US3129740A - Modified toric free drop container - Google Patents
Modified toric free drop container Download PDFInfo
- Publication number
- US3129740A US3129740A US203412A US20341262A US3129740A US 3129740 A US3129740 A US 3129740A US 203412 A US203412 A US 203412A US 20341262 A US20341262 A US 20341262A US 3129740 A US3129740 A US 3129740A
- Authority
- US
- United States
- Prior art keywords
- container
- fin
- free drop
- diaphragm
- drop container
- 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
- 239000000463 material Substances 0.000 claims description 13
- 239000012530 fluid Substances 0.000 claims description 4
- 230000005484 gravity Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000012254 powdered material Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
Definitions
- the invention relates to free drop containers of the type used to drop commodities, usually liquids or powdered materials, from a flying aircraft without the use of conventional parachutes.
- the container be stabilized in some way so that it lands in a uniform position no matter how dropped and also that such position is the one in which the container can best absorb the shear effect of the contents of the container walls whereby to minimize the chances of the container bursting upon impact.
- the invention is intended as an improvement over prior art devices such as the patents to Stavely, No. 2,700,517 and Bender, No. 2,784,755.
- Stavley patent aforesaid relies upon streamers to insure a stability during fall while the Bender patent relies upon an annular fin.
- Both of these patents are modified cylinders which are disc-like in structure whereby they tend to sail or side slip in flight whereby not to make flat landings regularly under adverse conditions such as high or gusty winds.
- a further object is to provide an improved free drop container in the form of a hollow torus which has been modified by the addition of an inverted, frusto-conical fin.
- a further object is to provide an improved free drop container as that last described to which has been added an annular diaphragm extending inwardly and upwardly of the container.
- FIGURE 1 is a plan view of the invention.
- FIGURE 2 is a transverse vertical sectional view taken substantially on the plane of the line 2-2 of FIGURE 1.
- 10 designates generally the free drop container according to one species of the invention which comprises a hollow torus 11 formed of flexible sheet material such as fabric reinforced elastomeric sheets.
- Torus 11 is provided with any suitable filling opening which may be closed by any suitable closure means 12.
- Torus 11 has a horizontal axis or center of gravity designated by the plane A and a normal topmost point lying along the horizontal plane T.
- annular fin 13 which is preferably of inverted frusto-conical form and which may be formed of any suitable flexible material.
- the fin 13 is formed with a plurality of hand holes 14 around the edge thereof to aid in manually transporting the loaded container.
- fin 13 is hollow and comprises a lower wall 15 which has a lower edge 16 which is secured to the torus 11 in the region of the horizontal axis A or even slightly above the same.
- Fin 13 also includes an upper Wall 17 which has an inner edge 3,129,740 Patented Apr. 21, 1964 18 which is secured to the torus 11 in the region of its topmost point as defined by the plane T.
- Fin walls 15 and 17 converge in outward and upward directions to provide the hollow fin 13. Their outer or free edges merge and are integrally connected together to provide a common outer rim 19.
- the interior of the fin 13 may be filled with resilient compressible cushioning material such as an inert gas as in our co-pending applications, Serial Nos. 203,414 and 203,415 both filed June 18, 1962 for the same purpose as there set forth.
- Diaphragm 20 extends upwardly and inwardly of the torus 11 concentrically thereof.
- the diaphragm 20 comprises upper and lower walls 21 and 23 respectively.
- the upper wall 21 has an inner edge 22 which is secured to the torus 11 in the region of its topmost point as defined by the plane T.
- the lower wall 23 has a lower edge 24 which is secured to the torus 11 in the region of the horizontal axis thereof as defined by the plane A.
- Diaphragm walls 21 and 23 converge upwardly and inwardly and are integrally connected together to provide a common inner edge or rim 25 which defines a center opening or hole 26 through the diaphragm.
- the diaphragm 20 is hollow and is preferably filled with any suitable resilient cushioning material to alleviate the shock of impact upon the walls of the torus 11.
