Taxi and slope landing symbology for a helicopter

• US 6,052,069 A
• Filed: 10/29/1997
• Issued: 04/18/2000
• Est. Priority Date: 10/29/1997
• Status: Expired due to Fees

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Occhiato, John J., Silder, Stephen H. Jr., Harper, Howard P.
• Primary Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US08/959,834
• Time in Patent Office: 902 Days
• Field of Search: 340/946, 340/963, 340/945, 340/960, 340/971, 340/980, 244/1 R, 244/17-11, 73/178 H, 701/14, 701/9, 701/8, 701/15, 701/16
• US Class Current: 340/946
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Abstract

Taxi and slope landing symbology for a helicopter having a main rotor drive shaft and a main rotor hub defining a hub moment, wherein the main rotor drive shaft and the main rotor hub have hub moment limits. The taxi and slope landing symbology comprises a first symbol for providing a symbolic representation of the hub moment limits, and a second symbol for providing a dynamic symbolic representation of the hub moment, wherein the second symbol is disposed in combination with the first symbol to provide a visual cue of the hub moment relative to the hub moment limits.

Claims

1. Taxi and slope landing symbology for a helicopter having a main rotor drive shaft and a main rotor hub defining a hub moment, the main rotor drive shaft and the main rotor hub having hub moment limits, the taxi and slope landing symbology comprising:

(a) a first symbol for providing a symbolic representation of the hub moment limits;

(b) a second symbol for providing a dynamic symbolic representation of the instantaneous hub moment, and disposed in combination with said first symbol to provide a visual cue of the instantaneous hub moment relative to the hub moment limits; and

(c) a third symbol for providing a symbolic representation of zero hub moment, and disposed in combination with said first symbol and said second symbol to provide a visual cue of the instantaneous hub moment relative to the hub moment limits and said zero hub moment.

2. The taxi and slope landing symbology of claim 1, wherein said first symbol comprises a polygon having sides representative of the instantaneous hub moment limits, and defining an interior region.

3. The taxi and slope landing symbology of claim 2, wherein said second symbol comprises a closed curvilinear geometric figure disposed within said interior region of said polygon and capable of movement relative to said sides of said polygon in response to changes in the hub moment, wherein the position of said closed curvilinear geometric figure relative to said sides of said polygon provides said visual cue of the instantaneous hub moment relative to the hub moment limits of the helicopter.

4. The taxi and slope landing symbology of claim 1, wherein said first symbol comprises a polygon having sides representative of the hub moment limits, and defining an interior region.

5. The taxi and slope landing symbology of claim 4, wherein said third symbol comprises cross hairs disposed within said interior region of said polygon in a static relationship relative to said sides of said polygon.

6. The taxi and slope landing symbology of claim 1,

(a) wherein the helicopter further includes a landing assembly for supporting the helicopter relative to a surface;

and

(b) wherein the taxi and slope landing symbology further comprises a fourth symbol disposed in combination with said first symbol, for providing a symbolic representation of contact status between said landing assembly and the surface.

7. The taxi and slope landing symbology of claim 6, wherein:

(a) said landing assembly comprises landing gear having a plurality of wheels; and

(b) said fourth symbol comprises a plurality of closed curvilinear geometric figures, each of said closed curvilinear geometric figures corresponding to one of said plurality of wheels;

(c) wherein each of said closed curvilinear geometric figures has a first configuration representative of said corresponding wheel not contacting the surface, and a second configuration representative of said corresponding wheel contacting the surface, wherein said first configuration and said second configuration provide, respectively, a visual cue as to which of said plurality of wheels are not in contact with the surface and which of said plurality of wheels are in contact with the surface.

8. Taxi and slope landing symbology for a helicopter having a video display subsystem, a main rotor drive shaft and a main rotor hub defining a hub moment, a hub moment sensor subsystem disposed in combination with the main rotor drive shaft for generating data representative of the instantaneous hub moment, a computer subsystem for processing the data representative of the instantaneous hub moment, the computer subsystem being programmed with hub moment limit data representative of hub moment limits for the helicopter, the computer subsystem also including a symbol generator for generating the taxi slope landing symbology in combination with the video display subsystem, the taxi and slope landing symbology comprising:

(a) a first symbol for providing a symbolic representation of the hub moment limits;

(b) a second symbol for providing a dynamic symbolic representation of the instantaneous hub moment, and disposed in combination with said first symbol to provide a visual cue of the instantaneous hub moment relative to the hub moment limits;

a

(c) a third symbol for providing a symbolic representation of zero hub moment, and disposed in combination with said first symbol and said second symbol to provide a visual cue of the instantaneous hub moment relative to the hub moment limits and said zero hub moment.

