Patent US4898343A successfully refreshed from Google Patents.
US4898343A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Thrust-deflecting vane device of V/STOL aircraft
Assignee: Subaru Corp
•
Filing: 1988-12-20
•
Granted: 1990-02-06
•
Expires: 2008-12-20
Abstract
Abstract Two tail control surfaces operable doubly as thrust-deflecting vanes are rotatably supported on respective lateral sides of a jet engine of a V/STOL aircraft. Each tail surface can be actuated to rotate about an axis parallel to the engine axis and also to rotate about an axis perpendicular to the engine axis. The tail surfaces can be placed in outer positions on respective lateral sides of the engine for high-speed flight to function as stabilizer surfaces and to be placed within the engine exhaust gas stream and, moreover, to be placed in an inclined state relative thereto thereby to deflect the stream downward for slow-speed or hovering flight.
Inventors
- 👤 Keisuke Kamo
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 18:39
CPC Classifications
B; B64; B64C; B64C29/00; B64C29/0008; B64C29/0041; B64C29/0075; B64C15/00; B64C15/02
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
204 words
A thrust-deflecting vane device for a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces and said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including a universal joint mechanism with a first yoke having a root part secured to the airframe side, a second yoke having a root art secured to the tail surface side, first and second rods rigidly fixed perpendicularly to each other to form a cross-shaped spider, the ends of said first rod being pivotally connected to respective tines of said first yoke, the ends of said second rod being pivotally connected to respective tines of said second yoke, a horizontal actuator connected between one end of said first rod and the tail surface side to controllably vary the distance therebetween, and a vertical actuator connected between one end of said second rod and the airframe side to controllably vary the distance therebetween.
Claim 2
Dependent Claim
204 words
A thrust-deflecting vane device for a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces and said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including a universal joint mechanism with a first yoke having a root part secured to the airframe side, a second yoke having a root art secured to the tail surface side, first and second rods rigidly fixed perpendicularly to each other to form a cross-shaped spider, the ends of said first rod being pivotally connected to respective tines of said first yoke, the ends of said second rod being pivotally connected to respective tines of said second yoke, a horizontal actuator connected between one end of said first rod and the tail surface side to controllably vary the distance therebetween, and a vertical actuator connected between one end of said second rod and the airframe side to controllably vary the distance therebetween.
Claim 3
Dependent Claim
133 words
A thrust-deflecting vane device for a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces being provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces with said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including brackets extending longitudinally along and being fixed to a housing of said jet engine, vane bosses being mounted on said respective brackets and adapted to rotate about respective longitudinal axes, and said tail surfaces being mounted on said respective vane bosses and adapted to rotate about respective lateral axes.
Claim 4
Dependent Claim
133 words
A thrust-deflecting vane device for a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces being provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces with said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including brackets extending longitudinally along and being fixed to a housing of said jet engine, vane bosses being mounted on said respective brackets and adapted to rotate about respective longitudinal axes, and said tail surfaces being mounted on said respective vane bosses and adapted to rotate about respective lateral axes.
Claim 5
Dependent Claim
88 words
A thrust-deflecting vane device of a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces being provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces with said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including a universal joint mechanism.
Claim 6
Dependent Claim
88 words
A thrust-deflecting vane device of a vertical/short take-off and landing (V/STOL) aircraft having an airframe and a jet engine which discharges an exhaust gas stream, comprising: tail surfaces being provided at an aft part of said airframe; and a tail surface deflecting device intercoupling said tail surfaces with said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said tail surface deflecting device including a universal joint mechanism.
Claim 7
Dependent Claim
93 words
A thrust-deflecting vane device for a vertical/short take-off and landing aircraft having a jet engine which discharges a rearward exhaust gas stream, comprising: a pair of boom-like brackets fixedly supported along respective side faces of a housing of said jet engine; runner boss means, rotatably mounted on said boomlike brackets about a longitudinal axis, for providing a high-speed flight position and a low-speed flight position; and tail control surface means, rotatably mounted on said runner boss means about a lateral axis, for deflecting said exhaust gas stream and controlling attitude of said aircraft.
Claim 8
Dependent Claim
93 words
A thrust-deflecting vane device for a vertical/short take-off and landing aircraft having a jet engine which discharges a rearward exhaust gas stream, comprising: a pair of boom-like brackets fixedly supported along respective side faces of a housing of said jet engine; runner boss means, rotatably mounted on said boomlike brackets about a longitudinal axis, for providing a high-speed flight position and a low-speed flight position; and tail control surface means, rotatably mounted on said runner boss means about a lateral axis, for deflecting said exhaust gas stream and controlling attitude of said aircraft.
Claim 9
Dependent Claim
197 words
A thrust-deflecting vane device for a vertical/short take-off and landing aircraft having an airframe and a jet engine which discharges a rearward exhaust gas stream, comprising: tail surfaces provided as an aft part of said airframe; and a universal joint mechanism intercoupling said tail surfaces and said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said universal joint mechanism including a first yoke having a root part secured to the airframe side, a second yoke having a root part secured to the tail surface side, first and second rods rigidly fixed perpendicularly to each other to form a cross-shaped spider, the ends of said first rod being pivotally connected to respective tines of said first yoke, the ends of said second rod being pivotally connected to respective tines of said second yoke, a horizontal actuator connected between one end of said first rod and the tail surface side to controllably vary the distance therebetween, and a vertical actuator connected between one end of said second rod and the airframe side to controllably vary the distance therebetween.
Claim 10
Dependent Claim
197 words
A thrust-deflecting vane device for a vertical/short take-off and landing aircraft having an airframe and a jet engine which discharges a rearward exhaust gas stream, comprising: tail surfaces provided as an aft part of said airframe; and a universal joint mechanism intercoupling said tail surfaces and said airframe and being operable to move said tail surfaces selectively between first positions on the outer lateral sides of said airframe and second positions in said exhaust gas stream, said universal joint mechanism including a first yoke having a root part secured to the airframe side, a second yoke having a root part secured to the tail surface side, first and second rods rigidly fixed perpendicularly to each other to form a cross-shaped spider, the ends of said first rod being pivotally connected to respective tines of said first yoke, the ends of said second rod being pivotally connected to respective tines of said second yoke, a horizontal actuator connected between one end of said first rod and the tail surface side to controllably vary the distance therebetween, and a vertical actuator connected between one end of said second rod and the airframe side to controllably vary the distance therebetween.
References Cited (Backward Citations)
US3515361A
Cited
US3730460A
Cited
US4116405A
Cited
US4203569A
Cited
JPS5526038A
Cited
US4296896A
Cited
JPS57134396A
Cited
US4482109A
Cited
US4538779A
Cited
JPS59141753A
Cited
JPS60237147A
Cited
US4726545A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-02-05 | 1993-08-07 | 1994-02-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-02-05 | 1997-08-07 | 1998-02-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-02-05 | 2001-08-07 | 2002-02-06 | $7700.00 | Window Closed / Lapsed |