US2416028A - Release assembly for bomb shackles - Google Patents
Release assembly for bomb shackles Download PDFInfo
- Publication number
- US2416028A US2416028A US550025A US55002544A US2416028A US 2416028 A US2416028 A US 2416028A US 550025 A US550025 A US 550025A US 55002544 A US55002544 A US 55002544A US 2416028 A US2416028 A US 2416028A
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- US
- United States
- Prior art keywords
- bomb
- release
- indicated
- lever
- casing
- 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.)
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Definitions
- 'Ihis invention relates to the control mechanism for operating the bomb supporting hooks on a bomb shackle. It is designed particularly for the purpose of maintaining the releasing mechanism against accidental release of the bombs until the plane carrying the bombs is over the target. In some common forms of mechanism for this purpose it has happened that the releasing mechanism, by reason of sudden jars or other external causes, operates untimely.
- Fig. 1 is a side elevational view of a bomb shackle, partly in section, showing a release assembly attached thereto;
- Fig. 2 is a cross sectional view on line 2 2, Fig. 1;
- Fig. 3 is a cross sectional view on line 3--3, Fig. 1;
- Fig. 4 is an enlarged elevational view of the release assembly shown in Fig. 1, the parts being shown in locked position assumed before .the bomb has been released;
- Fig. 5 is a view similar to Fig. 4, showing the parts in position assumed when the bomb has been released;
- Fig. 6 is an elevational view of a portion of the release assembly showing the safety lever form; ing part of the bomb arming mechanism; and
- Fig. 7 is an enlarged side view partly in section showing the connection of the sear lever to the plunger of the solenoid.
- Fig. 1 of the drawings I have shown a conventional type of bomb shackle. This structure is not in itself new, nor does it form any part of the present invention any more than to illustrate the working of the release assembly.
- I0 indicates one side plate of a frame to which is attached a similar plate (not shown) by means of bolts or studs II.
- I2 indicates the bomb hooks
- the release assembly for the bomb shackle consists of the following interengaging elements.
- the cocking arm 28 is pivotally connected by means of a pin 30 to -the outer end of an actuating rod or plunger indicated at 32.
- This rod 32 is slidably mounted in guides 34 and 35 formed as parts of a casing 36 which houses the release assembly and which is mounted on the bomb shackle structure by means of bolts and studs indicated at 38.
- the inner end of the actuating rod 32 is slotted to receive the upper end cf a rod locking lever indicated at 4I). This lever is slotted at its upper end as indicated at 4I to receive a pin 42 secured in the slotted .inner end of the actuating rod or plunger.
- the lower nd of the rod locking lever 4I] is formed with a toe 43, the corner of which, in the position shown in Fig; 1, engages in a notch 44 formed in one end of a release lever 45 which is pivotally mounted in the casing by means of a pin indi cated at 45.
- the other end of the releasing lever or scar ispivotally connected by means ofa pin 48 to the end of a plunger-49 of a solenoid indicated at 50, which solenoid may be termed -the bomb shackle release solenoid.
- the endg-'ofi the lever 45 engageable with the toe 43 on the lever 40 is yieldingly held in such engagement by means of a flat spring indicated at 52, one end of which is secured in the casing by means of a stud indicated at 53.
- a compression spring indicated at 55 is mounted on the actuating rod 32, one end of which engages the guide 35 and the other end of which engages a shoulder E formed on the actuating rod 32.
- This spring 55 tends to move the actuating rod in a left-hand direction and thereby through the connection of the slotted end of the rod 32 and the pin 42 to the lever 4U to firmly hold the toe 43 on the lever 40 in. the notch 44 of the lever 45.
- the spring 55 tends to move the actuating rod to the left and thereby operates the arm 28 to release the bomb shackle.
- a safety hook indicated at 62- which is pivotally mounted upon a stud or bolt indicated at 63 mounted in the casing.
- This safety arm is yieldingly held in the position shown in Fig. 1 by means of a coiled spring indicated at 64 which is attached to and extends from the arm 62 to a portion of the casing as shown in Fig. 6, the arm being limited in its movement by means of pins or bolts indicated at 61 and 68.