- a hollow toric fluid container formed of flexible sheet material, an inverted frustoconical skirt surrounding said container concentrically thereof to provide an annular fin, said fin being hollow and being defined by upper and lower walls converging in upward and outward directions, and said walls being formed of flexible sheet material.
- a hollow toric fluid container formed of flexible sheet material, an inverted frustoconical skirt concentrically surrounding said container to provide an annular fin, said fin being formed of flexible sheet material, and an annular diaphragm of flexible sheet material carried by said container and extending radially inwardly and concentrically thereof.
- a free drop container according to claim 4, wherein said diaphragm is hollow and comprises upper and lower walls of flexible sheet material, and said walls of said diaphragm converging in upward and inward directions.
- said lower wall of said diaphragm has an inner edge secured to said container in the region of the horizontal axis thereof.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Packages (AREA)
Description
April 21, 1964 J. H. NOURSE ETAL Filed June 18, 1962 a fii ZzT Z/ 7' mvau'rons F 3 WilltlamB Crawford JESS 8 ATTORNEY United States Patent 3,129,740 MODIFIED TORIC FREE DROP CONTAINER Jess H. Nourse, Ypsilanti, Mich, and William B. Crawford, Mishawalra, Ind., assignors to the United States of America as represented by the Secretary of the Army Filed June 18, 1962, Ser. No. 203,412 7 Claims. (Cl. 150.5)
The invention relates to free drop containers of the type used to drop commodities, usually liquids or powdered materials, from a flying aircraft without the use of conventional parachutes. In such devices, it is of the essence that the container be stabilized in some way so that it lands in a uniform position no matter how dropped and also that such position is the one in which the container can best absorb the shear effect of the contents of the container walls whereby to minimize the chances of the container bursting upon impact. Specifically, the invention is intended as an improvement over prior art devices such as the patents to Stavely, No. 2,700,517 and Bender, No. 2,784,755.
The Stavley patent aforesaid relies upon streamers to insure a stability during fall while the Bender patent relies upon an annular fin. Both of these patents are modified cylinders which are disc-like in structure whereby they tend to sail or side slip in flight whereby not to make flat landings regularly under adverse conditions such as high or gusty winds.
With the foregoing in view, it is an object of the invention to provide an improved free drop container of the class described.
A further object is to provide an improved free drop container in the form of a hollow torus which has been modified by the addition of an inverted, frusto-conical fin.
A further object is to provide an improved free drop container as that last described to which has been added an annular diaphragm extending inwardly and upwardly of the container.
Other objects and advantages reside in the particular structure of the invention, the structure of the several elements thereof, combinations and subcombinations of such elements, all of which will be readily apparent to those skilled in the art upon reference to the attached drawing which illustrates one species of the invention and to the following specification wherein the invention is described and claimed.
In the drawing:
FIGURE 1 is a plan view of the invention; and
FIGURE 2 is a transverse vertical sectional view taken substantially on the plane of the line 2-2 of FIGURE 1.
Referring specifically to the drawing, wherein like reference characters designate like parts in all views, 10 designates generally the free drop container according to one species of the invention which comprises a hollow torus 11 formed of flexible sheet material such as fabric reinforced elastomeric sheets. Torus 11 is provided with any suitable filling opening which may be closed by any suitable closure means 12. Torus 11 has a horizontal axis or center of gravity designated by the plane A and a normal topmost point lying along the horizontal plane T. To stabilize the container 10 during its free fall, there has been provided an annular fin 13 which is preferably of inverted frusto-conical form and which may be formed of any suitable flexible material. In the embodiment illustrated, the fin 13 is formed with a plurality of hand holes 14 around the edge thereof to aid in manually transporting the loaded container. Also, fin 13 is hollow and comprises a lower wall 15 which has a lower edge 16 which is secured to the torus 11 in the region of the horizontal axis A or even slightly above the same. Fin 13 also includes an upper Wall 17 which has an inner edge 3,129,740 Patented Apr. 21, 1964 18 which is secured to the torus 11 in the region of its topmost point as defined by the plane T. Fin walls 15 and 17 converge in outward and upward directions to provide the hollow fin 13. Their outer or free edges merge and are integrally connected together to provide a common outer rim 19. The interior of the fin 13 may be filled with resilient compressible cushioning material such as an inert gas as in our co-pending applications, Serial Nos. 203,414 and 203,415 both filed June 18, 1962 for the same purpose as there set forth.
