GB408803A - Quotient or mean speed indicator - Google Patents

Quotient or mean speed indicator

Info

Publication number
GB408803A
GB408803A GB9774/33A GB977433A GB408803A GB 408803 A GB408803 A GB 408803A GB 9774/33 A GB9774/33 A GB 9774/33A GB 977433 A GB977433 A GB 977433A GB 408803 A GB408803 A GB 408803A
Authority
GB
United Kingdom
Prior art keywords
spindle
wheel
cam
gear
rotated
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
GB9774/33A
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.)
FRANCOIS MARIE MICHEL BERNARD
Original Assignee
FRANCOIS MARIE MICHEL BERNARD
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 FRANCOIS MARIE MICHEL BERNARD filed Critical FRANCOIS MARIE MICHEL BERNARD
Publication of GB408803A publication Critical patent/GB408803A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P11/00Measuring average value of speed

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Transmission Devices (AREA)
  • Gears, Cams (AREA)
  • Switches With Compound Operations (AREA)

Abstract

408,803. Average speed indicators. SALOMON, F. M. M. B., 3, Rue de l'Universite, and GOVARE, H. P., 4, Rue Guy de Maupassant, both in Paris. Oct. 20, 1932, No. 9774/33. Convention date, Dec. 7, 1931. Divided on 408,702. [Classes 106 (iii) and 106 (iv).] The calculation of the average speed is performed by a four-sided pivoted-link system in apparatus of the kind in which the primary elements of a differential gear are controlled by cams giving displacements proportional to the logarithms of space and time respectively as disclosed in Specification 283,175, [Class 106 (iii)], the cam system having been disclosed in Specification 349,338. In the apparatus shown diagrammatically in Fig. 1, the foursided link system comprises two equal links SD, SE movable independently about the point S and connected respectively to two equal links DF, EF, the pin F being slidable in a slot R in an arm pivoted also about the point S and operating a pointer 60 which indicates directly the mean speed during any period from zero setting. The points D move in circles lying in parallel planes and start in opposite directions f<1>1, f<1>2 from a common zero, the movement of the point D being effected by a spiral cam rotated, for example, by the wheels of a vehicle. The point E is similarly moved by a spiral cam from a clock. In the constructional form of the apparatus shown in Fig. 4, the distance cam 65 is driven at reduced speed through worm gearing 86, 87, a vertical spindle 88 and toothed gearing 89, 90, 91. The spindle 88 can be moved out axially to disengage the worm gear 86, 87 and then rotated by the knob 102, to return the distance cam 65 to zero. The time cam 65<1> is rotated by a spring and is controlled by an escapement, the cam being secured to a spindle, which carries the gear wheel 94, and the inner end of a spring contained in the fixed barrel 92. The wheel 94 meshes with a wheel (not shown) mounted on a spindle carrying the wheel 98 which is in constant engagement with the wide gear wheel 99 on the end of the time zeroizing spindle 100. When the spindle 100 is pushed inwards by the knob 101, the gear wheel 99 meshes with gear wheel 97 connected by the wheel 96 and a series of wheels (not shown) with an escapement, so that the time cam 65<1> is then rotated by the spring at a definite speed. When the spindle 100 is withdrawn, as shown, the gear wheel 99 is clear of the wheel 97 and the escapement is disconnected so that the gear wheel 94 may be rotated by rotation of the knob 101 thus winding up the spring and zeroizing the time cam. To prevent back rotation of the gear wheel 94 during the winding, the gear 99 is connected by gearing 103, 105 to a ratchet wheel 108 engaged by a pawl which is put out of action by a cone 107 on the spindle 100 when the spindle is pushed in to put the escapement in gear. Specification 408,884 also is referred to.
GB9774/33A 1931-12-07 1932-10-20 Quotient or mean speed indicator Expired GB408803A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE408702X 1931-12-07

Publications (1)

Publication Number Publication Date
GB408803A true GB408803A (en) 1934-04-19

Family

ID=3869192

Family Applications (2)

Application Number Title Priority Date Filing Date
GB29411/32A Expired GB408702A (en) 1931-12-07 1932-10-20 Speed indicator
GB9774/33A Expired GB408803A (en) 1931-12-07 1932-10-20 Quotient or mean speed indicator

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB29411/32A Expired GB408702A (en) 1931-12-07 1932-10-20 Speed indicator

Country Status (2)

Country Link
FR (1) FR744191A (en)
GB (2) GB408702A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2543872A (en) * 1947-12-30 1951-03-06 Link Aviation Inc Computer for aviation trainers and the like
US2551440A (en) * 1948-11-30 1951-05-01 Kreitner John Computing apparatus
US2602244A (en) * 1947-03-27 1952-07-08 Link Aviation Inc Computer for aviation trainers and the like
US2652195A (en) * 1951-02-27 1953-09-15 Raytheon Mfg Co Correction device for function generators
US2652978A (en) * 1951-03-14 1953-09-22 Raytheon Mfg Co Multiplication and division linkage operator

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2602244A (en) * 1947-03-27 1952-07-08 Link Aviation Inc Computer for aviation trainers and the like
US2543872A (en) * 1947-12-30 1951-03-06 Link Aviation Inc Computer for aviation trainers and the like
US2551440A (en) * 1948-11-30 1951-05-01 Kreitner John Computing apparatus
US2652195A (en) * 1951-02-27 1953-09-15 Raytheon Mfg Co Correction device for function generators
US2652978A (en) * 1951-03-14 1953-09-22 Raytheon Mfg Co Multiplication and division linkage operator

Also Published As

Publication number Publication date
GB408702A (en) 1934-04-19
FR744191A (en) 1933-04-13

Similar Documents

Publication Publication Date Title
FR2442433B1 (en)
GB408803A (en) Quotient or mean speed indicator
US2603940A (en) Horological apparatus
US1948946A (en) Combined odometer and oiling indicator
GB460008A (en) Improvements in or relating to testing apparatus for gear wheels
GB709775A (en) Improvements in or relating to timepieces
GB842516A (en) Improvements relating to backlash-free drive gearings
US1589462A (en) Attachment for micrometers
US2285856A (en) Means for evaluating and indicating the average value of successive time observations
US2265635A (en) Variable rate gearing for vending machines
DE1277564B (en) Device for measuring the distance traveled by a vehicle in a specific direction
US2144949A (en) Route indicating device
US2324560A (en) Navigational timepiece and setting mechanism
SU96436A1 (en) The device for determining the course angle of the moving crew
GB489232A (en) Improvements in aircraft instruments
US2468269A (en) Radio direction finding equipment
DE840314C (en) Pendulum Sextant
US1075998A (en) Tachometer.
GB774498A (en) Improvements in or relating to taximeters
GB1058195A (en) Improvements relating to indicating devices
USRE15348E (en) Joseph f
GB474178A (en) Improvements in or relating to speed indicators for aircraft or other moving bodies
GB479398A (en) Apparatus with a plurality of driving shafts for the control of aircraft landing gear
GB474718A (en) Improvements in and connected with the ascertaining and the indicating of the speed and position of vehicles (including aircraft, submarines, ships); and with the automatic correction of the latitude-speed-course error of gyro-compasses
GB351973A (en) Improvements in and relating to the measurement of electrical energy