US1542547A - Kite balloon - Google Patents

Kite balloon Download PDF

Info

Publication number
US1542547A
US1542547A US756379A US75637924A US1542547A US 1542547 A US1542547 A US 1542547A US 756379 A US756379 A US 756379A US 75637924 A US75637924 A US 75637924A US 1542547 A US1542547 A US 1542547A
Authority
US
United States
Prior art keywords
rigging
balloon
band
elastic
bands
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
US756379A
Inventor
Gibbs Herbert Gray
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 US756379A priority Critical patent/US1542547A/en
Application granted granted Critical
Publication of US1542547A publication Critical patent/US1542547A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons

Definitions

  • This invention relates to the construction of kite balloons, of the type in which the balloon is permitted to expand or to contract as the volume of the gas increases or diminishes, owing to decrease or increase in atmospheric pressure or to changes in tem perature of the gas.
  • the balloon is constructed in streamline form, and is of a capacity sufficient to contain the gas when expanded by diminution in atmospheric pressure'to the capacity required for attaining great altitudes, say for instance 30,000 ft.
  • cqui-distant riggingbands Longitudinally within the balloon four cqui-distant riggingbands are attached to the fabric, the location of the two upper. rigging bands being equi-distant from a vertical plane passing through the longitudinal axis of the balloon, and the two lower rigging bands being also equi-distant from the same vertical plane, c
  • the rigging band on the port side of the upper pair of'rigging bands is connected by elastic. tensionmemberswith the rigging band on the starboard'side of the lower pair 7 of rigging bands; and the rigging band on the starboard side of the upper pair of rigging bands is connected by a separate system of elastic tension members with the rigging band on the port side of the lower pair of rigging bands;
  • the said elast c tension members may be composed of indla rubber, although they may if desired be constructed of steel springs; butindia rubber elastic is preferable in most instances in order to facilitate packing of the kite balloon when deflated.
  • the said elastic tension members may be circular in cross section and spaced apart in the manner of lacing,
  • Fig. 1 is a perspective view partly in section, showing the after part of a kite balloon with the interior rigging bands, the
  • Flg. 2 is a cross section of the same baloon.
  • Figs. 3 and 4 are detail views of the method of attachment of a rigging band to the interior of the balloon fabric
  • Fig. 5 is a further detail illustrating a convenient method of distributing the tension of the tension members onto the rig ging band and thence to the balloon fabric.
  • Fig. 6 illustrates an alternativeconstruction of elastic balloon constructed'in accor ance with this invention. 0 0
  • A is the starboardupper rigging, band, and B the port upper rigging band.
  • E, E are the elastic members connecting the starboard upper rigging band A with the port lower rigging band D
  • F, F are the elastic members connecting the port upper rigging band B. with the starboard lower rigging band C.
  • the tension members E and F have, caused the rigging bands A and D to be drawn together and the rigging bands B and C also to be drawn together, to the extent at which the pressure of the gas balances the tension on the elastic members E and F, and .in the dotted line around the full line section the balloon isshown to have expanded to'a larger cubic capacity, either by reason of diminutionof external atmospheric pressure due for instance to increasing altitude, or to expansion of the gas contained in the balloon due to increase in temperature. In such case the expansion of the balloon increases the tension on'the elastic members E and F.
  • rigging bands instead of being placed equidistant circumferentially around the longitudinal axis of the balloon, are placed in symmetrical positions but closer together in vertical directions and farther apart in horizontal directions than when they are equidistant circumferentially. This increases the surface of the balloon on the upper side and on the lower side where two large lobes are formed, and diminishes'the surface of the portion of the balloon on the port and starboard sides where smaller lobes are formed.
  • the effect of changing the propor tion in this way is to lessen the liability of the collection of snow or water in the longitudinal folds of theballoon outside the location ofv the rigging bands A, B, C and D.
  • the larger lobe on the under side of the balloon also facilitates the suitable attachment of the patches to which the rigging G of the car suspension is attached. 7
  • the elastic tension members may completely traverse the balloon diagonally as before described, or they may be shortened by the introduction of fabric gussets eX- tending inwardly from the rigging bands.
  • Figs. 8 and 4 a suitable method of attachment of the rigging band to the fabric of the balloon is shown.
  • the band is constructed of fabric doubled upon itself so as to leave two edges A A for attachment to the interior walls of the balloon,
  • This folded portion A may be extended whereby the shortening of the elastic tension members is facilitated.
  • non-elastic cords may be employed with the object of reducing the length of the elastic tension members.
  • the non-elastic cords may, for example, be attached to the rigging bands as shown at Fig. 5, where the elastic tension members E are attached to divide crows feet E E which in their turn are attached to eyelets E in the folded portion A of the rigging band.
  • tail fins may be employed with their centres at angles radiating 120 apart, and thesaid fins may be made to communicate with the interior of the balloon and contain gas instead of air, which is the general practice.
  • the inflation of the said fins with gas maintains their form, while the balloon is on the ground, and promotes stability when letting out and hauling down when the balloon is near the ground.
  • An elastic kite balloon in which the gas is maintained at the desired degree of pressure by means of tension members, four rigging bands spaced equi-distant apart on the interior of the balloon, two on the starboard side and two on the port side, elastic tension members connecting the upper starboard rigging band to the lower port rigging band, and elastic tension members connecting the upper port rigging band to the lower starboard rigging band.
  • An elastic kite balloon in which the gas is maintained at the desired degree of pressure by means of tension members, four rigging bands on the interior of the balloon, two on the starboard side and two on the port side, the distance between the starboard rigging bands and the port rigging bands being greater than the distance of upper and lower rigging bands in each pair from each other, elastic tension members connecting the upper starboard rigging band to the lower port rigging band, and elastic tension members connecting the upper port rigging band to the lower starboard rigging band.

