GB168837A - Improvements in or relating to projectiles particularly for use on aircraft - Google Patents

Improvements in or relating to projectiles particularly for use on aircraft

Info

Publication number
GB168837A
GB168837A GB479/18A GB47918A GB168837A GB 168837 A GB168837 A GB 168837A GB 479/18 A GB479/18 A GB 479/18A GB 47918 A GB47918 A GB 47918A GB 168837 A GB168837 A GB 168837A
Authority
GB
United Kingdom
Prior art keywords
aircraft
base
projectiles
relating
sleeve
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
GB479/18A
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.)
VICENTE ALMONACID
Original Assignee
VICENTE ALMONACID
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 VICENTE ALMONACID filed Critical VICENTE ALMONACID
Publication of GB168837A publication Critical patent/GB168837A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B25/00—Fall bombs

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

168,837. Almonacid, V. Jan. 8, 1917, [Convention date]. Void [Published under Sect. 91 of the Act]. Projectiles.-A heavy bomb of high explosive powder, intended to be dropped from aircraft, is made by uniting two ordinary artillery shells a, b, base to base. Nose and rear fuzes f, h, with screw arming-devices k, l, are provided, and a tail consisting of a cylindrical sleeve e is attached. The sleeve, which has triangular openings n for the passage of air, holds the two shells together, e.g. by its frictional fit, cr by having its inner end crimped over the driving-band d of the shell a.
GB479/18A 1917-01-08 1918-01-08 Improvements in or relating to projectiles particularly for use on aircraft Expired GB168837A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR168837X 1917-01-08

Publications (1)

Publication Number Publication Date
GB168837A true GB168837A (en) 1921-09-12

Family

ID=8877166

Family Applications (1)

Application Number Title Priority Date Filing Date
GB479/18A Expired GB168837A (en) 1917-01-08 1918-01-08 Improvements in or relating to projectiles particularly for use on aircraft

Country Status (1)

Country Link
GB (1) GB168837A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101578492B (en) * 2006-12-21 2012-12-05 桑布尔河桥机械车间公司 Shrouded penetrating aerial bomb

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101578492B (en) * 2006-12-21 2012-12-05 桑布尔河桥机械车间公司 Shrouded penetrating aerial bomb

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