Closed loop control system for controlling an air discharge out of an aircraft body

• US 5,934,614 A
• Filed: 07/11/1997
• Issued: 08/10/1999
• Est. Priority Date: 07/13/1996
• Status: Expired due to Term

• Current Assignee: Daimlerchrysler North America Corporation (Mercedes-Benz Group AG)
• Original Assignee: Daimlerchrysler North America Corporation (Mercedes-Benz Group AG)
• Inventors: Klein, Bernd, Mueller, Wolfgang
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US08/891,519
• Time in Patent Office: 760 Days
• Field of Search: 244/118.5, 244/129.1, 454/76, 454/71, 454/74, 454/162
• US Class Current: 244/118.5
• CPC Class Codes: B64D 13/04 Automatic control of pressure
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

The flow volume of used air to be discharged from an aircraft cabin is controlled in a valve control system in which each outflow valve has at least two slave controllers responsive to any one of at least two master controllers in a closed loop control system. For this purpose the slave controllers and the master controllers are interconnected by an intermeshed conductor network including a plurality of conductor sections interconnected by electrical conductor junctions or optical conductor couplers forming interfaces between the conductor sections to provide a redundant number of communication paths to keep the system operable even if failures or faults occur.

Claims

1. A closed loop system for controlling an air discharge out of an aircraft body having a body wall, said system comprising least one air discharge valve for passing used air through said body wall, at least two master controllers for each air discharge valve, at least two slave valve controllers for controlling the operation of said at least one air discharge valve in response to any one of said at least two master controllers, and a ring circuit (3A to 3H) forming an information transmission loop interconnecting said master controllers with said slave valve controllers for transmitting control information from any one of said master controllers to any one of said slave valve controllers and for transmitting feedback information from any one of said slave valve controllers to any one of said master controllers, said ring circuit establishing under all operating conditions the shortest possible conductor path between any one of said master controllers and any one of said slave valve controllers for passing signals from any one of said master controllers to any one of said slave valve controllers and vice versa through said shortest possible conductor path.

2. The closed loop control system of claim 1, wherein said ring circuit forming said information transmission loop comprises a plurality of conductor sections (3E, 3F, 3G, 3H) and interfaces (3A, 3B, 3C, 3D) interconnecting said conductor sections for forming a plurality of transmission cross-links at said interfaces, and a plurality of access conductor sections (1B, 1C, 2B, 2C) connecting said master controllers and said a slave valve controllers to certain of said interfaces in said ring circuit.

3. The closed loop control system of claim 2, wherein said interfaces are conductor junctions or optical couplers.

4. The closed loop control system of claim 1, comprising at least two air discharge valves, at least two master controllers for each of said two air discharge valves, at least two slave valve controllers for each of said two air discharge valves, and wherein said ring circuit forming said information transmission loop comprises interlinked information transmission paths for controlling anyone of said slave valve controllers through any one of said master controllers whereby in an emergency an operable yet shortest possible transmission path can bypass a currently inoperable transmission path.

5. The closed loop control system of claim 4, further comprising additional linking transmission paths in said ring circuit for increasing the number of possible bypass transmission paths.

6. The closed loop control system of claim 1, wherein said ring circuit comprises at least four interfaces arranged in pairs (3A, 3D and 3B, 3C), a plurality of first conductor sections (3E, 3G) interconnecting said interfaces (3A, 3D;

3B, 3C) forming pairs, second conductor sections (3F, 3H) cross-linking said interfaces (3A, 3B;

3C, 3D) thereby closing said ring circuit and ring entering and exiting third conductor sections (1B, 2B, 2C, 1C) connecting said slave valve controllers and said master controllers to said ring circuit.

7. The closed loop control system of claim 6, wherein said first, second and third conductor sections are insulated electrical conductors and said interfaces are electrical junctions.

8. The closed loop control system of claim 6, wherein said first, second and third conductors sections are lightwave conductors and said interfaces are fiber optical couplers.

9. The closed loop control system of claim 6, wherein said first, second and third conductor sections are bidirectional databus conductors.

10. The closed loop control system of claim 1, wherein said ring circuit forming said information transmission loop comprises at least one conductor mesh network (3'"'"') including intermeshing interfaces in said mesh network and conductor sections interconnected by said interfaces, wherein any interface is intermeshed with any other interface in said conductor mesh network.

11. The closed loop control system of claim 1, wherein each of said master controllers comprises an information evaluating logic circuit for determining faulty system sections in response to received information and for providing respective control signals that cause bypassing any faulty system sections along said shortest possible conductor paths.

12. The closed loop control system of claim 11, wherein said information for evaluation by said logic circuit is feedback information from said slave valve controllers.