[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US3484951A - Control apparatus - Google Patents

Control apparatus Download PDF

Info

Publication number
US3484951A
US3484951A US617449A US3484951DA US3484951A US 3484951 A US3484951 A US 3484951A US 617449 A US617449 A US 617449A US 3484951D A US3484951D A US 3484951DA US 3484951 A US3484951 A US 3484951A
Authority
US
United States
Prior art keywords
pin
turret
ring
basket
disc
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 - Lifetime
Application number
US617449A
Inventor
Uwe Menzel
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.)
Honeywell GmbH
Original Assignee
Honeywell GmbH
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 Honeywell GmbH filed Critical Honeywell GmbH
Application granted granted Critical
Publication of US3484951A publication Critical patent/US3484951A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/04Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of land vehicles

Definitions

  • a basket which supports the tank crew and the devices which have to be submitted to the various movements, is cardanically supported within two concentric rings with a mechanism engaging the inner ring below the bottom of the basket and tilting this ring about its gimbal axis.
  • the inner dimensions and the equipment of the basket correspond to that of an actual tank.
  • a light training turret for motion together with the basket.
  • the driving mechanism includes a pin which is fixed to the inner ring and extends in the direction of the axis of that inner gimbal ring.
  • This pin is guided by means of a supporting disc which is rotatable about the same axis.
  • the pin supporting means can be displaced by controlled amounts away from the center of the disc. If the link between the pin and the disc is displaced from the disc center and the disc rotates about its center, the inner gimbal ring, including the basket and the training turret, carries out wobbled movements which are a combination of movements about the pitch and roll axis. In predetermined angular positions of the turret these wobble movements can be restricted to either pitch or roll movements. The amount of the displacement of the pin guiding means away from the center determines the amplitude of the motion.
  • the training turret with its circular track is supported rotatably by the inner gimbal ring.
  • an intermediate ring is mounted rotatably within and with respect to the inner gimbal ring and bears the circular track of the turret so that the turret can be rotated with respect to this intermediate ring. If the intermediate ring is rotated, it has the same influence on the turret and its crew as a rotation of tank about its vertical axis.
  • the crew can pivot the turret within the intermediate ring in such a manner that ice the orientation of the turret with respect to the terrain remains constant.
  • an intermediate ring one could use a rotatable supporting plate which carries the supporting pillars for the outer gimbal ring. Turning the turret about its yaw axis, then however, would require more energy. Such rotation of the turret about its yaw axis, of course, could also be simulated by feeding suitable disturbance signals into the azimuth aiming mechanism.
  • two spindles preferably threaded spindles, extending parallel to the supporting disc are used.
  • two spindle nuts Guided by these two spindles are two spindle nuts which bear a supporting piece for the pin which can be displaced out of its center position.
  • the supporting piece is rotatable about an axis which lies in the plane of the two spindles and cuts the spindles under angle.
  • the pin is guided within a hole of the plug support so that it can be moved axially and also can be rotated with respect to the guiding piece.
  • the rotation of the supporting disc about its center axis and the displacement of the guiding piece on the supporting disc or preferably accomplished by separate motors so that during the rotation of the supporting disc the amplitude of the wobble motion may be changed by means of displacing the supporting piece.
  • the training turret 1 with its basket 2 is with its circular track rotatably supported in the inner gimbal ring 3 of the training apparatus.
  • basket 2 is only schematically shown by four poles and a platform at the bottom. In practice the basket will be closed and support all equipment of a normal tank turret.
  • the inner gimbal ring 3 is supported pivotally at the outer ring 5 by means of two pins 4.
  • the two supporting pins 6 of the outer ring 5 are displaced with respect to that of the inner ring about 90 degrees and are born in two supporting pillars 7.
  • This cardanic support turret 1 can be tilted about any axis lying in the horizontal. plane through pins 6.
  • the tilting motion of the turret 1 is effected by means of a driving mechanism which engages the basket 2 below its bottom.
  • a pin 15 which extends in direction of the center axis of the inner gimbal ring 3.
  • the free end of pin 15 is guided within a guiding piece 13 which can be rotated about axle 16 and can be moved in a direction parallel to supporting disc 8 by means of two threaded spindles 10.
  • Guided by these spindles 10 are two spindle nuts 11 which bear axle 16.
  • this may be provided with a hole in which the pin 15 can be displaced axially as well as rotated.
  • Apparatus for simulating the motion of a tank about its pitch and roll axes as such tank is moving through the terrain comprising:
  • a basket for carrying the equipment and the crew; an inner and an outer concentric ring, the inner ring being attached to said basket, the outer ring being attached to support means, and the two rings being connected to each other for relative angular motion with respect to each other; and driving means for tilting said inner ring, said driving means including, a pin rigidly connected to the inner ring and extending along the direction normal to the plane of the ring, a pin guiding means attached to a rotatable supporting disc for engaging said pin in a manner which will determine its position relative to said disc but which Will leave it free to turn relative to said pin guiding means as the disc rotates, said pin guiding means being adjustable for various positions relative to said disc, and means for rotating said disc.
  • said pin is carried by a frame which surrounds the basket and is fixed to the inner ring.