- a fuse release or arming hook indicated at 69 pivotally mounted on the stud or bolt 63. This hook is yieldingly held clear of the throat El by means of a coiled spring indicated at 1D,
- the position of parts indicated ⁇ in Fig. 1 are in the relation assumed whenv the bomb shackle is carrying the bomb and when in this position the safety hook 62 is nin engagement with the ring G of the bomb arming mechanism.
- the aviator wishes to drop the bomb armed, he, through suitable electrical connections, energizes the bomb arming solenoid l5. This causes the plunger of the solenoidto be retracted and through the connecting mechanism described pull the fuse release hook 69 .across the throat below the safety hook 62 into the position shown in Fig. 4.
- The'bomb release solenoid- 5D is then energized through suitable electrical connections and the core retracted, thereby pulling the release lever 45 into the position shown in Fig. 5 of the drawings.
- the actuating rod locking lever 4B s'free to moveinto the positionv shown irl-Fig. 5
- the safety lever 62 is moved clear of the throat 6I and as the bomb drops away the ring 64 of the fuse connection is caught by the fuse release hook 69 and the fuse is set.
- the safety hook 62 is moved clear of the throat or notch 6I just referred to by means of a foot formed on a yoke 8l which engages in an annular groove 82 in the actuating rod 32 as shown in Fig. 2.
- This foot 80 engages the upper end 83 of the safety hook 62 and swings the hook free of the throat. This movement of the safety hook also performs another function,
- a release assembly for bombshackles comprising: a casing; an actuating rod slidably mounted in the casing; spring means on said rod for yieldably moving said rod outwardly; a rod locking lever pivotally mounted ⁇ in said casing; means on said actuating rod engaging one end of said rod locking lever; a release lever pivotally mounted in said casing; said release lever having a notch in one end engaged by the adjacent end of the rod locking lever; spring means mounted in said casing for yieldably holding the release lever in engagement with the rod locking ⁇ lever; a solenoid in said casing, a movable plunger in the solenoid, means for pivotally connecting the plunger to the other end of the release lever; said casing having an open throat in the lower portion of the casing; a safety hook pivotally mounted in the casing extending across said throat; spring means for yieldingly holding said safety hook across the said throat; a fuse release hook pivotally mounted in said casing; spring means for yieldingly holding said fuse release hookfree of the said throat; a bomb
Description
l. SLOAN RELEASE ASSEMBLYl FOR BOMB SHACKLES Feb. 18, 1947.
2 Sheets-Sheet l Filed Aug. 1a, 1944 Feb. 18, 1947. D, SLOAN 2,416,028
RELEASE ASSEMBLY FOR BOMB SHACKLES Filed Aug. 18, 1944 2 Sheets-Sheet 2 69 61 6,2 a4 s .5g
Daft/AL@ Z S2 amv I N V EN TOR.
A Trae/v5 Y Patented Feb. 18, 1947 RELEASE ASSEMBLY FOR BOMB SHACKLES Donald I. Sloan, Los Angeles, Calif., assignor to Interstate Aircraft and Engineering Corp., a corporation of California Application August 18, 1944, Serial No. 550,025
'Ihis invention relates to the control mechanism for operating the bomb supporting hooks on a bomb shackle. It is designed particularly for the purpose of maintaining the releasing mechanism against accidental release of the bombs until the plane carrying the bombs is over the target. In some common forms of mechanism for this purpose it has happened that the releasing mechanism, by reason of sudden jars or other external causes, operates untimely.
It is an object of this invention to produce a release assembly for bomb shackles of simple form and construction in which the mechanism is so arranged that accidental operation of the releasing mechanism is obviated.
It is another object of this invention to provide a release assembly for -bomb shackles of simple form and construction which is positive in operation and which operates in conjunction with and coincident with what is commonly referred to as the bomb arming mechanism.
Other objects and advantages will appear hereinafter from the following description and drawings.
