GB215300A - Improvements in apparatus for gun mounting laying and sighting arrangements for artillery on aeroplanes - Google Patents

Improvements in apparatus for gun mounting laying and sighting arrangements for artillery on aeroplanes

Info

Publication number
GB215300A
GB215300A GB18678/23A GB1867823A GB215300A GB 215300 A GB215300 A GB 215300A GB 18678/23 A GB18678/23 A GB 18678/23A GB 1867823 A GB1867823 A GB 1867823A GB 215300 A GB215300 A GB 215300A
Authority
GB
United Kingdom
Prior art keywords
sight
frame
trunnions
gun
target
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
GB18678/23A
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.)
Scheider & Cie
Original Assignee
Scheider & Cie
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 Scheider & Cie filed Critical Scheider & Cie
Publication of GB215300A publication Critical patent/GB215300A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/02Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
    • B64D7/06Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms movably mounted
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G5/00Elevating or traversing control systems for guns
    • F41G5/14Elevating or traversing control systems for guns for vehicle-borne guns
    • F41G5/18Tracking systems for guns on aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Balance (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

215,300. Schneider et Cie. May 3, 1923, [Convention date]. Addition to 195,371. Sights and methods of sighting.- The means described in the parent Specification for mounting, laying and sighting guns on aircraft is modified to suit the case where the. aircraft fiies at a constant altitude in a vertical plane passing at a certain distance from the target. The invention is shown in Figs. 1 and 2 applied to the mounting described in Figs. 7 to 14 of -the parent Specification, in which the gun cradle C is trunnioned at c in a frame B which can ba inclined transversely on trunnions b mounted in a frame A trainable on a ring A<1>. The sight E, the entry prism of which has correcting movements applied thereto to suit tangent elevation and longitudinal component of wind as described in the parent Specification, is mounted in a box D which is adjusted round the trunnion b by a worm gear A<2> on the frame A which operates on an arm D<1> extending from the box. This arm is connected to an arm C<2> extending from the trunnion c by a link F, ball-joint f and adjustable pin G. The operation of the gear A<2> to bring the sight on to the target therefore, through the link F, sets the gun in the inclined plane passing through the line of flight and the target, the angle of inclination i being measured on a scale H by a pointer I. The gun is then moved independently of the sight to correct for altitude, angle i, and wind by operating the gear c<3> to adjust the pin G and set one of the marks I<1>, I<2>, I<3>, Fig. 5, to that part of the appropriate height scale 1, 2, 3, which corresponds to the angle i shown by the pointer I on the scale H<1>. To correct for wind, a preliminary adjustment of the scale H is made by turning a worm H<4> to the reading of a mark a<5> on a wind scale H<2>. After these initial adjustments, the gun is elevated, whilst the sight is kept on the target, by turning a wheel d<2>, the elewating-pinions B<2> being turned by a worm geaa- B<4> geared to the sight elevating shaft D<4>. During this elevation of the gun about the inclined trunnions c, the frame B receives a correcting movement about the trunnions b through the medium of the connection F, G In a modification, Fig. 9, the sight box D is fixed to the frame B and the entry prism is deviated by linkage L, M to bring the sight on to the target during the transverse movement of the frame B about the trunnions b effected bv operating a worm gear J. The length of the link L is varied by graduated screw-drums U, V to suit the altitude and wind respectively. During the elevation of the gun about the inclined trunnions c, effected by a worm gear B<5>, the sight is kept on the target by the compensating movement imparted to the frame B by a worm gear A'. In a further modification, Fig. 22, the sight is mounted on the trainable frame A in which the frame B is trunnioned at b for elevation purposes. The transverse, inclination of the gun is effected by moving the cradle. C on trunnions c in the frame B by operating a worm X<4> to rock a bell-crank X<2> the upper arm of which is connected to the cradle by arcuate slides X, C<5>. The rotation of the shaft X<3> is communicated to the entry prism of the sight E to bring the sight on the target. The slide X is adjustable on the arm X<2> for wind correction by a worm gear X<5>. When the gun is elevated about the trunnions b, the arcuate slide X imparts a compensating movement to the cradle about the trunnions c. In this construction, further transverse corrections may be applied by mounting the frame A on longitudinal trunnions.
GB18678/23A 1923-05-03 1923-07-19 Improvements in apparatus for gun mounting laying and sighting arrangements for artillery on aeroplanes Expired GB215300A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR215300X 1923-05-03

Publications (1)

Publication Number Publication Date
GB215300A true GB215300A (en) 1924-07-17

Family

ID=8881152

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18678/23A Expired GB215300A (en) 1923-05-03 1923-07-19 Improvements in apparatus for gun mounting laying and sighting arrangements for artillery on aeroplanes

Country Status (2)

Country Link
US (1) US1638962A (en)
GB (1) GB215300A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011106489B4 (en) * 2011-06-14 2019-03-28 Mbda Deutschland Gmbh Load carrier for an aircraft
CN110510122B (en) * 2019-08-22 2024-06-18 成都立航科技股份有限公司 Six-degree-of-freedom adjusting mechanism of load mounting vehicle

Also Published As

Publication number Publication date
US1638962A (en) 1927-08-16

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