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Toys (AREA)

Description

Dec. 23, 1969 u. MENZEL CONTROL APPARATUS Filed Feb. 10, 1967 INVENTOR. UWE MENZEL ATTORNEY United States Patent US. CI. 35-11 4 Claims ABSTRACT OF THE DISCLOSURE Apparatus for simulating the movements about pitch and roll axes of a tank traveling through a terrain.
BRIEF SUMMARY OF THE INVENTION For training a tank crew it is necessary to submit the crew during aiming exercises to the various movements of a tank traveling through a terrain, in order to exercise the correct reaction of the crew with respect to the various types of movements. Such training by means of a tank traveling through a terrain involves some disadvantages. In many casesno training area of suflicient size can be used. It is furthermore disadvantageous that such practice runs require a great quantity of fuel and that such training tanks often show essential wear. It, therefore, is desirable to train a tank crew by means of a simulator in a manner already done in pilot training. It is an object of this invention to disclose a suitable apparatus for simulating the movement of a tank about its pitch and roll axis by means of a training turret which is mounted stationary.
According to the invention a basket which supports the tank crew and the devices which have to be submitted to the various movements, is cardanically supported within two concentric rings with a mechanism engaging the inner ring below the bottom of the basket and tilting this ring about its gimbal axis. The inner dimensions and the equipment of the basket correspond to that of an actual tank. At the top of the basket here is mounted a light training turret for motion together with the basket.
According to a preferred embodiment of the invention, the driving mechanism includes a pin which is fixed to the inner ring and extends in the direction of the axis of that inner gimbal ring. This pin is guided by means of a supporting disc which is rotatable about the same axis. The pin supporting means can be displaced by controlled amounts away from the center of the disc. If the link between the pin and the disc is displaced from the disc center and the disc rotates about its center, the inner gimbal ring, including the basket and the training turret, carries out wobbled movements which are a combination of movements about the pitch and roll axis. In predetermined angular positions of the turret these wobble movements can be restricted to either pitch or roll movements. The amount of the displacement of the pin guiding means away from the center determines the amplitude of the motion.
The training turret with its circular track is supported rotatably by the inner gimbal ring. In order to submit the turret additionally to rotation about its vertical or yaw axis according to further improvement of the invention an intermediate ring is mounted rotatably within and with respect to the inner gimbal ring and bears the circular track of the turret so that the turret can be rotated with respect to this intermediate ring. If the intermediate ring is rotated, it has the same influence on the turret and its crew as a rotation of tank about its vertical axis. By means of the azimuth aiming mechanism the crew can pivot the turret within the intermediate ring in such a manner that ice the orientation of the turret with respect to the terrain remains constant. Instead of an intermediate ring one could use a rotatable supporting plate which carries the supporting pillars for the outer gimbal ring. Turning the turret about its yaw axis, then however, would require more energy. Such rotation of the turret about its yaw axis, of course, could also be simulated by feeding suitable disturbance signals into the azimuth aiming mechanism.
For displacing the pin support out of its center position according to a preferred embodiment of the invention, two spindles, preferably threaded spindles, extending parallel to the supporting disc are used. Guided by these two spindles are two spindle nuts which bear a supporting piece for the pin which can be displaced out of its center position. The supporting piece is rotatable about an axis which lies in the plane of the two spindles and cuts the spindles under angle. The pin is guided within a hole of the plug support so that it can be moved axially and also can be rotated with respect to the guiding piece. The rotation of the supporting disc about its center axis and the displacement of the guiding piece on the supporting disc, or preferably accomplished by separate motors so that during the rotation of the supporting disc the amplitude of the wobble motion may be changed by means of displacing the supporting piece.