Referring to the drawings, which are for illustrative purposes only:
Fig. 1 is a side elevational view of a bomb shackle, partly in section, showing a release assembly attached thereto;
Fig. 2 is a cross sectional view on line 2 2, Fig. 1;
Fig. 3 is a cross sectional view on line 3--3, Fig. 1;
Fig. 4 is an enlarged elevational view of the release assembly shown in Fig. 1, the parts being shown in locked position assumed before .the bomb has been released;
Fig. 5 is a view similar to Fig. 4, showing the parts in position assumed when the bomb has been released;
Fig. 6 is an elevational view of a portion of the release assembly showing the safety lever form; ing part of the bomb arming mechanism; and
Fig. 7 is an enlarged side view partly in section showing the connection of the sear lever to the plunger of the solenoid.
Referring more particularly to Fig. 1 of the drawings, I have shown a conventional type of bomb shackle. This structure is not in itself new, nor does it form any part of the present invention any more than to illustrate the working of the release assembly.
I0 indicates one side plate of a frame to which is attached a similar plate (not shown) by means of bolts or studs II. I2 indicates the bomb hooks,
1 Claim. (Cl. 89-1.5)
each of which is pivotally mounted on its respective pin or bolt I3. These hooks, when carrying the bomb as in the position shown, close recesses indicated at I4 formed in the side walls III of the bomb shackle. The two jaws I2 are connected by a linkage indicated at I5, such connection being a pivotal connection by reason of pins I6. The linkage I5 is provided with a foot indicated at vI'I which engages an abutment I8 formed on a lever I9 pivotally mounted on a bolt or stud `2!) supported in the side walls of the bomb shackle.
In the position of the parts shown in Fig, 1, the bomb is being carried and the parts are locked in the bomb carrying position. The free end 2I' of the lever I9 extends into a recess 22 formed in a pivoted arm 23, such arm being mounted upon or on a stud or bolt indicated at 24. Pivotally connected to the free end of the arm 23 is a link 26 which is-also pivotally connected to a cooking arm 28, such arm being pivotally mounted on a stud or bolt 29. The portion of the mechanism described above constitutes the mechanism of the bomb shackle proper. j
The release assembly for the bomb shackle consists of the following interengaging elements. The cocking arm 28 is pivotally connected by means of a pin 30 to -the outer end of an actuating rod or plunger indicated at 32. This rod 32 is slidably mounted in guides 34 and 35 formed as parts of a casing 36 which houses the release assembly and which is mounted on the bomb shackle structure by means of bolts and studs indicated at 38. It will be noted that by arranging the shackle release mechanism as a self-contained assembly in a casing detachably secured to the shackle structure, the advantage is secured that if the release mechanism breaks down, the casing and contained mechanism can be readily removed and replaced by another with very little loss of time, The inner end of the actuating rod 32 is slotted to receive the upper end cf a rod locking lever indicated at 4I). This lever is slotted at its upper end as indicated at 4I to receive a pin 42 secured in the slotted .inner end of the actuating rod or plunger. The lower nd of the rod locking lever 4I] is formed with a toe 43, the corner of which, in the position shown in Fig; 1, engages in a notch 44 formed in one end of a release lever 45 which is pivotally mounted in the casing by means of a pin indi cated at 45. The other end of the releasing lever or scar ispivotally connected by means ofa pin 48 to the end of a plunger-49 of a solenoid indicated at 50, which solenoid may be termed -the bomb shackle release solenoid. The endg-'ofi the lever 45 engageable with the toe 43 on the lever 40 is yieldingly held in such engagement by means of a flat spring indicated at 52, one end of which is secured in the casing by means of a stud indicated at 53.
Mounted on the actuating rod 32 is a compression spring indicated at 55, one end of which engages the guide 35 and the other end of which engages a shoulder E formed on the actuating rod 32. This spring 55 tends to move the actuating rod in a left-hand direction and thereby through the connection of the slotted end of the rod 32 and the pin 42 to the lever 4U to firmly hold the toe 43 on the lever 40 in. the notch 44 of the lever 45. The spring 55, as stated above, tends to move the actuating rod to the left and thereby operates the arm 28 to release the bomb shackle.
