US4716763A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Jet flow in an angular velocity sensor
Assignee: RTX Corp
•
Filing: 1984-10-22
•
Granted: 1988-01-05
•
Expires: 2004-10-22
Abstract
Abstract An angular velocity sensor utilizing the Coriolis effect on a fluid jet employs increased spacing between the sensing elements to increase the scale factor and to reduce flow disturbances. A metal diaphragm pump is utilized to improve the ability to control the flow rate. Flow disturbances are further reduced by using a single, symmetrical central flowhole, eliminating curtain holes, and providing only two discharge paths oriented 180° apart.
Inventors
- 👤 E. Marston Moffatt
- 👤 Richard E. Swarts
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 07:49
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/58
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
227 words
Angular velocity sensor means, comprising: a nozzle block for enclosing a jet chamber having a reference jet chamber with a reference jet axis and having nozzle means disposed at one end of said chamber for discharging a fluid jet along said reference jet axis; a sensor plug having at least one pair of sensing elements mounted thereon, said plug disposed at an opposite end of said chamber such that said sensing elements are disposed symmetrically about said reference jet axis in a plane perpendicular thereto, each pair of sensing elements being cooled differentially in response to deflection of said fluid jet from said reference jet axis in the presence of sensor rotation about a rotation axis perpendicular to said reference jet axis, said deflection being in proportion to the angular velocity of said sensor, each of said sensing elements having resistance values which vary according to the amount of cooling received by each, said plug having a single passage for discharging fluid from said jet chamber, said passage disposed symmetrically with respect to said chamber and said sensing elements for reducing flow disturbances; an impulse pump having a diaphragm of a selected material for delivering a fluid under pressure to said nozzle means to form said fluid jet; and detector circuit means, responsive to said sensing elements resistance values for providing signals indicative of said angular velocity.
Claim 2
Dependent Claim
227 words
Angular velocity sensor means, comprising: a nozzle block for enclosing a jet chamber having a reference jet chamber with a reference jet axis and having nozzle means disposed at one end of said chamber for discharging a fluid jet along said reference jet axis; a sensor plug having at least one pair of sensing elements mounted thereon, said plug disposed at an opposite end of said chamber such that said sensing elements are disposed symmetrically about said reference jet axis in a plane perpendicular thereto, each pair of sensing elements being cooled differentially in response to deflection of said fluid jet from said reference jet axis in the presence of sensor rotation about a rotation axis perpendicular to said reference jet axis, said deflection being in proportion to the angular velocity of said sensor, each of said sensing elements having resistance values which vary according to the amount of cooling received by each, said plug having a single passage for discharging fluid from said jet chamber, said passage disposed symmetrically with respect to said chamber and said sensing elements for reducing flow disturbances; an impulse pump having a diaphragm of a selected material for delivering a fluid under pressure to said nozzle means to form said fluid jet; and detector circuit means, responsive to said sensing elements resistance values for providing signals indicative of said angular velocity.
Claim 3
Dependent Claim
12 words
The sensor of claim 1, wherein said diaphragm selected material is metal.
Claim 4
Dependent Claim
27 words
The sensor of claim 1, wherein said sensing elements are separated to maximize scale factor and minimize flow disturbances due to heating effects in said sensing elements.
Claim 5
Dependent Claim
18 words
The sensor of claim 1, wherein said sensing elements are wires, each about 5×10 -6 meter in diameter.
Claim 6
Dependent Claim
19 words
The sensor of claim 1, wherein said nozzle end of said jet chamber is penetrated only by said nozzle.
Claim 7
Dependent Claim
17 words
The sensor of claim 5, wherein said impulse pump operates at a frequency of about 3000 Hz.
Claim 8
Dependent Claim
17 words
The sensor of claim 1, wherein said impulse pump operates at a frequency of about 3000 Hz.
Claim 9
Dependent Claim
23 words
The sensor of claim 1, wherein said pump discharges into two passages in said nozzle block disposed on opposite sides of said chamber.
Claim 10
Dependent Claim
36 words
The sensor of claim 1, wherein said fluid discharged from said single passage is returned by means of said impulse pump to said nozzle means through two passages disposed 180 degrees apart within said nozzle block.
Claim 11
Dependent Claim
53 words
The sensor of claim 2, wherein said pump further comprises a magnetic steel laminated core having a drive coil wound thereon, said core providing a low reluctance path for magnetic drive flux in a magnetic drive circuit including said core, said magnetic steel diaphragm, and a gap between said core and said diaphragm.
Claim 12
Dependent Claim
10 words
The sensor of claim 10, wherein said core is E-shaped.
Claim 13
Dependent Claim
85 words
The sensor of claim 10, wherein said pump further comprises sensing poles having a sensing coil wound thereon, said poles providing a low reluctance path for magnetic sensing flux in a magnetic circuit for inducing a sensing signal in a sensing circuit, said sensing signal being indicative of diaphragm displacement amplitude and frequency, said magnetic circuit including said poles, said diaphragm, and a gap between said poles and said diaphragm and wherein said sensing coils is disposed in quadrature with respect to said drive coil.
Claim 14
Dependent Claim
17 words
The sensor of claim 2, wherein said pump includes a steel flexure resostance welded to said diaphragm.
Claim 15
Dependent Claim
13 words
The sensor of claim 12, wherein said magnetic sensing circuit includes permanent magnets.
References Cited (Backward Citations)
US2312712A
Cited
US3381623A
Cited
US3587328A
Cited
US3635095A
Cited
SU617716A1
Cited
US4254659A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-01-04 | 1991-07-06 | 1992-01-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-01-04 | 1995-07-06 | 1996-01-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-01-04 | 1999-07-06 | 2000-01-05 | $7700.00 | Window Closed / Lapsed |