GB1078806A – Improvements in devices for controlling operation of an aerial bomb
– Google Patents
GB1078806A – Improvements in devices for controlling operation of an aerial bomb
– Google Patents
Improvements in devices for controlling operation of an aerial bomb
Info
Publication number
GB1078806A
GB1078806A
GB31113/64A
GB3111364A
GB1078806A
GB 1078806 A
GB1078806 A
GB 1078806A
GB 31113/64 A
GB31113/64 A
GB 31113/64A
GB 3111364 A
GB3111364 A
GB 3111364A
GB 1078806 A
GB1078806 A
GB 1078806A
Authority
GB
United Kingdom
Prior art keywords
parachute
recess
spring
bomb
sleeve
Prior art date
1963-08-05
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
Application number
GB31113/64A
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.)
1963-08-05
Filing date
1964-08-04
Publication date
1967-08-09
1964-08-04
Application filed by Individual
filed
Critical
Individual
1967-08-09
Publication of GB1078806A
publication
Critical
patent/GB1078806A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
Classifications
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42—AMMUNITION; BLASTING
F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
F42C14/00—Mechanical fuzes characterised by the ammunition class or type
F42C14/06—Mechanical fuzes characterised by the ammunition class or type for fall bombs
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
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
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
B64D1/06—Bomb releasing; Bombs doors
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42—AMMUNITION; BLASTING
F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type
Abstract
1,078,806. Dropping bombs. R. A. ROBERT Aug. 4, 1964 [Aug. 5, 1963], No. 31113/64. Headings F3A and F3C [Also in Division F2] A bomb attached to an aircraft is connected to a parachute. The connection is in the inoperative condition as long as the bomb is not effectively released but assumes the operative condition as soon as the bomb is released. The connection is shown in Fig. 4 the bomb being attached to sleeve 32 and the parachute being -connected to the yoke 108. The latter is integral with a piston 81 which is connectible to the sleeve 32 by balls 84 being forced into groove 86 by a sheath 106 which is loaded by a spring 105 and the movement of which is controlled by a rod 41 and cap 57. When the bomb is in place on the aircraft, cap 57 abuts the bottom of the bomb dropping gear and is held in the position shown so that the rod 41 is prevented from moving upwards under the influence of spring 46 by balls 64 held in holes 65 abutting shoulders 61. The, arms of the yoke 42, Fig. 10, integral with the rod 41 connect the piston 81, sheath 106 and sleeve 33 by holding balls 74 to 77 in recess 78 of the piston. If the parachute is untimely extracted a spring spider 96 is deformed and the assembly formed by piston 81, sheath 106 and sleeve 89 is withdrawn from the sleeve 32. However, when the bomb is dropped the cap 57 moves upwardly under the influence of spring 69 permitting the ball 64 to be forced outwardly into recess 71 and thus allow the rod 41 to move upwardly. The yoke 42 allows the balls 74 to 77 to drop to the bottom of casing 112 so that springs 102 and 105 can move the piston 81 and sheath 106 to the left, sheath 106 being locked in position by engagement of recess 135 with split ring 134 to hold the balls 84 in engagement with recesses 86 to operatively connect the parachute to the bomb. At the same time as the rod 41 moves upwardly a timing device starts which controls the release of the parachute and the activation of the bomb fuze. A pin 161 normally prevents rotation of a spring-loaded cup 152 having a pinion 156 secured thereto but when the rod 41 moves upwards the pin 161 moves to a portion of the hub 157 of larger diameter so that the pinion 156 rotates under the action of the spring- loading. The pinion 156 drives gear 165, Fig. 13, having a drum 170 rotating therewith. A lever 174 pivoted at 175 bears on the inner periphery 172 of the drum. A nose 178, Fig. 15, on a disc 179 co-operates with a bead 177 on the lever 174 and a flat portion 183 of the disc shaft 180 co-operates with a spring-loaded plunger 185. The latter slides in a bore of a sleeve 189 connected to a cable 191 which controls the release of the parachute. The sleeve 189 is held in the position shown by balls 195 held in recess 196
