US4095761A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aerial refueling spoiler
Assignee: Boeing Co
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Filing: 1976-09-29
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Granted: 1978-06-20
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Expires: 1996-09-29
Abstract
Abstract An aerodynamic spoiler mounted on the upper forward surface of the fuselage of an aircraft which is equipped to be refueled by another aircraft while in flight. The spoiler counteracts aerodynamic disturbances produced by the refueling boom and the resultant instabilities in pitch in the aircraft receiving fuel. Four species of the spoiler are disclosed and the device may be made retractable to eliminate drag when not in use.
Inventors
- 👤 Ardell J. Anderson
- 👤 Kenneth D. Hurley
- 👤 Richard H. Leckman
- 👤 Ronald H. Robinson
- 👤 Edward N. Tinoco
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 05:13
CPC Classifications
B; B64; B64D; B64D39/00
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
102 words
In combination with an aircraft having an aerial refueling apparatus for receiving fuel while in flight including a refueling receptacle located on the forward surface of its fuselage, the improvement comprising aerodynamic means mounted on said forward surface of the fuselage for improving the pitch stability of the aircraft during aerial refueling wherein said means comprises a spoiler plate having a forward face of height h and width w, and a thickness t substantially less than h or w, said spoiler plate being oriented such that a normal to said forward face is substantially perpendicular to the pitch axis of the aircraft.
Claim 2
Dependent Claim
102 words
In combination with an aircraft having an aerial refueling apparatus for receiving fuel while in flight including a refueling receptacle located on the forward surface of its fuselage, the improvement comprising aerodynamic means mounted on said forward surface of the fuselage for improving the pitch stability of the aircraft during aerial refueling wherein said means comprises a spoiler plate having a forward face of height h and width w, and a thickness t substantially less than h or w, said spoiler plate being oriented such that a normal to said forward face is substantially perpendicular to the pitch axis of the aircraft.
Claim 3
Dependent Claim
25 words
The improvement of claim 1 wherein said spoiler plate is located aft of said receptacle and extends upward from said forward surface of the fuselage.
Claim 4
Dependent Claim
17 words
The improvement of claim 2 further comprising means for retracting said spoiler plate into a stowed position.
Claim 5
Dependent Claim
39 words
The improvement of claim 3 wherein said spoiler plate is pivotally mounted to said fuselage and may be rotated by said means for retracting from an extended position into a stowed position essentially flush with the local fuselage surface.
Claim 6
Dependent Claim
37 words
The improvement of claim 1 wherein said aircraft has a cockpit and a cockpit roof located in the upper forward portion of the fuselage and wherein said spoiler plate is located on the roof of said cockpit.
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) | 1981-06-19 | 1981-12-19 | 1982-06-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-06-19 | 1985-12-19 | 1986-06-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-06-19 | 1989-12-19 | 1990-06-20 | $7700.00 | Window Closed / Lapsed |