US4566656A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Steering mechanism for an explosively fired projectile
Assignee: Hughes Missile Systems Co
•
Filing: 1984-03-06
•
Granted: 1986-01-28
•
Expires: 2004-03-06
Abstract
Abstract A projectile trajectory correction system, the projectile itself including a unique steering arrangement. The projectile, initially part of a shell cartridge, is fired, and its position is automatically sensed. A corrected trajectory necessary to hit a target is calculated and data commands are transmitted to the projectile. The data command signals are sensed by an antenna on the projectile. The antenna in turn generates a signal which is fed to the projectile steering mechanism which is deflected in response thereto to steer the projectile onto the correct trajectory. The steering mechanism includes an elongated rod extending from the rear of the projectile into the surrounding air stream. Deflection of the rod provides the actual steering.
Inventors
- 👤 Inge Maudal
- 👤 Byron M. Niemeier
- 👤 Larry D. Wedertz
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 19:58
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/30; F41G7/301; F42; F42B; F42B10/00; F42B10/60; F42B10/62; F42B10/64
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
167 words
A system for correcting the trajectory of a projectile while in flight, the projectile being propelled by a powder charge fired from a cartridge shell in a gun at a ground position, the system comprising: means remote from the projectile for sensing the position of the projectile in flight; said remote means including: (a) means responsive to said sensing means for determining the correct trajectory for said projectile and generating command signals for controlling the projectile to follow said correct trajectory; and (b) means for transmitting said command signals to an antenna mounted to said projectile; and means coupled to the antenna for generating signals in response to said command signals to cause an elongated member extending rearwardly from said projectile to deflect off-axis in the air stream interacting therewith, said elongated member extending into said powder charge prior to firing and being selectively deflectable relative to the longitudinal axis of the projectile in response to said generated signals, thereby steering said projectile to the correct trajectory.
Claim 2
Independent Claim
167 words
A system for correcting the trajectory of a projectile while in flight, the projectile being propelled by a powder charge fired from a cartridge shell in a gun at a ground position, the system comprising: means remote from the projectile for sensing the position of the projectile in flight; said remote means including: (a) means responsive to said sensing means for determining the correct trajectory for said projectile and generating command signals for controlling the projectile to follow said correct trajectory; and (b) means for transmitting said command signals to an antenna mounted to said projectile; and means coupled to the antenna for generating signals in response to said command signals to cause an elongated member extending rearwardly from said projectile to deflect off-axis in the air stream interacting therewith, said elongated member extending into said powder charge prior to firing and being selectively deflectable relative to the longitudinal axis of the projectile in response to said generated signals, thereby steering said projectile to the correct trajectory.
Claim 3
Dependent Claim
25 words
The system of claim 1 wherein said elongated member comprises a rod which extends substantially the length of the powder charge within the cartridge shell.
Claim 4
Dependent Claim
10 words
The system of claim 2 wherein said rod is hollow.
Claim 5
Dependent Claim
10 words
The system of claim 3 wherein said rod is perforated.
Claim 6
Dependent Claim
31 words
The system of claim 1 wherein the length of the elongated member, prior to firing, is less than the length of the space for the powder charge within the cartridge shell.
Claim 7
Dependent Claim
27 words
The system of claim 5 wherein the elongated member extending from the projectile in flight exceeds the length of the powder charge space within the cartridge shell.
Claim 8
Dependent Claim
27 words
The system of claim 6 wherein the elongated member is extendible from a first length before firing to a second length when the projectile is in flight.
Claim 9
Dependent Claim
27 words
The system of claim 7 wherein said elongated member comprises a telescoping metal rod including a plurality of sections of differing diameters capable of being telescoped together.
References Cited (Backward Citations)
US1388932A
Cited
US1277225A
Cited
US1506785A
Cited
US2579823A
Cited
US2397088A
Cited
US2421085A
Cited
US2792190A
Cited
US3020457A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-01-27 | 1989-07-29 | 1990-01-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-01-27 | 1993-07-29 | 1994-01-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-01-27 | 1997-07-29 | 1998-01-28 | $7700.00 | Window Closed / Lapsed |