Further features of the invention are disclosed in the claims and will become apparent from the following description of the embodiment as shown in the drawing.
DETAILED DESCRIPTION The training turret 1 with its basket 2 is with its circular track rotatably supported in the inner gimbal ring 3 of the training apparatus. In the drawing basket 2 is only schematically shown by four poles and a platform at the bottom. In practice the basket will be closed and support all equipment of a normal tank turret. The inner gimbal ring 3 is supported pivotally at the outer ring 5 by means of two pins 4. The two supporting pins 6 of the outer ring 5 are displaced with respect to that of the inner ring about 90 degrees and are born in two supporting pillars 7. By means of this cardanic support turret 1 can be tilted about any axis lying in the horizontal. plane through pins 6. The tilting motion of the turret 1 is effected by means of a driving mechanism which engages the basket 2 below its bottom.
For this purpose four support members 14, extending downwardly, are fixed to the inner gimbal ring 3 and are joined together below the bottom of basket 2. Fixed to these support members is a pin 15 which extends in direction of the center axis of the inner gimbal ring 3. The free end of pin 15 is guided within a guiding piece 13 which can be rotated about axle 16 and can be moved in a direction parallel to supporting disc 8 by means of two threaded spindles 10. Guided by these spindles 10 are two spindle nuts 11 which bear axle 16. By these means guiding piece 13 can be displaced away from its central position and the pin can move along its axis within the guiding hole of guiding piece 13. If now disc 8 is rotated by means of motor 9, the inner gimbal ring 3 and with it turret 1 and basket 2 carry out wobble motions about the two cardan axes 4-4 and 6-6. The more guiding piece 13 for pin 15 is displaced out of the central position the greater will be the amplitude of such wobble motion. Additionally, turret 1 and basket 2 can be rotated by means of the azimuth aiming mechanism and the circular track with respect to cardan ring 3.
For guiding pin 15 in the guiding piece 13 this may be provided with a hole in which the pin 15 can be displaced axially as well as rotated.
I claim:
1. Apparatus for simulating the motion of a tank about its pitch and roll axes as such tank is moving through the terrain, said apparatus comprising:
a basket for carrying the equipment and the crew; an inner and an outer concentric ring, the inner ring being attached to said basket, the outer ring being attached to support means, and the two rings being connected to each other for relative angular motion with respect to each other; and driving means for tilting said inner ring, said driving means including, a pin rigidly connected to the inner ring and extending along the direction normal to the plane of the ring, a pin guiding means attached to a rotatable supporting disc for engaging said pin in a manner which will determine its position relative to said disc but which Will leave it free to turn relative to said pin guiding means as the disc rotates, said pin guiding means being adjustable for various positions relative to said disc, and means for rotating said disc. 2. Apparatus according to claim 1 wherein said pin is carried by a frame which surrounds the basket and is fixed to the inner ring.
3. Apparatus according to claim 1 wherein the pin guiding means is supported by means of two parallel threaded spindles carried by said supporting disc.
4. Apparatus according to claim 3 wherein said pin guiding means is supported on an aXle extending between the two spindles and carried by two spindle nuts, said guiding means further having a central hole for engaging said pin.
References Cited UNITED STATES PATENTS 2,485,266 10/1949 Edinburg 3512 X 2,524,238 10/1950 Soule 35-12 X 2,930,144 3/1960 Fogarty 35l2 EUGENE R. CAPOZIO, Primary Examiner P. v. WILLIAMS, Assistant Examiner U.S. Cl. X.R.
US617449A 1967-02-10 1967-02-10 Control apparatus Expired - Lifetime US3484951A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61744967A 1967-02-10 1967-02-10