9. The taxi and slope landing symbology of claim 8, wherein said first symbol comprises a polygon having sides representative of the hub moment limits, and defining an interior region.

10. The taxi and slope landing symbology of claim 9, wherein said second symbol comprises a closed curvilinear geometric figure disposed within said interior region of said polygon and capable of movement relative to said sides of said polygon in response to changes in the instantaneous hub moment, wherein the position of said closed curvilinear geometric figure relative to said sides of said polygon provides said visual cue of the instantaneous hub moment relative to the hub moment limits.

11. The taxi and slope landing symbology of claim 8, wherein said first symbol comprises a polygon having sides representative of the hub moment limits, and defining an interior region.

12. The taxi and slope landing symbology of claim 11, wherein said third symbol comprises cross hairs disposed within said interior region of said polygon in a static relationship relative to said sides of said polygon.

13. The taxi and slope landing symbology of claim 8,

(a) wherein the helicopter further comprises a landing assembly for supporting the helicopter relative to a surface, a landing sensor subsystem disposed in combination with said landing assembly for generating data representative of contact status between said landing assembly and the surface, wherein the computer subsystem is operable to process said data representative of said contact status between said landing assembly and the surface;

and

(b) a fourth symbol disposed in combination with said first symbol, for providing a symbolic representation of said contact status between said landing assembly and the surface.

14. The taxi and slope landing symbology of claim 13, wherein:

(a) said landing assembly comprises landing gear having a plurality of wheels; and

(b) said fourth symbol comprises a plurality of closed curvilinear geometric figures, each of said closed curvilinear geometric figures corresponding to one of said plurality of wheels;

(c) wherein each of said closed curvilinear geometric figures has a first configuration representative of said corresponding wheel not contacting the surface, and a second configuration representative of said corresponding wheel contacting the surface, wherein said first configuration and said second configuration provide, respectively, a visual cue as to which of said plurality of wheels are not in contact with the surface and which of said plurality of wheels are in contact with the surface.

15. Taxi and slope landing symbology display system for a helicopter having a main rotor drive shaft and a main rotor hub defining a hub moment, the taxi and slope landing symbology display system comprising:

(a) a video display subsystem;

(b) a hub moment sensor subsystem disposed in combination with the main rotor drive shaft for generating data representative of the instantaneous hub moment; and

(c) a computer subsystem for processing said data representative of the instantaneous hub moment, said computer subsystem being programmed with hub moment limit data representative of hub moment limits for the helicopter, and including a symbol generator for generating taxi and slope landing symbology in combination with said video display subsystem, said taxi and slope landing symbology comprising

first symbol for providing a symbolic representation of said hub moment limits,

a second symbol for providing a dynamic symbolic representation of the instantaneous hub moment, and disposed in combination with said first symbol to provide a visual cue of the instantaneous hub moment relative to said hub moment limits, and

a third symbol for providing a symbolic representation of zero hub moment, and disposed in combination with said first symbol and said second symbol to provide a visual cue of the instantaneous hub moment relative to said hub moment limits and said zero hub moment.

16. The taxi and slope landing symbology display system of claim 15,

(a) wherein the helicopter further comprises a landing assembly for supporting the helicopter relative to a surface, a landing sensor subsystem disposed in combination with said landing assembly for generating data representative of contact status between said landing assembly and the surface, wherein said computer subsystem is operable to process said data representative of said contact status between said landing assembly and the surface;

and

(b) a fourth symbol disposed in combination with said first symbol, for providing a symbolic representation of said contact status between said landing assembly and the surface.

17. The taxi and slope landing symbology display system of claim 16, wherein:

(a) said landing assembly comprises landing gear having a plurality of wheels; and

(b) said fourth symbol comprises a plurality of closed curvilinear geometric figures, each of said closed curvilinear geometric figures corresponding to one of said plurality of wheels;

(c) wherein each of said closed curvilinear geometric figures has a first configuration representative of said corresponding wheel not contacting the surface, and a second configuration representative of said corresponding wheel contacting the surface, wherein said first configuration and said second configuration provide, respectively, a visual cue as to which of said plurality of wheels are not in contact with the surface and which of said plurality of wheels are in contact with the surface.