US2741159A - Master bomb rainer - Google Patents
Master bomb rainer Download PDFInfo
- Publication number
- US2741159A US2741159A US297731A US29773152A US2741159A US 2741159 A US2741159 A US 2741159A US 297731 A US297731 A US 297731A US 29773152 A US29773152 A US 29773152A US 2741159 A US2741159 A US 2741159A
- Authority
- US
- United States
- Prior art keywords
- bomb
- bombs
- pockets
- chutes
- rainer
- 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
- 230000001276 controlling effect Effects 0.000 description 3
- 230000004075 alteration Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000003892 spreading Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/01—Feeding of unbelted ammunition
- F41A9/04—Feeding of unbelted ammunition using endless-chain belts carrying a plurality of ammunition
- F41A9/05—Feeding of unbelted ammunition using endless-chain belts carrying a plurality of ammunition in tandem sequence
-
- 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
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bomb doors
Definitions
- Fig. 12 is an enlarged fragmentary section on the line 1313:of:Fig. l0. 1
- Fig. 14 is a slightly enlarged sectionv of suchchute' control.
- each of these means includes a plate 33, whereon is mounted a shaft 34, which is rotated by a lever 35. On this shaft 34 is fixed a gear 36, which meshes'with a rack member 37 welded to the lower end 30 of a chute.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
April 10, 1956 5. J. PROCOS MASTER BOMB RAINER 5 Sheets-Sheet 1 Filed July 8, 1952 III INVENTOR, 1 Steve J. Procos,
April 10, 1956 5. J. PRocos 2,741,159
MASTER BOMB RAINER Filed July 8, 1952 5 Sheets-Sheet 2 llll lllll l-l k L {I I u u INVENTOR,
.Si'eve d. Procos,
HTTORN 5Y6 S. J. PROCOS MASTER BOMB RAINER April 10, 1956 5 Sheets-Sheet 3 Filed July 8, 1952 April 10, 1956 s. J. PRocos 2,741,159
MASTER BOMB RAINER Filed July 8, 1952 5 Sheets-Sheet 4 INVENTOR, Steve d1 ProcoS.
HTTORNE Y5 April 10, 1956 s. J. PROCOS 2,741,159
MASTER BOMB RAINER Filed July 8, 1952 5 Sheets-Sheet 5 U 0 0 M E Q 4955 d INVENTOK, Steve J1 Procos,
m w g MASTER BOMB RAINER Steve J. Procos, Chicago, Ill.
Application July 8, 1952, Serial No. 297,731
1 Claim. (Cl. 89-15) This invention relates to a bomb dropping device for airplanes.
One important object of the invention is to provide novel means whereby a multiplicity of bombs may be carried by an airplane and discharged therefrom in groups, each group consisting of a plurality of bombs.
A second important object of the invention is to provide a device of this character wherein the bombs are loaded on the airplane in a series of rows extending longitudinally oi the plane and each row consisting of bombs.
A third important object of the invention is to provide a device of this character wherein the rows are driven by endless chains and bombs are discharged from the rows simultaneously on reaching one extremity of the endiess chain device.
. A fourth important object of the invention is to provide a device of this character having the multiplicity of bomb pockets carried by endless chains, each of said pockets holding an individual bomb and discharging these bombs as-the endless chain turns to move from its forward direction to its rearward direction.
A fifth important object of the invention is to provide such bomb carrying pockets with open ends so that tilting of the pockets etfects the discharge of the bombs.
A sixth important object of the invention is to provide a novel form of pocket consisting of two halves movable toward and from each other so as to hold a bomb when the halves are moved toward each other and to release the bomb when the halves are moved away from each other.
A seventh important object of the invention is to provide a novel chute arrangement for properly distributing the bombs as they pass out of the bomb holding pockets.
An eighth important object of the invention is to provide controlling means for regulating the passage of the bombs from the chutes, controlling means being arranged to effect proper distribution in accordance with the height of the airplane above the ground.
