Primary flight display presenting resolution advisory information provided by a traffic alert and collision avoidance system

• US 5,185,606 A
• Filed: 05/08/1990
• Issued: 02/09/1993
• Est. Priority Date: 05/08/1990
• Status: Expired due to Fees

• Current Assignee: Fokker Aircraft, B.V.
• Original Assignee: Fokker Aircraft, B.V.
• Inventors: Schless, Michel M. C., Verbaarschot, Petrus A. A., Hultzer, Wim J.
• Primary Examiner(s): Ng, Jin F.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/520,507
• Time in Patent Office: 1,008 Days
• Field of Search: 340/961, 340/967, 340/968, 340/974, 340/975, 364/461, 342/29, 342/455
• US Class Current: 340/961
• 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
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft

Abstract

A display for presenting symbolically to an aircraft flight crew the resolution advisory information developed by a Traffic Collision Avoidance System (TCAS) computer aboard an aircraft. The flight display shows a a line symbol representing the artificial horizon, a pitch scale extending perpendicular to said line symbol and indicating pitch angles with reference to said line symbol, and an aircraft reference symbol indicating by its position along said pitch scale the momentaneous aircraft pitch attitude. Furthermore a pitch cue symbol is displayed consisting of a first line segment extending parallel to the artificial horizon and across said pitch scale, said first line segment indicating a limit pitch value processed from the TCAS vertical speed limit ouput, and an area indicator extending below or above said line segment indicating a range of pitch values bounded by said limit pitch value, which range of pitch values has to be avoided by the aircraft flight crew.

Claims

1. A display for presenting symbolically to an aircraft flight crew resolution advisory information developed by a Traffic Collision Avoidance System (TCAS) computer aboard an aircraft said computer providing a vertical speed limit output wherein said display comprises:

a line symbol representing the artificial horizon,

a pitch scale extending perpendicularly to said line symbol and indicating pitch angles with reference to said line symbol,

an aircraft reference symbol indicating by its position on said pitch scale the instantaneous aircraft pitch attitude, wherein said display further comprises;

a pitch cue symbol having

a first line segment extending parallel to the artificial horizon and across said pitch scale, said first line-segment indicating a limit pitch value processed from said TCAS vertical speed limit output, and

an area indicator extending from said line segment and indicating a range of pitch values bounded by said limit pitch value, which range of pitch values has to be avoided by the aircraft flight crew.

2. A display according to claim 1 wherein the area indicator comprises two auxilliary line segments extending from the opposite ends of said first line segment perpendicular thereto in the direction of the pitch values to be avoided such that a U-shaped symbol is obtained.

3. A display according to claim 1 wherein said pitch cue symbol further comprises:

a second line segment extending parallel to the artificial horizon and across said pitch scale, said line segment indicating a second limit pitch value processed from the TCAS vertical speed limit output; and

a second area indicator extending from said second line segment and indicating a second range of pitch values bounded by said second limit pitch value, which second range of pitch values is not coinciding with said first range of pitch value and has to be avoided also by the aircraft flight crew.

4. A display according to claim 3 wherein the second area indicator consists of two further auxiliary line segments extending from the opposite ends of said second line segment perpendicularly thereto in the direction of the pitch values to be avoided such that a U-shaped symbol is obtained.

5. A display according to claim 3 wherein said pitch cue symbol further comprises an arrow shaped symbol positioned within the area indicator and pointing to said first or second line segment respectively.

6. A display according to claim 2 wherein the aircraft reference symbol is of a generally known X-bar type reference signal comprising a boresight symbol and two wing symbols and wherein the distance between the auxiliary line segments is smaller than the distance between the wing symbols of the aircraft reference symbol.

7. A display according to claim 1 wherein said area indicator is rendered visually distinctive by markings selected from the group consisting of shading, hatching, crosshatching or a color differentiation.