To further stabilize the container 10 during free fall, there has been provided an annular diaphragm 20 of any suitable flexible sheet material. Diaphragm 20 extends upwardly and inwardly of the torus 11 concentrically thereof. In the embodiment illustrated, the diaphragm 20 comprises upper and lower walls 21 and 23 respectively. The upper wall 21 has an inner edge 22 which is secured to the torus 11 in the region of its topmost point as defined by the plane T. Also, the lower wall 23 has a lower edge 24 which is secured to the torus 11 in the region of the horizontal axis thereof as defined by the plane A. Diaphragm walls 21 and 23 converge upwardly and inwardly and are integrally connected together to provide a common inner edge or rim 25 which defines a center opening or hole 26 through the diaphragm.
As in the case of the fin 13, the diaphragm 20 is hollow and is preferably filled with any suitable resilient cushioning material to alleviate the shock of impact upon the walls of the torus 11.
During static conditions, it is understood that the container 10 when its torus 11 is filled with fluid or the like will assume the shape shown in full lines in FIGURE 2. However, during free fall the fin 13 and, to a lesser extent, the diaphragm 20, will be deflected upwardly to the broken line positions of FIGURE 2. By olfsetting the fin and diaphragm upwardly of the horizontal axis A, the container is assured of presenting its underside to the impact surface at all times. The diaphragm 20 together with its opening 26 minimizes any sailing or side slip and insures a level fall, opening 26 functioning like the like opening in a conventional parachute to increase stability. Fin 13, of course, assists in stabilizing the container and to a lesser extent retards the free fall speed. As aforesaid, both fin 13 and diaphragm 20 by virtue of their resilient contents reinforce inner and outer portions of the torus wall against the shock of impact.
While there has been shown and described what is now believed to be a preferred species of the invention, it should be understood that the same is susceptible of other forms and expressions. Consequently, we do not limit ourselves to the exact embodiment shown and described hereinabove except as hereinafter claimed.
We claim:
1. In a free drop container, a hollow toric fluid container formed of flexible sheet material, an inverted frustoconical skirt surrounding said container concentrically thereof to provide an annular fin, said fin being hollow and being defined by upper and lower walls converging in upward and outward directions, and said walls being formed of flexible sheet material.
2. In a free drop container, a hollow toric fluid container formed of flexible sheet material, an inverted frustoconical skirt concentrically surrounding said container to provide an annular fin, said fin being formed of flexible sheet material, and an annular diaphragm of flexible sheet material carried by said container and extending radially inwardly and concentrically thereof.
3. A free drop container according to claim 1, wherein said lower wall of said fin includes an inner edge secured to said container in the region of its horizontal axis, and said upper wall of said fin having an inner edge secured to said container in the regions of its topmost point.
4. A free drop container according to claim 3, there being an annular diaphragm carried by said container and extending radially inwardly and concentrically thereof.
5. A free drop container according to claim 4, wherein said diaphragm is hollow and comprises upper and lower walls of flexible sheet material, and said walls of said diaphragm converging in upward and inward directions.
6. A free drop container according to claim 5, wherein said upper wall of said diaphragm has an inner edge secured to said container in the region of its topmost point,
4. and said lower wall of said diaphragm has an inner edge secured to said container in the region of the horizontal axis thereof.
7. A free drop container according to claim 2, wherein 5 both said fin and diaphragm are connected to said container above the horizontal center of gravity thereof.