GB31113/64A
1963-08-05
1964-08-04
Improvements in devices for controlling operation of an aerial bomb
Expired
GB1078806A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
FR943777A
FR1439831A
(en)
1963-08-05
1963-08-05
Apparatus for controlling the operation of an aerial bomb
Publications (1)
Publication Number
Publication Date
GB1078806A
true
GB1078806A
(en)
1967-08-09
Family
ID=8809915
Family Applications (2)
Application Number
Title
Priority Date
Filing Date
GB38183/66A
Expired
GB1078807A
(en)
1963-08-05
1964-08-04
Improvements in devices for the control of the fall of an aerial bomb
GB31113/64A
Expired
GB1078806A
(en)
1963-08-05
1964-08-04
Improvements in devices for controlling operation of an aerial bomb
Family Applications Before (1)
Application Number
Title
Priority Date
Filing Date
GB38183/66A
Expired
GB1078807A
(en)
1963-08-05
1964-08-04
Improvements in devices for the control of the fall of an aerial bomb
Country Status (5)
Country
Link
US
(1)
US3299810A
(en)
DE
(1)
DE1428803A1
(en)
FR
(1)
FR1439831A
(en)
GB
(2)
GB1078807A
(en)
NL
(1)
NL136335C
(en)
Cited By (2)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
FR2443663A1
(en)
*
1978-08-31
1980-07-04
Matra
Bomb for dropping by aircraft – has light alloy body and is armed upon leaving aircraft and reaching given speed
FR2654505A1
(en)
*
1989-11-14
1991-05-17
Diehl Gmbh & Co
ARTILLERY PROJECTILE SUBMUNITION.
Families Citing this family (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
DE2745454C2
(en)
*
1977-10-08
1983-11-17
Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen
Arrangement for targeting a bomb dropped by an aircraft
FR2457219A1
(en)
*
1979-05-23
1980-12-19
Thomson Brandt
DEVICE AND METHOD FOR TRANSPORTING AND RELEASING A PLURALITY OF LOADS CONTAINED IN A SINGLE CONTAINER, AND CONTAINER EQUIPPED WITH SUCH A DEVICE
USD748433S1
(en)
*
2014-10-07
2016-02-02
Urban Trend Llc
Beverage holder
Family Cites Families (7)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2377587A
(en)
*
1939-03-30
1945-06-05
James H Strong
Low altitude bomb
US2709961A
(en)
*
1951-03-19
1955-06-07
Harold W Klas
Parachute release device
US2723876A
(en)
*
1951-07-21
1955-11-15
Technical Service Inc
Parachute release
US2845024A
(en)
*
1953-01-08
1958-07-29
Jr Robert E Greene
Safety arming device
US2796284A
(en)
*
1953-02-18
1957-06-18
Charles J Benson
Flush release device for external stores
US2969212A
(en)
*
1956-08-31
1961-01-24
Martin James
Apparatus for ejecting bodies from a parent aerodyne
US3087695A
(en)
*
1961-09-20
1963-04-30
Jr James H Potts
Parachute pack opening mechanism
1963
1963-08-05
FR
FR943777A
patent/FR1439831A/en
not_active
Expired
1964
1964-07-29
DE
DE19641428803
patent/DE1428803A1/en
active
Pending
1964-07-30
US
US386279A
patent/US3299810A/en
not_active
Expired – Lifetime
1964-08-04
GB
GB38183/66A
patent/GB1078807A/en
not_active
Expired
1964-08-04
GB
GB31113/64A
patent/GB1078806A/en
not_active
Expired
1965
1965-06-14
NL
NL6507589A
patent/NL136335C/xx
active
Cited By (2)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
FR2443663A1
(en)
*
1978-08-31
1980-07-04
Matra
Bomb for dropping by aircraft – has light alloy body and is armed upon leaving aircraft and reaching given speed
FR2654505A1
(en)
*
1989-11-14
1991-05-17
Diehl Gmbh & Co
ARTILLERY PROJECTILE SUBMUNITION.
Also Published As
Publication number
Publication date
NL6507589A
(en)
1966-12-15
DE1428803A1
(en)
1969-02-27
NL136335C
(en)
1972-08-15
FR1439831A
(en)
1966-05-27
GB1078807A
(en)
1967-08-09
US3299810A
(en)
1967-01-24
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