In devices of the kind herein referred to it is desirable to provide for the arming of the bomb as it is released from the bomb shackle. This is usually done by providing mechanism which coacts with the bomb shackle which engages a ring attached to a cable, which cable is attached tothe fuse. of the bomb. This construction of the ring and cable being common, merely the ring is indicated in the drawings. yThe ring just referred to is indicated at 6U, and while the bomb is being carried it normally assumes the position indicate-d in Fig. 1 within a throat or notch indicated at 6| formed in the walls of the casing 36. It is retained in this position during normal operations by means of a safety hook indicated at 62- which is pivotally mounted upon a stud or bolt indicated at 63 mounted in the casing. This safety arm is yieldingly held in the position shown in Fig. 1 by means of a coiled spring indicated at 64 which is attached to and extends from the arm 62 to a portion of the casing as shown in Fig. 6, the arm being limited in its movement by means of pins or bolts indicated at 61 and 68. Also pivotally mounted on the stud or bolt 63 is a fuse release or arming hook indicated at 69. This hook is yieldingly held clear of the throat El by means of a coiled spring indicated at 1D,
which spring also is attached to the casing 36. Attached also to the hook t!! by means of a pin 1l is a link 12 pivotally connected at 13 to the plunger 14 of what I have termed a bomb arming solenoid 15.
As stated heretofore, the position of parts indicated` in Fig. 1 are in the relation assumed whenv the bomb shackle is carrying the bomb and when in this position the safety hook 62 is nin engagement with the ring G of the bomb arming mechanism. When the aviator wishes to drop the bomb armed, he, through suitable electrical connections, energizes the bomb arming solenoid l5. This causes the plunger of the solenoidto be retracted and through the connecting mechanism described pull the fuse release hook 69 .across the throat below the safety hook 62 into the position shown in Fig. 4. The'bomb release solenoid- 5D is then energized through suitable electrical connections and the core retracted, thereby pulling the release lever 45 into the position shown in Fig. 5 of the drawings. When in this, position the actuating rod locking lever 4B s'free to moveinto the positionv shown irl-Fig. 5
and is caused to move into such positionby rea- 23 releases the-leverl'andnpermits'the weight;
4 of the bombs to open the hooks l2, thereby releasing the bombs.
During the outward movement of the actuating rod or plunger 32 just described, the safety lever 62 is moved clear of the throat 6I and as the bomb drops away the ring 64 of the fuse connection is caught by the fuse release hook 69 and the fuse is set. The safety hook 62 is moved clear of the throat or notch 6I just referred to by means of a foot formed on a yoke 8l which engages in an annular groove 82 in the actuating rod 32 as shown in Fig. 2. This foot 80 engages the upper end 83 of the safety hook 62 and swings the hook free of the throat. This movement of the safety hook also performs another function,
vas follows, the curved end 84 of the hook engages .the end of aslide indicated at 85 of a slide switch indicated at 8S which switch is electrically connected to the bomb shackle release solenoid 50 and by such movement the bomb shackle release solenoid and bomb arming solenoid 15 are de-energized, arming hook 69A thereby freeing ring 60.
Although one form of the invention has been particularly shown and described, it is contemplated that various. changes. and modifications can be made without departing from the scope of the invention and it is intended to cover such changes and modifications as come within the scope of the appended claim.
I claim as my invention:
A release assembly for bombshackles comprising: a casing; an actuating rod slidably mounted in the casing; spring means on said rod for yieldably moving said rod outwardly; a rod locking lever pivotally mounted` in said casing; means on said actuating rod engaging one end of said rod locking lever; a release lever pivotally mounted in said casing; said release lever having a notch in one end engaged by the adjacent end of the rod locking lever; spring means mounted in said casing for yieldably holding the release lever in engagement with the rod locking` lever; a solenoid in said casing, a movable plunger in the solenoid, means for pivotally connecting the plunger to the other end of the release lever; said casing having an open throat in the lower portion of the casing; a safety hook pivotally mounted in the casing extending across said throat; spring means for yieldingly holding said safety hook across the said throat; a fuse release hook pivotally mounted in said casing; spring means for yieldingly holding said fuse release hookfree of the said throat; a bomb arming solenoid in said casing, a movable plungerin said solenoidpivotally connected to said fuse release hook; and a foot on said actuating rod engageable with said safety .hook to move said safety hook clear of the said throat. DONALD I. SLOAN.
