US4331032A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Variometers
Assignee: Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
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Filing: 1980-01-21
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Granted: 1982-05-25
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Expires: 2000-01-21
Abstract
Abstract A variometer for an aerodyne. The variometer has at least one dial conventionally graduated to represent speed, a needle indicating on said graduation the instantaneous vertical speed. The variometer also has an indicator which is representative of the potential vertical speed, and can move around the dial so that the position of the indicator with respect to the needle indicates instantaneously the acceleration on the trajectory of the aircraft.
Inventors
- 👤 Jean-Luc Sicre
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 23:34
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0615; G01; G01P; G01P3/00; G01P3/62
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
126 words
An improved variometer system for an aircraft having a dial with graduations representative of speed, comprising: a. means for determining the instantaneous vertical speed of the aircraft; b. means, responsive to said determining means, for displaying the instantaneous vertical speed of the aircraft, including a needle for indicating the instantaneous vertical speed on said graduations; c. means for determining the potential vertical speed of the aircraft, which is based on the total kinetic and potential energy of the aircraft; and d. at least one indicator, responsive to said determining means of potential vertical speed, for displaying potential vertical speed, said indicator being movable around the dial and the position of which with respect to said needle indicates the instantaneous acceleration on the trajectory of the aircraft.
Claim 2
Dependent Claim
126 words
An improved variometer system for an aircraft having a dial with graduations representative of speed, comprising: a. means for determining the instantaneous vertical speed of the aircraft; b. means, responsive to said determining means, for displaying the instantaneous vertical speed of the aircraft, including a needle for indicating the instantaneous vertical speed on said graduations; c. means for determining the potential vertical speed of the aircraft, which is based on the total kinetic and potential energy of the aircraft; and d. at least one indicator, responsive to said determining means of potential vertical speed, for displaying potential vertical speed, said indicator being movable around the dial and the position of which with respect to said needle indicates the instantaneous acceleration on the trajectory of the aircraft.
Claim 3
Dependent Claim
20 words
An improved variometer as claimed in claim 1, including a digital display means for indicating the gradient of the aircraft.
Claim 4
Dependent Claim
97 words
A system as claimed in claim 1, including means for generating a signal representative of the instantaneous vertical speed h* o which is used in the variometer, said signal being obtained by the calculation, ##EQU8## in which h* o is the signal of instantaneous vertical speed, h o A is a signal of vertical speed possibly coming from a central anemometric unit, τ 1 is a time constant, τ 2 is a time constant, S is the Laplace operator, J z is the component of acceleration on the vertical axis, and g is the acceleration of gravity.
Claim 5
Dependent Claim
139 words
A system as claimed in claim 3, comprising a circuit having: a. a direct chain, the input of which receives a signal representative of the expression (J z -g), comprising an integrator having a transfer function 1/S, the output of which provides the signal h* o of instantaneous vertical speed; and b. a counter-feedback loop comprising a first subtractor receiving a signal h o A of vertical speed, the output of said first subtractor connected to a transfer function integrator 1/(τ 1 τ 2 S) and also to an amplifier (τ 1 +τ 2 )/(τ 1 ×τ 2 ), said integrator and said amplifier being arranged in parallel and coupled by their outputs to two inputs of an adder which is serially connected to a second adder in the direct chain, before the integrator of the transfer function 1/S.
Claim 6
Dependent Claim
65 words
A system as claimed in claim 1, including means for generating a signal representative of the potential vertical speed h o T of an aircraft to activate said indicator, in which the signal is obtained by the calculation, ##EQU9## in which h o is the vertical speed, g is the acceleration of gravity, and Vx is the ground speed provided by a central inertial unit.
Claim 7
Dependent Claim
70 words
A system as claimed in claim 1, including means for generating a signal representative of the potential vertical speed h o T of an aircraft for activating said indicator in which the signal is obtained by the calculation, ##EQU10## in which Va is the air speed, Vx is the anomemetric speed, τ3 is a time constant, of approximately 10 seconds, and τ4 is a time constant, of approximately 3 seconds.
Claim 8
Dependent Claim
44 words
A variometer as claimed in claim 1, said indicator including the emitting ends of at least one bundle of a set of bundles of optic fibres wherein the other ends are connected to a set of lamps, with one lamp being provided per bundle.
Claim 9
Dependent Claim
22 words
A variometer as claimed in claim 1, said indicator being activated by the emitting ends of two adjacent bundles of optic fibres.
Claim 10
Dependent Claim
122 words
A system as claimed in claim 1, in which the signals representative of h o *, h o T , γS and the total gradient γ T are processed in a central unit which receives, from a central anemometric unit, signals representative of the air speed Va and of the vertical speed of the aircraft h o A , and also, from an inertial platform signals representative of the acceleration J z and of the ground speed Vx, the transfer of the value h o * to the variometer being by analog signals, and the transfer of digital information representative of the values of h o T and γS, which are displayed digitally on the variometer, is by a parallel multiplexed bus.
Claim 11
Dependent Claim
115 words
A variometer as claimed in claim 9, the processing means for the signals representative of h o *, h o T and γS comprising an analog converter receiving signals from an inertial platform and from a central anemometric unit which supplies signals for the parameters Va, h o A , J z and Vx to said central unit which processes the signals h o *, h o T and γS and transmits digital signals for h o T and γ ground to a sequencer connected to the leads of said bus and also, signals for h o *, to a selector connected to a linear/logarithmic converter then to a digital/analog converter connected to said variometer.
Claim 12
Dependent Claim
31 words
A variometer as claimed in claim 10, in which the signals h* T and γS provided by the central unit are sampled and transmitted sequentially to the leads of the bus.
Claim 13
Dependent Claim
27 words
A variometer as claimed in claim 11, in which transmission sequence comprises a pulse representative of γ ground and two pulses representative of h o T .
Claim 14
Dependent Claim
84 words
A variometer as claimed in claim 10, in which said selector is also connected to a circuit providing signals for the delayed vertical speed h o =h o A/(1+τS) and also switching means effecting the control of said selector in order to transmit to the variometer said signals for the delayed vertical speed, in the case of a malfunction of the central unit and, also a signal cancelling the indicator and digital display of the variometer, and displaying a signal indicative of the breakdown.
Claim 15
Dependent Claim
51 words
A variometer as claimed in claim 10, comprising in the central anemometric unit, a digital signal of vertical speed h o A , a safety circuit comprising, in the variometer, switching means for controlling the needle directly by said digital signal, the decimal/logarithmic conversion being accomplished mechanically by a conventional cam.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-05-24 | 1985-11-23 | 1986-05-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-05-24 | 1989-11-23 | 1990-05-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-05-24 | 1993-11-23 | 1994-05-25 | $7700.00 | Window Closed / Lapsed |