Doppler radar velocity measurement horn

• US 4,660,050 A
• Filed: 04/06/1983
• Issued: 04/21/1987
• Est. Priority Date: 04/06/1983
• Status: Expired due to Fees

• Current Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Original Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Phillips, Oliver A.
• Primary Examiner(s): Lieberman, Eli
• Application Number:
  US06/482,527
• Time in Patent Office: 1,476 Days
• Field of Search: 343/7 UM, 343/8, 343/9, 343/713, 343/754, 343/912, 343/753, 343/786
• US Class Current: 343/753
• CPC Class Codes: F16F 15/08 with rubber springs grommet- or bushing-type resilient mountings F16F1/3732, F16F1/38; with springs made of rubber and metal arrangement of internal-combustion or jet-propulsion units B60K5/12; mounting of propulsion plants on vessels B63H21/30; mounting of vehicle drivers' cabs B62D33/0604
• CPC Class Codes: G01S 13/60 wherein the transmitter and receiver are mounted on the moving object, e.g. for determining ground speed, drift angle, ground track G01S13/64 takes precedence
• CPC Class Codes: H01Q 19/08 for modifying the radiation pattern of a radiating horn in which it is located corrugated horns H01Q13/0208; producing a circular polarisation H01Q13/0241

Abstract

Doppler radar apparatus for use in a velocity measuring system for farm tractors and the like. The apparatus includes a dual mode conical horn having a flare angle substantially in excess of 12.5°, and a dielectric lens formed of a glass filled polymer. The doppler output signal provided by the RF transceiver associated with the dual mode horn is high pass filtered to remove low frequency signals therefrom. The horn is mounted in such a way that it is isolated from mechanical vibrations which would induce doppler signal frequencies in excess of the cutoff frequency of the high pass filter. Moreover, the horn assembly (which is aluminum) and a steel housing assembly are coupled together in such a way that thermal expansion and contraction will not loosen the friction fit between the two assemblies. The two assemblies are held together by a single, large diameter annular locking ring.

Claims

1. Apparatus for use in a doppler radar velocity measurement system, comprising

means including a rectangular waveguide for generating an RF wave in said rectangular waveguide, said RF wave having a frequency in the range of 24 GHz,

waveguide transformer means for providing a smooth RF transition between said rectangular waveguide and a circular waveguide,

a circular pyramidal horn antenna having a flared section with a mouth and a throat, said horn also including a circular waveguide section formed at the throat of said flared section, said circular waveguide being coupled to said waveguide transformer for receiving said RF wave from said waveguide transformer and being dimensioned so that said RF wave can propogate in only the TE₁₁ mode, mode generator means disposed at the junction of said circular waveguide and the throat of said flared section for generating a TM₁₁ mode RF wave, said flared section guiding both RF wave modes from said mode generator means into free space, wherein said flared section has an interior mouth diameter of about 4.4 inches and a flare angle of about 39°

so that the length of said flared section is only about 5.3 inches, and

a dielectric lens positioned across the mouth of said flared section, said RF lens being spaced axially from the mouth of said horn so as to reduce the standing wave ratio in said horn, and having a focal length corresponding approximately to its axial spacing from the phase center of said horn antenna.

2. Apparatus for use in a doppler radar velocity measurement system, comprising

a microwave horn assembly for receiving and transmitting an RF electromagnetic wave, said assembly providing an electrical doppler signal having a frequency equal to the difference between the frequencies of said transmitted and received waves,

electronic filter means responsive to said doppler signal provided by said microwave horn assembly for high pass filtering said signal to provide an output signal that includes only frequencies above a predetermined cutoff frequency, and

means for resiliently mounting said microwave horn assembly on a vehicle, said resilient mounting means having spring rate and damping characteristics such that said microwave horn assembly is isolated from low level vibrations having frequencies which would produce doppler signals with frequencies greater than the cutoff frequency of the high pass filter means, whereby erroneous doppler signals produced by horn vibrations are effectively eliminated.

3. Apparatus as set forth in claim 2, wherein said resilient mounting means includes (a) at least two annular vibration isolators encircling and firmly engaging said microwave horn assembly at two axially spaced locations along said assembly, and (b) rigid means engaging said vibration isolators for attaching the isolators to said vehicle.

4. Apparatus as set forth in claim 3, wherein said resilient mounting means further includes a spacer tube arranged between and abutting with said vibration isolators, and wherein said horn assembly includes (a) at least two discrete components, each having a radially extending surface adapted to abut a corresponding one of two circumferential surfaces on opposing axial ends of said resilient mounting means and spacer tube arrangement, and (b) means for fastening said first and second parts axially together when assembled with said resilient mounting means and spacer tube arrangement.

