the aircraft.
- the cord 34 may be released for automatically elevating the block 29 and projecting the folded parachute 10 outwardly of the upper end of the post 14, and the cord 31 being then released, the spring 30 automatically opens the parachute 10 in the form of an umbrella ermitting the entire device to gradually falli to the ground without injuring the remainder of the balloon or the contents of the basket 13.
- the primary object is to automatically project the parachute 10 to its operative open position when required inthe event of an accident and which operation has been fully described while it will only be necessary to close the parachute and restore the same within the postI 1d when the balloon is on the ground and at which time the attendants may readily fold the fabric portion of the parachute 'for admitting the same into the post 14 upon pulling inwardly upon the cord 34.
- a serviceable device is provided for use in time of war by means of which observations may be taken at high altitudes as well" as the dropping of missiles upon the enemy, while the safe descent of the operators will be insured by the mechanism provided and which takes up but little room during the aerial operation of the balloon.
- An aircraft comprising a gas bag, a hollow post extending therethrough, a basket carried by the said post beneath the bag,
- a folding parachute normally positionedv within the post and'projecting and opening means for the arachute adapted for control within the bas et.
- a cargo carrier attached to the post, a toldable parachute adapted for normal arrangement wit-hin the post, means adapted for projecting the parachute outwardly of the post, lopening means for the parachute and Controlling members for the said projecting andopening means operable from a point within the cargo carrier.
- a device of the class described coinprising an elevating bag for a balloon, a tubular post positioned ,therethrough attached to the top of the bag, a basket upon the lower end of the post beneath the bag, a block slidably arranged within the post, a mounting spring within the post beneath the block, lowering means for the block and tensioning means for the spring arranged within the basket and a folding parachute mounted upon the pocket and normally positioned within the post adapted for automatic opening when the block is elevated within the est.
- a device of the class described comprising an elevating bag for a balloon, a tubular post positioned therethrough attached to the top of the bag, a basket upon the lower end of the post beneath the bag, a block slidably arranged within the post, a mounting spring'within the post beneath the block, lowering means for the block and tensioning means forA the spring arranged within the basket, a parachute including a pole mounted upon the block axially of the post, a rinig upon the pole adapted for opening and c osing 'the parachute, an opening spring for the parachute tensioned between the said block and ring and a pull cord attached to the ring and extending to a point within the basket.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Emergency Lowering Means (AREA)
Description
J. SORDYKA.
BALLOON CONSTRUCTION.
APPLlcArloN Vmin Dic. 5. |911.
1,274,207. 4 Y Ptented Ju1y'3,1918.
2 SHEETS-*SHEET l.
J. SORDYKA.
BALLOON CONSTRUCTION.
APPLICATION min Dic. 5,'19x1.
1 ,274,207, Patented July 30, 1918.`
2 SHEETS-SHEET 2.
JOZEF SORDYKA, 0F GRAND RAPIDS, MICHIGAN.
BALLOON CONSTRUCTION.
Specification-o1' Letters Patent.
Patented July 30, 1918K.
Application led December 5, 1917. Serial No. 205,536.`
To all whom it may concern.'
Be it known that I, JOZEF SORDYKA, a citizen of the United States of America, residing at Grand Ra ids, in the county of Kent and State of Niichigan, have invented certain new and useful Improvements in Balloon `Construction, of whichv the following is a specification.
The primary object of the invention is the provision of a balloon adapted for carrying passengers such as soldiers detailed for dropping bombs upon. the enemy, arrangement being made for preserving the lives of 'the occupants in the event of damage to the elevating member.
A further object of the invention is the provision ofa compact' arrangement of parachute carried by a balloon adapted for instant use when the balloonis damaged but occupying only a small space when the parachute is not in use.
A still further object of the device is to provide a balloon especially adapted for war purposes'in dropping bombs and other explosives, the device being arranged with a Steering means and with a parachute adapted for opening automatically in the event of an accident to the balloon.
In the drawings forming a part of this application and in which like designating characters refer to correspondingparts throughout the several views,
Figure 1 is a side elevation of the device with the parachute in its open arrangement.
Fig. 2 is a vertical central sectional view thereof with parts broken away.
Fig. 3 is a view similar to Fig. 2 with the parachute in its inclosed i folded arrangemeit, and portions of `the device omitted an Fig. 4 is an enlarged transverse sectional view taken upon line IV-IV of Fig. 2.
Referring more in detail to the drawin it will be noted that my invention broa ly consists in a parachute 10 of umbrella form carried by a balloon 11 of substantially the usual appearance in such a manner as to be completely inclosed when not in use but automatically projected and opened for use when the occasion requires.
The balloon 11 has an inverted pearshaped gas bag 12 adapted for inflation for causing the device to rise in the air, a basket 13 beingsuspended therefrom by means of a tubular post`14 extending through the bag 12 and secured to the top thereof as at 15.
A telescope or sighting apparatus 16 is mounted in the basket 13 for looking downwardly through the bottom 17 of the basket for assisting the "soldiers operating the balloon to correctly aim the bombs 18 upon the nellpy when dropping the same out of the as et.
It Wai be understood that the basket 13 is i also connected with the bag 12 by the usual arrangement of suspending cables 19, and a sail 20 is carried at one side of the balloon for assisting the occupants in steering the device in its movements through the air. Upper and lo- wer supporting frames 21 and 22 carry the sail 20, and cords 23 are provided for lifting the sail when found desirable. y
The parachute 10 being in the form lof an umbrella, has a central pole or stick 24 having a cap 25 upon the upper end thereof, and a ring 26 is slidably arranged upon the pole 24 connected to the ribs ofthe parachute 10 by means of bows 27, whereby,r as will be apparent, the parachute may -be opened or closed, by elevating or lowering the ring 26. A reduced lower extension 28 is provided for the pole 24 mounted upon a disk or block 29 arranged within the post 14 in the manner of a piston. A spring'30 encircles the extension 28 and bars between the ringA 26 and block 29, and a cord 31 is attached to the ring 26 and passes through the post 14 to a suitable winding mechanismarf ranged within the basket 13.' By operating the winding mechanism the cord 31 pulls down on the ring 26, compressing the spring 30 and closing the parachute. It will be un-` derstood that when so compressed, a releasing of the ring 26 permits the spring 30 to automatically open the parachute 10 unless the same is otherwise restrained. l
A helical spring 32 is arranged within the post 14 being mounted at lts lower end upon an inner shoulder 33 of the post, and bearing at its upper end against the block 29. A cord 34 is arranged within the post 14 having its upper end attached to the block 29 and its other end connected to a winding mechanism 35 within the basket 13. It will be seen that when the parachute 10 has been compactly folded by pulling downwardly upon the cord 31, the parachute may be drawn inwardly of the post 14 by ranging the parachute in 'its normal inoperative position within the balloonI bag 12 as illustrated in Fig. 3 of the drawings.
During the use of the balloon, the parachute l0 is normally inclosed within the post 14, and the bag l2 being lilled with a suitable gas, the balloon will rise to the desired altitude `:tor viewing the enemy through the telescope 16 and dropping the bombs 18, while the rudder or sail 20 .slightly assists in steering the aircraft. ln the event of an injury to the bag 12, such for instance, as that occasioned by a shot from the enemy, the cord 34 may be released for automatically elevating the block 29 and projecting the folded parachute 10 outwardly of the upper end of the post 14, and the cord 31 being then released, the spring 30 automatically opens the parachute 10 in the form of an umbrella ermitting the entire device to gradually falli to the ground without injuring the remainder of the balloon or the contents of the basket 13. It will be seen that theprimary object is to automatically project the parachute 10 to its operative open position when required inthe event of an accident and which operation has been fully described while it will only be necessary to close the parachute and restore the same within the postI 1d when the balloon is on the ground and at which time the attendants may readily fold the fabric portion of the parachute 'for admitting the same into the post 14 upon pulling inwardly upon the cord 34.
A serviceable device is provided for use in time of war by means of which observations may be taken at high altitudes as well" as the dropping of missiles upon the enemy, while the safe descent of the operators will be insured by the mechanism provided and which takes up but little room during the aerial operation of the balloon.
What I claim as new is:-
1. An aircraft comprising a gas bag, a hollow post extending therethrough, a basket carried by the said post beneath the bag,
a folding parachute normally positionedv within the post and'projecting and opening means for the arachute adapted for control within the bas et.