REFERENCES CITED The following references are of record in the le of this patent:
UNITED STATES PATENTS v Date Number Name 4v2,341,456 Markey et al. Feb. 8,'1944 2,362,210 Mar-key e Nov. '7, 1944 f FQRE'IGN PATENTS Number CountryV Date 422,274- Vickers-Armstrongs
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US550025A US2416028A (en) | 1944-08-18 | 1944-08-18 | Release assembly for bomb shackles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US550025A US2416028A (en) | 1944-08-18 | 1944-08-18 | Release assembly for bomb shackles |
Publications (1)
Publication Number | Publication Date |
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US2416028A true US2416028A (en) | 1947-02-18 |
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Application Number | Title | Priority Date | Filing Date |
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US550025A Expired - Lifetime US2416028A (en) | 1944-08-18 | 1944-08-18 | Release assembly for bomb shackles |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2473597A (en) * | 1945-09-27 | 1949-06-21 | George H Leland | Bomb shackle and release |
US2571381A (en) * | 1946-03-13 | 1951-10-16 | Ainsworth Mfg Corp | Bomb release mechanism |
US2604353A (en) * | 1941-12-22 | 1952-07-22 | Vickers Armstrongs Ltd | Bomb slip, towing gear, and analogous releasable attachments |
US2756091A (en) * | 1951-10-29 | 1956-07-24 | Ainsworth Mfg Corp | Military stores rack |
US2776570A (en) * | 1954-06-22 | 1957-01-08 | Electro Seal Corp | Electro-mechanical actuator |
US4049222A (en) * | 1976-07-20 | 1977-09-20 | The United States Of America As Represented By The Secretary Of The Air Force | Ejector rack for nuclear stores |
US4922799A (en) * | 1988-05-03 | 1990-05-08 | Messerschmitt-Boelkow-Blohm Gmbh | Apparatus for suspending, strapping, and launching a flying body from a carrier |
US11465744B2 (en) * | 2020-02-03 | 2022-10-11 | Alkan | Aeronautical conveying and release device |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB422274A (en) * | 1932-03-14 | 1933-12-14 | Vickers Armstrongs Ltd | Improvements in or relating to devices for carrying bombs and other heavy bodies on and releasing them from aircraft |
US2341456A (en) * | 1942-01-20 | 1944-02-08 | Pollak Mfg Company | Bomb releasing shackle |
US2362210A (en) * | 1941-08-07 | 1944-11-07 | Pollak Mfg Company | Bomb releasing shackle |
-
1944
- 1944-08-18 US US550025A patent/US2416028A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB422274A (en) * | 1932-03-14 | 1933-12-14 | Vickers Armstrongs Ltd | Improvements in or relating to devices for carrying bombs and other heavy bodies on and releasing them from aircraft |
US2362210A (en) * | 1941-08-07 | 1944-11-07 | Pollak Mfg Company | Bomb releasing shackle |
US2341456A (en) * | 1942-01-20 | 1944-02-08 | Pollak Mfg Company | Bomb releasing shackle |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2604353A (en) * | 1941-12-22 | 1952-07-22 | Vickers Armstrongs Ltd | Bomb slip, towing gear, and analogous releasable attachments |
US2473597A (en) * | 1945-09-27 | 1949-06-21 | George H Leland | Bomb shackle and release |
US2571381A (en) * | 1946-03-13 | 1951-10-16 | Ainsworth Mfg Corp | Bomb release mechanism |
US2756091A (en) * | 1951-10-29 | 1956-07-24 | Ainsworth Mfg Corp | Military stores rack |
US2776570A (en) * | 1954-06-22 | 1957-01-08 | Electro Seal Corp | Electro-mechanical actuator |
US4049222A (en) * | 1976-07-20 | 1977-09-20 | The United States Of America As Represented By The Secretary Of The Air Force | Ejector rack for nuclear stores |
US4922799A (en) * | 1988-05-03 | 1990-05-08 | Messerschmitt-Boelkow-Blohm Gmbh | Apparatus for suspending, strapping, and launching a flying body from a carrier |
US11465744B2 (en) * | 2020-02-03 | 2022-10-11 | Alkan | Aeronautical conveying and release device |
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