GB803722A - Vertical velocity meter - Google Patents
Vertical velocity meterInfo
- Publication number
- GB803722A GB803722A GB32324/56A GB3232456A GB803722A GB 803722 A GB803722 A GB 803722A GB 32324/56 A GB32324/56 A GB 32324/56A GB 3232456 A GB3232456 A GB 3232456A GB 803722 A GB803722 A GB 803722A
- Authority
- GB
- United Kingdom
- Prior art keywords
- output
- altimeter
- drum
- motor
- axis
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/62—Devices characterised by the determination or the variation of atmospheric pressure with height to measure the vertical components of speed
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Navigation (AREA)
Abstract
803,722. Measuring rate of climb. SPERRY RAND CORPORATION. Oct. 23, 1956 [Oct. 27, 1955], No. 32324/56. Class 40 (1). In a rate-of-climb indicator operated by integration of vertical acceleration cumulative errors are cancelled out by a signal derived from comparing the integrated accelerometer output with the differentiated output of an altimeter. In Fig. 1, a gyroscope rotor turns about an axis XX in a drum 8 which is eccentrically mounted on axis YY, the drum being balanced by weight 9 and spring 15 to be level when acted upon by gravity alone. Vertical acceleration (positive or negative) causes the drum to tilt about YY and this in turn induces precession of the frame 2 about the vertical axis ZZ. The tilt is detected by brushes 19 bearing on a contact segment 14, and these energize the winding 24 (Fig. 2) of motor 16 which rotates ring 4 in one direction or the other to oppose the precession and maintain the drum level. Stabilization of the whole apparatus is effected by gyroscope repeaters 21, 21<SP>1</SP> acting about the axes X<SP>1</SP>X<SP>1</SP> and Y<SP>1</SP>Y<SP>1</SP> respectively. The slider of potentiometer 28 is thus turned through an amount dependent on the velocity of climb and a signal output 34 (Fig. 2) is obtained from the transformer 92. The barometric altimeter 38 similarly produces an output from the E-type pick-up 32 which is amplified and differentiated in the motorgenerator unit 42, 46. Intermittent response of the altimeter is smoothed out by mechanical feedback through 44 and electrical feedback via 51. The integrated accelerometer output 34 is similarly smoothed in the unit 60 which comprises an amplifier feeding a motor controlling the slider of a mains-energized potentiometer 54. The signal from this is combined with a fraction of the output 34 and applied at 50 to a circuit 76 which is also supplied with the differentiated altimeter output at 48. The difference between the two signals is amplified and passed via 62 to the motor 18 which (Fig. 1) rotates the tilt axis of the drum 8 by an amount which compensates for the cumulative errors. A radio altimeter may be used instead of a barometric altimeter. The errors may be further reduced by introducing into the accelerometer output 34 a portion of the error signal applied to motor 18.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US803722XA | 1955-10-27 | 1955-10-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB803722A true GB803722A (en) | 1958-10-29 |
Family
ID=22156958
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32324/56A Expired GB803722A (en) | 1955-10-27 | 1956-10-23 | Vertical velocity meter |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB803722A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3296422A (en) * | 1962-02-12 | 1967-01-03 | Honeywell Inc | Apparatus for computing true vertical position, velocity and acceleration for aircraft |
CN110498038A (en) * | 2018-05-16 | 2019-11-26 | 贝尔直升机德事隆公司 | Rotor craft and its control method |
EP3575213A1 (en) * | 2018-06-01 | 2019-12-04 | Bell Helicopter Textron Inc. | System and method for controlling rotorcraft |
US11312480B2 (en) | 2018-06-01 | 2022-04-26 | Textron Innovations Inc. | System and method for controlling rotorcraft |
-
1956
- 1956-10-23 GB GB32324/56A patent/GB803722A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3296422A (en) * | 1962-02-12 | 1967-01-03 | Honeywell Inc | Apparatus for computing true vertical position, velocity and acceleration for aircraft |
CN110498038A (en) * | 2018-05-16 | 2019-11-26 | 贝尔直升机德事隆公司 | Rotor craft and its control method |
EP3575213A1 (en) * | 2018-06-01 | 2019-12-04 | Bell Helicopter Textron Inc. | System and method for controlling rotorcraft |
US10816999B2 (en) | 2018-06-01 | 2020-10-27 | Textron Innovations Inc. | System and method for controlling rotorcraft |
US11312480B2 (en) | 2018-06-01 | 2022-04-26 | Textron Innovations Inc. | System and method for controlling rotorcraft |
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