The invention consists in general of certain novel details of construction and combinations of parts hereinafter fully described, illustrated in the accompanying drawings, and particularly claimed.
In the accompanying drawings like characters of reference indicate like parts, and:
Fig. 1 is a plan view of one form of the bomb carrying apparatus, the airplane being shown in broken outline to indicate the position of this apparatus in the plane, the bombs being removed therefrom.
Fig. 2 is an enlarged fragmentary plan at the delivery end of a bomb carrying device.
Fig. 3 is an end view of Fig. 2, the view being taken from the right hand end thereof.
Fig. 4 is an enlarged detailed side view of that part of the device as shown in Figs. 2 and 3.
Fig. 5 is a view showing a further enlargement of the parts shown in Fig. 4 and showing the movement of bombs from the carrier to the chutes.
2,741,159 Patented Apr. 10,. 1956 Fig. 6- is a fragmentary detail-showing the manner of supporting. the: bomb chute.
Fig. 1 is a greatly enlarged plan view of one. form of a.- bomb carrying pocket.
Fig. 8 is asimilar view to Fig; 7 but showing a slightly modified form on the line 9--9 of Fig. 7.
Fig. 9 is a fragmentary view' of a portion of the bomb carrier having. split bomb pockets.
Fig. 10. is aside view showing a plurality of thepockets shown in Fig. 9.
Fig. 11 is an enlarged plan view of a portion of Fig. 9.
Fig. 12 is an enlarged fragmentary section on the line 1313:of:Fig. l0. 1
Fig. 13 is a detailed. view. showing a form of chute control.
Fig. 14 is a slightly enlarged sectionv of suchchute' control.
Fig. 15 is an end view of twov bomb delivery sections as installed inan airplane, the spreading of the bombs being, illustratedv below one of these sections.
In the embodiments of the invention as here shown, it is preferred that two general arrangements of bomb carrying dispensing means shall be used in the fuselage 10 oi an airplane, one being on each side of the axis of the plane. Each of. these devices, as best shown in Figs. 1 to 8, l0 and 14,. consists of a pair of laterally spaced side frames indicated in general at 11. Each of these frames includes an upper rail 12, and a lower rail. 13, the upper and lower rai-l being connected by arcuate members 14. In the space adjacent each end. of the frame is mounted a sprocket wheel 15. carried by a shaft 16 suitably supported from the frame by any suitable means. The sprocket wheel for each frame is coplanar with the frame and around the sprocketsv of each frame: is trained an. end less chain 17. The chain of one frame is connected to the chain of the other frame by means of tie bars 18, on which are mounted bomb holding pockets 19, which may have one end fully open as in Fig. 7 or may have a slight rib or flange 20 extending between the sides of the pockets as at Fig. 8. These pockets are in laterally spaced relation and are there fixedly secured to the tie bars, the arrangement being such that the pockets of one tie bar are arranged in alignment with the pockets of adjacent tie bars so that longitudinal rows of pockets are formed as clearly shown in Fig. 1. In use, bombs are carried in the pockets whichface upwardly, the pockets which face downwardly being thosefrom which the bombs21 have been discharged. In order to provide smooth movements of the upper run 22 of the chain, the upper rail 12 is provided with rollers 23, on which the chain travels. Rollers 24 are also provided on the lower rail 13 for the purpose of preventing slipping of the chain against the lower rail. At one end of the frames there is indicated in Fig. 1, a drive shaft 24, which is driven by any suitable means not deemed necessary here to be shown. This drive shaft is connected by bevelled gearing 25 with a sprocket shaft 16 at this end of the device. At the other end of the frames there is provided an auxiliary frame 26, which projects from the main frame beyond the sprockets and which is provided at its upper portion with a crossed bar 27. This crossed bar 27 carries the upper trumpetlike ends 28 of a series of chutes equal in number to and aligned with the rows of pockets 19. The connection of these upper ends 28 with the bar 27 is made in the form of a pivot 29 so that the lower delivery ends 30 of the chutes may rest against the lower cross bar 31 of the auxiliary frame.