5. Apparatus as set forth in claim 4, wherein said fastening means comprises complementary inner and outer circumferential threads on said two discrete components, said threads permitting said components to be screwed axially together.

6. Apparatus as set forth in claim 3, wherein each vibration isolator includes a thin frustoconical annulus of resilient material, first means coupled to the radially inner perimeter of said frustoconical annulus for providing a surface for engaging said horn assembly, and second means coupled to the radially outer perimeter of said frustoconical annulus for providing a surface for engaging said rigid mounting means.

7. Apparatus as set forth in claim 6, wherein said first and second surface providing means comprise first and second rigid rings to which said resilient material is bonded.

8. Apparatus as set forth in claim 7, wherein said frustoconical annuli of resilient material in the two vibration isolators are oriented in opposite directions, and wherein said resilient mounting means further comprises means for axially spacing said two first concentric rings from one another by a first amount and said two second concentric rings from one another by a second amount, said first and second amounts being such that each said frustoconical annulus is slightly buckled.

9. Apparatus as set forth in claim 7, wherein the first and second rigid rings of each of said vibration isolators have radially facing portions which are formed of resilient material and which are disposed at overlapping axial locations such that sudden mechanical shocks causing momentary collapse of said frustoconical annuli are absorbed by the resilient impact of said resilient facing portions of said first and second rings.

10. Apparatus as set forth in claim 9 wherein each said ring is composed of a resilient material but has a rigid ring adjoined thereto to provide dimensional stability.

11. Apparatus for use in a doppler velocity measurement system, comprising

a microwave horn assembly for transmitting and receiving an RF electromagnetic wave and providing a doppler signal having a frequency related to the velocity of the vehicle to which the system is attached, and

a housing assembly for housing said horn assembly, said housing assembly being formed of a structural material having a coefficient of thermal expansion which is different than the coefficient of thermal expansion of the material of which said horn assembly is formed, said housing assembly having interior surfaces which abut matching exterior surfaces of said microwave horn assembly,

wherein the planes of said surfaces are all selected to be parallel to the direction of movement of the material underlying said surfaces due to thermal expansion or contraction, whereby unequal thermal expansion or contraction of said materials of which said assemblies are formed causes said abutting surfaces to move parallel to one another rather than normal to one another.

12. Apparatus as set forth in claim 11 wherein said microwave horn assembly is aluminum and said housing assembly is steel.

13. Apparatus as set forth in claim 11, wherein said microwave horn assembly is generally cylindrical and has two frustoconical surfaces coaxial with said generally cylindrical horn assembly, wherein said surfaces have equal and opposite degrees of obliquity relative to said axis such that, if said surfaces were extended to form cones, the cones would be similar and would have a common apex disposed between them along the axis, and wherein said housing assembly has matching surfaces which abut said surfaces of said horn assembly.

14. Apparatus as set forth in claim 13, wherein each of said frustoconical surfaces is on a different part of said horn assembly, wherein said parts are adapted to be assembled with said housing assembly by being inserted axially through different ends of said housing assembly until said frustoconical surfaces of said parts meet the corresponding surfaces of said housing assembly, and wherein means are included for fastening said two parts together in the assembled position.

15. Apparatus as set forth in claim 14, wherein said fastening means draws said parts together axially, thereby insuring a tight friction fit between said surfaces of said assemblies.

16. Apparatus as set forth in claim 13 wherein said two frustoconical surfaces are on respective first and second parts of said microwave horn assembly, and where one of said parts carries coaxial outer threads and the other of said parts carries matching coaxial inner threads, whereby said horn assembly and housing assembly are assemblable by inserting said first and second parts axially through different ends of said housing assembly and screwing said two parts axially together until a tight friction fit is formed between said matching frustoconica1 surfaces of said housing assembly and said first and second parts.

17. Apparatus for use in a doppler radar velocity measurement system, comprising:

means for generating a dual mode RF electromagnetic wave and for guiding said wave to a horn;

a conical horn having a small diameter end and a large diameter end and being coupled adjacent its smaller diameter end to said generating means for transmitting said dual mode RF wave into free space, said horn having a flare angle substnatially in excess of 12.5°

;

lens means covering the large diameter end of said horn, said lens means having a focal length substantially equal to the distance from the phase center of said horn to said lens;

said generating means including microwave transceiver means for generating said RF wave and for receiving said RF wave back again after reflection from an obstacle, said transceiver means providing a doppler signal having a frequency equal to the frequncey difference between said generated and received RF waves;

high pass filter means for filtering said doppler signal to eliminate all frequencies in said doppler signal below a selected cutoff frequency; and

resilient means for mounting said generating means, horn and lens means on a vehicle, said resilient means having characteristics selected such that said generating means is isolated from low level vibrations having frequencies which would produce doppler signal frequencies in excess of the cutoff frequency of said high pass filter means.