2. An aircraft and elevating means, a hollow post secured to the elevating means,
a cargo carrier attached to the post, a toldable parachute adapted for normal arrangement wit-hin the post, means adapted for projecting the parachute outwardly of the post, lopening means for the parachute and Controlling members for the said projecting andopening means operable from a point within the cargo carrier.
3. A device of the class described coinprising an elevating bag for a balloon, a tubular post positioned ,therethrough attached to the top of the bag, a basket upon the lower end of the post beneath the bag, a block slidably arranged within the post, a mounting spring within the post beneath the block, lowering means for the block and tensioning means for the spring arranged within the basket and a folding parachute mounted upon the pocket and normally positioned within the post adapted for automatic opening when the block is elevated within the est. p 4. A device of the class described comprising an elevating bag for a balloon, a tubular post positioned therethrough attached to the top of the bag, a basket upon the lower end of the post beneath the bag, a block slidably arranged within the post, a mounting spring'within the post beneath the block, lowering means for the block and tensioning means forA the spring arranged within the basket, a parachute including a pole mounted upon the block axially of the post, a rinig upon the pole adapted for opening and c osing 'the parachute, an opening spring for the parachute tensioned between the said block and ring and a pull cord attached to the ring and extending to a point within the basket.
5t In combination with the gas bag of a balloon, a hollow post extending therethrough and attached to the top of the bag, a block slidably arranged within the post, automatic projecting means 'for the block, a parachute mounted upon the block adapted 'for arrangement in its folded position within the post, automatic opening means for the parachute and controlling means for the 4opening means and the projecting means operable at a point beneath the block.
In testimony whereof I aiix my signature. JOZEF SORDYKA.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20553617A US1274207A (en) | 1917-12-05 | 1917-12-05 | Balloon construction. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20553617A US1274207A (en) | 1917-12-05 | 1917-12-05 | Balloon construction. |
Publications (1)
Publication Number | Publication Date |
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US1274207A true US1274207A (en) | 1918-07-30 |
Family
ID=3341821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US20553617A Expired - Lifetime US1274207A (en) | 1917-12-05 | 1917-12-05 | Balloon construction. |
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US (1) | US1274207A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2492800A (en) * | 1948-08-16 | 1949-12-27 | Dewey And Almy Chem Comp | Fast rising sounding balloon |
US2575157A (en) * | 1950-05-09 | 1951-11-13 | Berthene Hugo | Parachute dropping kite |
US3120932A (en) * | 1960-11-14 | 1964-02-11 | Stahmer Bernhardt | Jet-balloon aircraft |
US4050653A (en) * | 1976-03-15 | 1977-09-27 | Bernard Sayers | Balloon |
US5967459A (en) * | 1997-05-19 | 1999-10-19 | Hayashi; Masahiko | Balloon with controlled parachute |
US6164594A (en) * | 1997-10-08 | 2000-12-26 | Etienne Lacroix Tous Artifices S.A. | Device for braking the fall of a load |
US20230338866A1 (en) * | 2022-04-21 | 2023-10-26 | Blake Barker | Helium Balloon Harness Assembly |
-
1917
- 1917-12-05 US US20553617A patent/US1274207A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2492800A (en) * | 1948-08-16 | 1949-12-27 | Dewey And Almy Chem Comp | Fast rising sounding balloon |
US2575157A (en) * | 1950-05-09 | 1951-11-13 | Berthene Hugo | Parachute dropping kite |
US3120932A (en) * | 1960-11-14 | 1964-02-11 | Stahmer Bernhardt | Jet-balloon aircraft |
US4050653A (en) * | 1976-03-15 | 1977-09-27 | Bernard Sayers | Balloon |
US5967459A (en) * | 1997-05-19 | 1999-10-19 | Hayashi; Masahiko | Balloon with controlled parachute |
US6164594A (en) * | 1997-10-08 | 2000-12-26 | Etienne Lacroix Tous Artifices S.A. | Device for braking the fall of a load |
US20230338866A1 (en) * | 2022-04-21 | 2023-10-26 | Blake Barker | Helium Balloon Harness Assembly |
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