Description

June 16, 1925.
5 HfG. area's KITE BALLOON Filed Dec. 17, 1924 2 Sheets-Sheet 1 June 16, 1925.
H. G. GIBBS KITE BALLOON 2 Sheets-Sheet 2 Filed Debq 1'7. 1924 (WWI Patented June 16, 1925.
HERBERT GRAY GIBBS, or Lennon, ENGLAND.
xrrn BALLOON.
Application filed December 17,1924. Serial No. 36,379. i
To all whom it may concern:
Be itknown that I, HERBERT GRAY GIBBS, a subject of the King of Great Britain, residing at 19, Surrey Street, Strand, London, IV. C. 2, England, have invented certain new and useful Improvements in KiteBalloons, of which the following is a specification. V
This invention relates to the construction of kite balloons, of the type in which the balloon is permitted to expand or to contract as the volume of the gas increases or diminishes, owing to decrease or increase in atmospheric pressure or to changes in tem perature of the gas.
According to this invention, the balloon is constructed in streamline form, and is of a capacity sufficient to contain the gas when expanded by diminution in atmospheric pressure'to the capacity required for attaining great altitudes, say for instance 30,000 ft.
Longitudinally within the balloon four cqui-distant riggingbands are attached to the fabric, the location of the two upper. rigging bands being equi-distant from a vertical plane passing through the longitudinal axis of the balloon, and the two lower rigging bands being also equi-distant from the same vertical plane, c
The rigging band on the port side of the upper pair of'rigging bands, is connected by elastic. tensionmemberswith the rigging band on the starboard'side of the lower pair 7 of rigging bands; and the rigging band on the starboard side of the upper pair of rigging bands is connected by a separate system of elastic tension members with the rigging band on the port side of the lower pair of rigging bands; The said elast c tension members may be composed of indla rubber, although they may if desired be constructed of steel springs; butindia rubber elastic is preferable in most instances in order to facilitate packing of the kite balloon when deflated. The said elastic tension members may be circular in cross section and spaced apart in the manner of lacing,
the distance apart of each strand and thestrength of such strands depending on the strength of the elastic connectlons employed, and on the degree of pressure at which it 1s desired to maintain the balloon,
In the drawings,
Fig. 1 is a perspective view partly in section, showing the after part of a kite balloon with the interior rigging bands, the
elastic tension members being arranged I diagonally across the balloon, and
Flg. 2 is a cross section of the same baloon.
Figs. 3 and 4 are detail views of the method of attachment of a rigging band to the interior of the balloon fabric, and
Fig. 5 is a further detail illustrating a convenient method of distributing the tension of the tension members onto the rig ging band and thence to the balloon fabric.
Fig. 6 illustrates an alternativeconstruction of elastic balloon constructed'in accor ance with this invention. 0 0
Referring particularly to Figs. 1, 2 and 6, A is the starboardupper rigging, band, and B the port upper rigging band. Cris the starboard lower rigging band, and D the port lower rigging band. E, E are the elastic members connecting the starboard upper rigging band A with the port lower rigging band D, and F, F are the elastic members connecting the port upper rigging band B. with the starboard lower rigging band C. i
As shown at Fig. 2, the tension members E and F have, caused the rigging bands A and D to be drawn together and the rigging bands B and C also to be drawn together, to the extent at which the pressure of the gas balances the tension on the elastic members E and F, and .in the dotted line around the full line section the balloon isshown to have expanded to'a larger cubic capacity, either by reason of diminutionof external atmospheric pressure due for instance to increasing altitude, or to expansion of the gas contained in the balloon due to increase in temperature. In such case the expansion of the balloon increases the tension on'the elastic members E and F.
In the modification shown at Fig. '6, the
rigging bands, instead of being placed equidistant circumferentially around the longitudinal axis of the balloon, are placed in symmetrical positions but closer together in vertical directions and farther apart in horizontal directions than when they are equidistant circumferentially. This increases the surface of the balloon on the upper side and on the lower side where two large lobes are formed, and diminishes'the surface of the portion of the balloon on the port and starboard sides where smaller lobes are formed. The effect of changing the propor tion in this way is to lessen the liability of the collection of snow or water in the longitudinal folds of theballoon outside the location ofv the rigging bands A, B, C and D. The larger lobe on the under side of the balloon also facilitates the suitable attachment of the patches to which the rigging G of the car suspension is attached. 7
The elastic tension members may completely traverse the balloon diagonally as before described, or they may be shortened by the introduction of fabric gussets eX- tending inwardly from the rigging bands. At Figs. 8 and 4 a suitable method of attachment of the rigging band to the fabric of the balloon is shown. The band is constructed of fabric doubled upon itself so as to leave two edges A A for attachment to the interior walls of the balloon,
- the folded portion A forming an inwardly extending pocket to receive wooden pegs H for locking the ends of the elastic tension members E in position. This folded portion A may be extended whereby the shortening of the elastic tension members is facilitated.
Instead of, or in addition to an inwardly extended folded portion A of the rigging bands, non-elastic cords may be employed with the object of reducing the length of the elastic tension members. The non-elastic cords may, for example, be attached to the rigging bands as shown at Fig. 5, where the elastic tension members E are attached to divide crows feet E E which in their turn are attached to eyelets E in the folded portion A of the rigging band.
The usual tail fins may be employed with their centres at angles radiating 120 apart, and thesaid fins may be made to communicate with the interior of the balloon and contain gas instead of air, which is the general practice. The inflation of the said fins with gas maintains their form, while the balloon is on the ground, and promotes stability when letting out and hauling down when the balloon is near the ground.
What I claim as my invention and desire to secure by Letters Patent is 1. An elastic kite balloon, in which the gas is maintained at the desired degree of pressure by means of tension members, four rigging bands on the interior of the balloon, two on the starboard side and two on the port side, elastic tension members connecting the upper starboard rigging band to the lower port rigging band, and elastic tension members connecting the upper port rigging band to the lower starboard rigging band.
I 2; An elastic kite balloon, in which the gas is maintained at the desired degree of pressure by means of tension members, four rigging bands spaced equi-distant apart on the interior of the balloon, two on the starboard side and two on the port side, elastic tension members connecting the upper starboard rigging band to the lower port rigging band, and elastic tension members connecting the upper port rigging band to the lower starboard rigging band.
8. An elastic kite balloon, in which the gas is maintained at the desired degree of pressure by means of tension members, four rigging bands on the interior of the balloon, two on the starboard side and two on the port side, the distance between the starboard rigging bands and the port rigging bands being greater than the distance of upper and lower rigging bands in each pair from each other, elastic tension members connecting the upper starboard rigging band to the lower port rigging band, and elastic tension members connecting the upper port rigging band to the lower starboard rigging band.
i In witness whereof I have hereunto set my hand in the presence of two witnesses.
HERBERT GRAY GIBBS.
itnesses R. UNGAR. LESLIE F. Rooms.
US756379A 1924-12-17 1924-12-17 Kite balloon Expired - Lifetime US1542547A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US756379A US1542547A (en) 1924-12-17 1924-12-17 Kite balloon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US756379A US1542547A (en) 1924-12-17 1924-12-17 Kite balloon