18. Apparatus as set forth in claim 17, wherein said flare angle is in excess of 25°

.

19. Apparatus as set forth in claim 17, wherein said lens is formed of a glass filled polymer.

20. Apparatus as set forth in claim 17, wherein said lens is formed of 40% glass filled polyester.

21. Apparatus as set forth in claim 17, wherein said generating means provides an RF wave having a frequency in the range of 24 GHz, and wherein said horn has length of about 5.3 inches and an interior diameter at its large diameter end of about 4.4 inches.

22. Apparatus for use in a doppler radar velocity measurement system, comprising:

means for generating a dual mode RF electromagnetic wave and for guiding said wave to a horn;

a conical horn having a small diameter end and a large diameter end and being coupled adjacent its smaller diameter end to said generating means for transmitting said dual mode RF wave into free space, said horn having a flare angle substantially in excess of 12.5°

, said horn and generating means are part of a microwave horn assembly;

lens means covering the large diameter end of said horn, said lens means having a focal length substantially equal to the distance from the phase center of said horn to said lens; and

a housing for said horn assembly, said housing being fabricated of a material having a coefficient of thermal expansion different from the coefficient of thermal expansion of a material of which said horn assembly is formed, said housing having interior surfaces which abut corresponding exterior surfaces of said horn assembly, said abutting interior and exterior surfaces being aligned at angles to a central longitudinal axis of the horn assembly selected so that expansion and contraction of the materials caused by temperature variation will produce movement of said abutting surfaces parallel to one another rather than normal to one another.

23. Apparatus as set forth in claim 22, wherein said flare angle is in excess of 25°

.

24. Apparatus as set forth in claim 22, wherein said lens is formed of a glass filled polymer.

25. Apparatus as set forth in claim 22, wherein said lens is formed of 40% glass filled polyester.

26. Apparatus as set forth in claim 22, wherein said generating means provides an RF wave having a frequency in the range of 24 GHz, and wherein said horn has length of about 5.3 inches and an interior diameter at its large diameter end of about 4.4 inches.

27. Apparatus for use in a doppler radar velocity measurement system, comprising:

means for generating an RF electromagnetic wave having a frequency of at least 24 GHz and for guiding said wave to a horn;

a horn coupled to said generating means for transmitting said RF wave into free space;

a dielectric lens covering the mouth of said horn, said lens being formed of a glass filled polymer material; and

said means for generating an RF electromagnetic wave comprises means for generating a wave in the dominant TE₁₁ mode and wherein said horn includes means responsive to said TE₁₁ mode RF wave for producing a TM₁₁ mode RF wave therefrom, whereby the generated RF wave propagates through said horn in both the dominant TE₁₁ and the higher order TM₁₁ modes.

28. Apparatus for use in a doppler radar velocity measurement system, comprising:

means for generating an RF electromagnetic wave and for guiding said wave to a horn;

a horn coupled to said generating means for transmitting said RF wave into free space;

a dielectric lens covering the mouth of said horn, said lens being formed of a glass filled polymer material;

said generating means comprises microwave transceiver means for generating said RF wave and for receiving said RF wave back again after reflection from an obstacle, said transceiver means providing a doppler signal having a frequency equal to the frequency difference between said generated and received RF waves;

high pass filter means for filtering said doppler signal to eliminate all frequencies therein below a selected cutoff frequency; and

resilient means for mounting said generating means, horn and lens means on a vehicle, said resilient means having characteristics selected such that said generating means is isolated from low level vibrations having frequencies which would produce doppler signal frequencies in excess of the cutoff frequency of said high pass filter means.

29. Apparatus for use in a doppler radar velocity meansurement system, comprising:

means for generating an RF electromagnetic wave and for guiding said wave to a horn;

a horn coupled to said generating means for transmitting said RF wave into free space, said horn and said generating means are part of a microwave horn assembly;

a dielectric lens covering the mouth of said horn, said lens being formed of a glass filled polymer material; and

a housing for said microwave horn assembly, said housing being fabricated of a material having a coefficient of thermal expansion different from the coefficient of thermal expansion of a material of which said microwave horn assembly is formed, said housing having interior surfaces which abut matching exterior surfaces of said horn assembly, said abutting interior and exterior surfaces being aligned at an angle to a central longitudinal axis of the horn assembly selected so that expansion and contraction of the materials which is caused by temperature variations will produce movement of said abutting surfaces parallel to one another rather than normal to one another.