As shown here there has been indicated seven rows of bombs and there are, of course, seven chutes. The central one of these seven chutes is fixed, as by a bolt 32, while the other chutes have their lower ends free for swinging adjustment on the pivots 28. In order to ob tain the adjustment of these lower ends the means best shown in Figs. 13 and 14 is provided. Each of these means includes a plate 33, whereon is mounted a shaft 34, which is rotated by a lever 35. On this shaft 34 is fixed a gear 36, which meshes'with a rack member 37 welded to the lower end 30 of a chute. On the lower edge of the rack member 37 is a series of ratchet teeth 38 wherewith meshes a pawl 39 mounted in a guide 40 fixed to the plate 33. Between the bottom of the guide 40 and the lower end of the pawl 39 is a coiled compression spring 41. This ratchet and pawl arrangement is such that movement of the lever 35 will cause the ratchet to slide over the pawl, the teeth being at proper angles to permit this. When this pawl has engaged the ratchet then the adjusting device will be releasably locked. If desired, an opening 42 may be provided in the member 37 and indicia 43 will be formed on the plate 33 and observable through the opening 42. This indicia may be graduated in accordance with the desired spreading of the bombs for different altitudes of the plane.
While seven rows of bombs and chutes are shown, any desired number may be used, as for instance, three to nine, or any other number of rows and bombing chutes.
In the form of the invention shown in Figs. 9 to 12, the bomb pocket 43 is split longitudinally so as to provide two halves which are adjustable to fit closely on the bomb depending on its diameter. These halves are supported by arms 44 from bars 45 and are guided by pins 46. The arms 44 are attached at their outer ends to rods 47, which by movement toward and from the bars 45 serve to open and close the halves of the pockets 43.
The upwardly facing bomb pockets are filled with bombs. When at proper position in relation to the target, the motor controlling the shaft 24 is put into operation and the bomb loaded pockets move successively toward the delivery chutes, the bombs feeding from the pockets into the chutes as indicated in Figs. 4 and The chutes, having had their lower ends adjusted to desired positions, then deliver these bombs in successive groups so that a multiplicity of bombs is rained from the airplane.
In Fig. there is illustrated the manner in which two bomb delivery mechanisms mounted on the same airplane may be effectively used. As shown in the left hand portion of Fig. 15, the delivery section has just discharged a number of bombs while the right hand section has discharged another group of bombs and it will be observed that each row of bombs in the right hand section is delivered intermediate the bombs in the left hand section so that a substantially continuous downpour of bombs is efiected. Also in Fig. 15 racks'are shown above the transverse member of the upper frame thus providing for storage of extra bombs and enabling the delivery chains to be loaded in flight.
In the construction shown in Fig. 11 if it is desired, handles may be applied to the members 47 so that they can be manually operated to open or close the bomb trays either singly or as a group.
It is to be understood that the bomb delivering devices may be made in sections which can be disassembled and removed from the plane when it is desired to use the airplane without bombing equipment of this character, the section thus being capable of assembly within the fuselage of the airplane.
While I have described the preferred embodiments of the invention and illustrated the same in the accompanying drawings, certain minor changes or alterations may appear to one skilled in the art to which this invention relates during the extensive manufacture of the same, and I, therefore, reserve the right to make such changes or alterations as shall fairly fall within the scope of the appended claim.
What is claimed, is:
In a bomb dispenser for airplanes, a pair of laterally spaced side frames each including an upper rail, pairs of sprocket wheels supported by said frames at the opposite ends thereof, said sprockets being coplanar with said side frames, endless chains running around said sprockets and having upper runs extending along and above said upper rails, tie bars connecting said chains and spaced therealong, bomb pockets fixed to said tie bars in laterally spaced relation, the pockets on the several bars being aligned one behind the other to form longitudinal rows, means to drive the sprockets at one end of said frames, rollers carried by said rails and supporting said upper runs, normally substantially disposed bomb chutes at one end of said frames and positioned to receive bombs from said pockets as the chains pass around the sprockets adjacent the bomb chutes to direct bombs into said chutes, each of said chutes including 'a rectangular top section outwardly flared and having a lip arcually inclined to ward' its adjacent pocket and cylindrical lower ends, means connected to said side frames for pivotally supporting the upper ends of said bomb chutes for lateral swinging adjustments of the lower ends of said chutes, and rack and pinion means connected between said side frames and otf-center chutes for transversely adjusting the lower ends of said off-center chutes.