Publications (1)

Publication Number Publication Date
US3484951A true US3484951A (en) 1969-12-23

Family

ID=24473691

Family Applications (1)

Application Number Title Priority Date Filing Date
US617449A Expired - Lifetime US3484951A (en) 1967-02-10 1967-02-10 Control apparatus

Country Status (1)

Country Link
US (1) US3484951A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4136467A (en) * 1977-06-20 1979-01-30 Chrysler Corporation Means and method for imparting stabilization error to the line of sight of a simulator
US4564356A (en) * 1985-03-18 1986-01-14 The United States Of America As Represented By The Secretary Of The Army Laboratory turret shaker

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485266A (en) * 1944-07-14 1949-10-18 Link Aviation Inc Training apparatus
US2524238A (en) * 1946-11-15 1950-10-03 Jessie Chess Soule Flight trainer
US2930144A (en) * 1954-07-06 1960-03-29 Gen Precision Inc Grounded aircraft trainer

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485266A (en) * 1944-07-14 1949-10-18 Link Aviation Inc Training apparatus
US2524238A (en) * 1946-11-15 1950-10-03 Jessie Chess Soule Flight trainer
US2930144A (en) * 1954-07-06 1960-03-29 Gen Precision Inc Grounded aircraft trainer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4136467A (en) * 1977-06-20 1979-01-30 Chrysler Corporation Means and method for imparting stabilization error to the line of sight of a simulator
US4564356A (en) * 1985-03-18 1986-01-14 The United States Of America As Represented By The Secretary Of The Army Laboratory turret shaker

Similar Documents

Publication Publication Date Title
EP2810268B1 (en) Apparatus to simulate driving a land véhicle
US4487410A (en) Fluid suspended passenger carrying spherical body having universal attitude control
US4186922A (en) Football offensive player training apparatus
US4120099A (en) Apparatus for training the telecontrol of a model helicopter or the like
CN104091518B (en) A kind of solar system the eight major planets of the solar system demonstrator
US3484951A (en) Control apparatus
CN100487752C (en) Coriolis force experimental equipment
US2385291A (en) Training device
US4386726A (en) Adapter for socket welds
US3529354A (en) Control system for platform having six degrees of freedom
US2601729A (en) Atomic model machine
US3734613A (en) Orbital simulation facility
GB1260617A (en) Improvements in or relating to stabilized base mounts
US3561137A (en) Training apparatus with hydrostatic motion system
US3196558A (en) Means for visually indicating flight paths of vehicles between the earth, venus and mercury
CN203910172U (en) Solar system eight-planet demonstration instrument
US2319115A (en) Training device for aviators
US4507086A (en) Turret shaker mechanism
US2978961A (en) Overhead coverage gun mount
CN108613592B (en) Body feeling simulator of transmitting device
US2885791A (en) Celestial navigation trainer
US2360399A (en) Directional gyroscope and follow-up
CN110243468B (en) Simple flexible brightness imaging system
US3706141A (en) Orbiting system simulator
US3033975A (en) Welding apparatus