References Cited in the file of this patent UNITED STATES PATENTS Wyllie Sept. 30, 1958
Claims (1)
1. IN A FREE DROP CONTAINER, A HOLLOW TORIC FLUID CONTAINER FORMED OF FLEXIBLE SHEET MATERIAL, AN INVERTED FRUSTOCONICAL SKIRT SURROUNDING SAID CONTAINER CONCENTRICALLY THEREOF TO PROVIDE AN ANNULAR FIN, SAID FIN BEING HOLLOW AND BEING DEFINED BY UPPER AND LOWER WALLS CONVERGING IN UPWARD AND OUTWARD DIRECTIONS, AND SAID WALLS BEING FORMED OF FLEXIBLE SHEET MATERIAL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US203412A US3129740A (en) | 1962-06-18 | 1962-06-18 | Modified toric free drop container |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US203412A US3129740A (en) | 1962-06-18 | 1962-06-18 | Modified toric free drop container |
Publications (1)
Publication Number | Publication Date |
---|---|
US3129740A true US3129740A (en) | 1964-04-21 |
Family
ID=22753887
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US203412A Expired - Lifetime US3129740A (en) | 1962-06-18 | 1962-06-18 | Modified toric free drop container |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3334676A (en) * | 1965-10-20 | 1967-08-08 | Ryan Aeronautical Co | Aerial delivery of liquid provisions |
US4516767A (en) * | 1982-08-09 | 1985-05-14 | Luther Eskijian | Inflatable platform for repetitive bouncing |
DE4339052A1 (en) * | 1993-11-16 | 1995-05-18 | Juergen Haro | Air transport containers |
US6663538B2 (en) * | 2000-12-26 | 2003-12-16 | Jung-Ho Yoon | Safety trampoline |
US20120241346A1 (en) * | 2008-11-26 | 2012-09-27 | Florian Wiest | Packaging having means for passive flight |
US9089732B2 (en) | 2011-06-09 | 2015-07-28 | Vuly Trampolines Pty, Ltd. | Trampolines |
US9486658B2 (en) | 2001-11-20 | 2016-11-08 | Board & Batten International Inc. | Edge fittings for soft-edged trampoline |
US11338992B2 (en) | 2009-11-25 | 2022-05-24 | Florian Wiest | Packaging having means for passive flight |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2854049A (en) * | 1956-12-11 | 1958-09-30 | Elliot Equipment Ltd | Collapsible storage tanks |
-
1962
- 1962-06-18 US US203412A patent/US3129740A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2854049A (en) * | 1956-12-11 | 1958-09-30 | Elliot Equipment Ltd | Collapsible storage tanks |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3334676A (en) * | 1965-10-20 | 1967-08-08 | Ryan Aeronautical Co | Aerial delivery of liquid provisions |
US4516767A (en) * | 1982-08-09 | 1985-05-14 | Luther Eskijian | Inflatable platform for repetitive bouncing |
DE4339052A1 (en) * | 1993-11-16 | 1995-05-18 | Juergen Haro | Air transport containers |
US6663538B2 (en) * | 2000-12-26 | 2003-12-16 | Jung-Ho Yoon | Safety trampoline |
US9486658B2 (en) | 2001-11-20 | 2016-11-08 | Board & Batten International Inc. | Edge fittings for soft-edged trampoline |
US9656110B2 (en) | 2001-11-20 | 2017-05-23 | Board & Batten International Inc. | Edge fittings for soft-edged trampolines |
US20120241346A1 (en) * | 2008-11-26 | 2012-09-27 | Florian Wiest | Packaging having means for passive flight |
US11338992B2 (en) | 2009-11-25 | 2022-05-24 | Florian Wiest | Packaging having means for passive flight |
US9089732B2 (en) | 2011-06-09 | 2015-07-28 | Vuly Trampolines Pty, Ltd. | Trampolines |
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