7 References Cited in the file of this patent UNITED STATES PATENTS 315,712 Buckner Apr. 14, 1885 866,607 Weimer Sept. 17, 1907 1,423,854 Howard July 25, 1922 2,342,022 Trimbach Feb. 15, 1944 2,581,634 Coons Ian. 8, 1952
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US297731A US2741159A (en) | 1952-07-08 | 1952-07-08 | Master bomb rainer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US297731A US2741159A (en) | 1952-07-08 | 1952-07-08 | Master bomb rainer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2741159A true US2741159A (en) | 1956-04-10 |
Family
ID=23147522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US297731A Expired - Lifetime US2741159A (en) | 1952-07-08 | 1952-07-08 | Master bomb rainer |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2741159A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4171664A (en) * | 1978-02-13 | 1979-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Mine simulator planting rack and release mechanism |
| US4318328A (en) * | 1979-10-09 | 1982-03-09 | The Boeing Company | Removable external payload carrier for aircraft |
| US5763811A (en) * | 1997-04-04 | 1998-06-09 | The Boeing Company | Internal weapon carriage system for wide body aircraft |
| USD453547S1 (en) | 1999-04-01 | 2002-02-12 | Celsiustech Electronics Ab | Dispenser for counter means |
| CN109387113A (en) * | 2018-09-21 | 2019-02-26 | 陶文英 | The transmission ammunition belt system of dozen aircraft is examined by a kind of omnidirectional |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US315712A (en) * | 1885-04-14 | Aerial drop for explosives | ||
| US866607A (en) * | 1907-02-21 | 1907-09-17 | Edgar A Weimer | Apparatus for casting and delivering pig metal. |
| US1423854A (en) * | 1918-12-16 | 1922-07-25 | Commw Steel | Sand feeder |
| US2342022A (en) * | 1940-01-27 | 1944-02-15 | Curtiss Wright Corp | Aircraft bomb carrier |
| US2581634A (en) * | 1944-12-05 | 1952-01-08 | Fmc Corp | Pear feeding and orienting apparatus |
-
1952
- 1952-07-08 US US297731A patent/US2741159A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US315712A (en) * | 1885-04-14 | Aerial drop for explosives | ||
| US866607A (en) * | 1907-02-21 | 1907-09-17 | Edgar A Weimer | Apparatus for casting and delivering pig metal. |
| US1423854A (en) * | 1918-12-16 | 1922-07-25 | Commw Steel | Sand feeder |
| US2342022A (en) * | 1940-01-27 | 1944-02-15 | Curtiss Wright Corp | Aircraft bomb carrier |
| US2581634A (en) * | 1944-12-05 | 1952-01-08 | Fmc Corp | Pear feeding and orienting apparatus |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4171664A (en) * | 1978-02-13 | 1979-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Mine simulator planting rack and release mechanism |
| US4318328A (en) * | 1979-10-09 | 1982-03-09 | The Boeing Company | Removable external payload carrier for aircraft |
| US5763811A (en) * | 1997-04-04 | 1998-06-09 | The Boeing Company | Internal weapon carriage system for wide body aircraft |
| USD453547S1 (en) | 1999-04-01 | 2002-02-12 | Celsiustech Electronics Ab | Dispenser for counter means |
| USD470561S1 (en) | 1999-04-01 | 2003-02-18 | Saab Ab | Dispenser for counter means |
| CN109387113A (en) * | 2018-09-21 | 2019-02-26 | 陶文英 | The transmission ammunition belt system of dozen aircraft is examined by a kind of omnidirectional |
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