Publications (1)

Publication Number Publication Date
US1542547A true US1542547A (en) 1925-06-16

Family

ID=25043207

Family Applications (1)

Application Number Title Priority Date Filing Date
US756379A Expired - Lifetime US1542547A (en) 1924-12-17 1924-12-17 Kite balloon

Country Status (1)

Country Link
US (1) US1542547A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2679224A (en) * 1949-01-21 1954-05-25 Goodyear Tire & Rubber Fluted salvage device
US2805830A (en) * 1952-07-01 1957-09-10 Helmut P G A R Von Zborowski Annular lift-producing wing
US3412957A (en) * 1965-09-24 1968-11-26 Arthur D. Struble Jr. Inflated balloon

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2679224A (en) * 1949-01-21 1954-05-25 Goodyear Tire & Rubber Fluted salvage device
US2805830A (en) * 1952-07-01 1957-09-10 Helmut P G A R Von Zborowski Annular lift-producing wing
US3412957A (en) * 1965-09-24 1968-11-26 Arthur D. Struble Jr. Inflated balloon

Similar Documents

Publication Publication Date Title
US3004737A (en) Retractable buoyant supporting means for vehicles
US3063656A (en) Plastic cylinder balloon
US1542547A (en) Kite balloon
US1372924A (en) Airship
US1682405A (en) Nonrigid airship
US3534927A (en) Structure of hot air aerial balloon
US2398744A (en) Kite balloon
US3350040A (en) High speed deceleration device
US3403876A (en) Parachutes
US2173262A (en) Deicer for airships
US1686646A (en) Kite balloon
US2384721A (en) Life preserving apparatus
US1475210A (en) upson
US1364596A (en) Pneumatically-reinforced casing for aeronautic carriers
US3602462A (en) Parachute
US2864569A (en) Captive balloon
US1370043A (en) Dirigible
US2450926A (en) Parachute made of self-supporting ribbons which are composed of broad and narrow bands
US1884705A (en) Pneumatic boat
US2175229A (en) Parachute
US1700096A (en) Gas cell for rigid airships
US2156175A (en) Pneumatic boat
US1925133A (en) Aircraft
US1502551A (en) Captive balloon
US1623865A (en) Airship