GB589177A - Improvements in or relating to mechanism for launching rocket projectiles - Google Patents

Improvements in or relating to mechanism for launching rocket projectiles

Info

Publication number
GB589177A
GB589177A GB2608444A GB2608444A GB589177A GB 589177 A GB589177 A GB 589177A GB 2608444 A GB2608444 A GB 2608444A GB 2608444 A GB2608444 A GB 2608444A GB 589177 A GB589177 A GB 589177A
Authority
GB
United Kingdom
Prior art keywords
projectile
moves
shoe
tube
launched
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
Application number
GB2608444A
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.)
HYDRAN PRODUCTS Ltd
Original Assignee
HYDRAN PRODUCTS Ltd
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 HYDRAN PRODUCTS Ltd filed Critical HYDRAN PRODUCTS Ltd
Priority to GB2608444A priority Critical patent/GB589177A/en
Publication of GB589177A publication Critical patent/GB589177A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01Feeding of unbelted ammunition
    • F41A9/24Feeding of unbelted ammunition using a movable magazine or clip as feeding element
    • F41A9/26Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine
    • F41A9/27Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine in revolver-type guns
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/03Shot-velocity control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/58Electric firing mechanisms
    • F41A19/64Electric firing mechanisms for automatic or burst-firing mode
    • F41A19/65Electric firing mechanisms for automatic or burst-firing mode for giving ripple fire, i.e. using electric sequencer switches for timed multiple-charge launching, e.g. for rocket launchers

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

589,177. Launching rockets. HYDRAN PRODUCTS, Ltd., and MOTLEY, L. Dec. 29, 1944, No. 26084. [Classes 92 (i)] and 92 (ii)] Rocket projectiles are fed one by one into the firing position at the rear end of a launching tube 1, Fig. 2, and means are provided for positively ensuring that each projectile cannot be fired until the preceding projectile has moved a given distance in its course. In the construction shown in Fig. 2, a cylindrical magazine 4 is disposed at the rear end of the tube and contains a spring-controlled feed element 5, having longitudinal blades forming housings for the projectiles 2. The lowermost projectile in the magazine is in alignment with the launching tube, and when in this position is fired automatically by mechanism such as that described in Specification 588,920. The spring 9, tending to rotate the feed element, surrounds the shaft 11 to which the element is connected and is secured at one end to the element and at the other to a bush 24 which, when in use, is locked against rotation in the magazine wall 8. The shaft 4, hence the feed element, is normally held against rotation by an escapement mechanism, comprising a twoarmed pivoted pawl 14, adapted to engage teeth on an escapement wheel 12, on the shaft 11. When a projectile is launched and has reached a point in the tube 1, it engages with and moves a timing lever 10 mounted on the same shaft 15 as the pawl 14. Such movement enables the feed element to move under the action of spring 9 to bring another projectile into line with the launching tube. In a modification, Figs. 4 and 5 (not shown), the lever 10 is replaced by a cap member which fits over a number of holes in the launching tube, the blast from a launched projectile serving to lift the member thereby to actuate the feed element as described above. In another modification, Fig. 6, the projectile when launched, depresses a pivoted shoe 30, which is connected by a rod 31 to the cocking mechanism to recock the striker, as in Specification 588,920. When the projectile has passed the shoe the latter moves upwards a short distance, where it is held by a spring-controlled latch 33. Thus the striker is not in a position to fire the next projectile. When, however, the launched projectile approaches the end of the tube, it moves a timing lever 34 on a rod 38, and an arm 39 on the rod depresses a pivoted lever 40 which, through a link 42, removes the latch from a notch 32 in shoe 30.- The shoe then returns to the position shown, and in doing so returns the striker to the firing position. A further modification, Fig. 7 (not shown), includes an electrical circuit, generally similar to that shown in Fig. 6 of Specification 588,920, but including two separate circuit making and breaking devices. As each projectile moves to its firing position it moves one of these devices through a step of its rotation to break the firing circuit, and as a launched projectile reaches the end of the launching tube it moves a shoe to produce a step of rotation of the other device to close the circuit.
GB2608444A 1944-12-29 1944-12-29 Improvements in or relating to mechanism for launching rocket projectiles Expired GB589177A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2608444A GB589177A (en) 1944-12-29 1944-12-29 Improvements in or relating to mechanism for launching rocket projectiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2608444A GB589177A (en) 1944-12-29 1944-12-29 Improvements in or relating to mechanism for launching rocket projectiles

Publications (1)

Publication Number Publication Date
GB589177A true GB589177A (en) 1947-06-13

Family

ID=10238094

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2608444A Expired GB589177A (en) 1944-12-29 1944-12-29 Improvements in or relating to mechanism for launching rocket projectiles

Country Status (1)

Country Link
GB (1) GB589177A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2764066A (en) * 1953-08-28 1956-09-25 Jr Robert A Doak Contact-latch type firing mechanism for rocket launchers
US2790352A (en) * 1951-03-08 1957-04-30 John L Jewett Spin stabilized rocket wing launcher
US2900874A (en) * 1948-09-18 1959-08-25 Lockheed Aircraft Corp Rocket launcher
US2965001A (en) * 1954-05-20 1960-12-20 William D Bobco Rocket launcher
US3134301A (en) * 1959-12-11 1964-05-26 Even Georges Francois Marie Gun loading apparatus
FR2402852A1 (en) * 1977-09-10 1979-04-06 Rheinmetall Gmbh ARMORED MORTAR IN STORE
GB2397114A (en) * 2003-01-10 2004-07-14 Ronald Anderson Garden Laser-guided tyre deflation dart system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2900874A (en) * 1948-09-18 1959-08-25 Lockheed Aircraft Corp Rocket launcher
US2790352A (en) * 1951-03-08 1957-04-30 John L Jewett Spin stabilized rocket wing launcher
US2764066A (en) * 1953-08-28 1956-09-25 Jr Robert A Doak Contact-latch type firing mechanism for rocket launchers
US2965001A (en) * 1954-05-20 1960-12-20 William D Bobco Rocket launcher
US3134301A (en) * 1959-12-11 1964-05-26 Even Georges Francois Marie Gun loading apparatus
FR2402852A1 (en) * 1977-09-10 1979-04-06 Rheinmetall Gmbh ARMORED MORTAR IN STORE
GB2397114A (en) * 2003-01-10 2004-07-14 Ronald Anderson Garden Laser-guided tyre deflation dart system

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