← Back to Patent Explorer
US4143548A Expired / Lapsed US ⏱️ 0.0 years remaining

Measuring the speed of an aircraft

Assignee: Vereinigte Flugtechnische Werke Fokker GmbH
•
Filing: 1977-10-26
•
Granted: 1979-03-13
•
Expires: 1997-10-26
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A continuous wave ultrasonic wave transmitter transmits modulated waves in two opposite directions being intercepted by a forward receiver and an aft receiver. The received signals are demodulated and the relative phase is used to obtain a speed reading. The wave length of the modulator signal must be larger than the two, preferably equal transmitter-to-receiver spacings. A similar but orthogonally arranged receiver system permits acquisition of a speed vector. Different modulation frequencies are to be used for different speed ranges; all these frequencies are transmitted simultaneously and selection of the desired one is made in the processing circuit only.

Inventors

  • 👤 Eberhard Graewe
  • 👤 Siegfried Krajeweski

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 21:09
CPC Classifications
G; G01; G01S; G01S15/00; G01S15/02; G01S15/50; G01S15/58; G01P; G01P5/00; G01P5/24; G01P5/245; G01P5/248

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 154 words
A system for measuring the speed of an aircraft having a longitudinal axis, comprising: an ultrasonic transmitter on the aircraft including means for continuously transmitting ultrasonic waves at least in two oppositely oriented directions along the longitudinal axis of the aircraft; means included in the transmitter for providing frequency modulation by at least one modulation frequency having a particular wavelength so that said ultrasonic signals as transmitted are frequency modulated by said modulation frequency; a pair of ultrasonic receivers respectively disposed to intercept the waves as transmitted by the transmitter in the said two opposite directions, said receivers being spaced from the transmitter by distances smaller than said wavelength; means included in the receivers for demodulating the signals as detected by the receivers; and means for determining the phases of demodulation signals as produced by the means for demodulating and for determining the speed of the aircraft on the basis of the determined phases.
Claim 2
Independent Claim 154 words
A system for measuring the speed of an aircraft having a longitudinal axis, comprising: an ultrasonic transmitter on the aircraft including means for continuously transmitting ultrasonic waves at least in two oppositely oriented directions along the longitudinal axis of the aircraft; means included in the transmitter for providing frequency modulation by at least one modulation frequency having a particular wavelength so that said ultrasonic signals as transmitted are frequency modulated by said modulation frequency; a pair of ultrasonic receivers respectively disposed to intercept the waves as transmitted by the transmitter in the said two opposite directions, said receivers being spaced from the transmitter by distances smaller than said wavelength; means included in the receivers for demodulating the signals as detected by the receivers; and means for determining the phases of demodulation signals as produced by the means for demodulating and for determining the speed of the aircraft on the basis of the determined phases.
Claim 3
Dependent Claim 30 words
A system as in claim 1, and including a second pair of receivers placed orthogonally to said pair, and circuit means connected to the receivers to obtain a speed vector.
Claim 4
Dependent Claim 44 words
A system as in claim 1, wherein the means for modulating provides plural modulation at different frequencies, said receivers including adjustable filters to select one frequency from the demodulation signals, a different frequency among the plural frequencies being selected for a different measuring range.

References Cited (Backward Citations)

US2274262A Cited
US2480646A Cited
US2515221A Cited
US3861211A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-03-12 1982-09-11 1983-03-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-03-12 1986-09-11 1987-03-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-03-12 1990-09-11 1991-03-13 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag