# US 11,441,514 B2 · Tertiary lock

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- Number: US 11,441,514 B2
- Document ID: US11441514B2
- Status: Granted
- Kind: B2
- Application number: 16/149,455
- Filed: 2018-10-02
- Published: 2020-04-02
- Granted: 2022-09-13
- Earliest claimed: 2018-10-02
- Assignees: Woodward, Inc.
- Applicants: Woodward, Inc.
- Inventors: Joseph Thomas Kopecek; Julian Sweet
- Web page: https://patentgrep.com/patent/US11441514B2

## CPC

- B64D 29/06: Attaching of nacelles, fairings or cowlings
- F02K 1/766: {with blocking systems or locking devices; Arrangement of locking devices for thrust reversers}
- B64D 33/04: of exhaust outlets or jet pipes
- E05B 47/0603: {the detent moving rectilinearly}
- F02K 1/763: {with actuating systems or actuating devices; Arrangement of actuators for thrust reversers}
- F05D 2270/52: by electrical means, e.g. relays or switches
- F05D 2270/62: Electrical actuators
- F05D 2270/66: Mechanical actuators (F05D2270/62 takes precedence)
- B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00)
- E05B: LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

The subject matter of this specification can be embodied in, among other things, a thrust reverser tertiary lock apparatus that includes a probe affixed to an aircraft engine frame and having a shaft having a barb at a first end and configurable to a first configuration and a second configuration, and a receiver affixed to a thrust reverser transcowl slider configured to accommodate the barb and having an end wall with an aperture defined therein, the aperture shaped to permit escapement of the barb in the first configuration and prevent escapement of the barb in the second configuration.

## Claims

### Claim 1

A thrust reverser tertiary lock apparatus comprising:
a probe affixed to an aircraft engine frame and comprising a shaft having a barb at a first end and rotatable about an axis to a first configuration and a second configuration; and
a receiver affixed to a thrust reverser transcowl slider or door configured to accommodate the barb and comprising an end wall having an aperture defined therein, the aperture shaped to permit escapement of the barb in the first configuration and prevent escapement of the barb in the second configuration;
wherein the barb comprises a bevel configured to contact an edge of the aperture and urge rotation of the barb about the axis from the second configuration to the first configuration during penetration of the aperture by the barb.

### Claim 2 (depends on 1)

The thrust reverser tertiary lock apparatus of claim 1, further comprising a rotary actuator configured to rotate the barb about the axis, wherein the barb is rotatable by the rotary actuator between the first configuration and the second configuration.

### Claim 3 (depends on 2)

The thrust reverser tertiary lock apparatus of claim 2, wherein the aperture is rotationally asymmetric relative to the axis and the barb is rotationally asymmetric about the axis between the first configuration and the second configuration, such that the barb is escapable from the receiver through the aperture in the first configuration and the barb is interfered with by the end wall such that escapement of the barb is prevented in the second configuration.

### Claim 4 (depends on 2)

The thrust reverser tertiary lock apparatus of claim 2, wherein the barb is configured to rotate to the first configuration when activated and rotate to the second configuration when deactivated.

### Claim 5 (depends on 2)

The thrust reverser tertiary lock apparatus of claim 2, wherein an edge of the aperture comprises a bevel configured to contact the barb and urge rotation of the barb about the axis from the second configuration to the first configuration during penetration of the aperture by the barb.

### Claim 6 (depends on 5)

The thrust reverser tertiary lock apparatus of claim 5, further comprising a torsion bias spring configured to rotate the barb about the axis from the first configuration to the second configuration after the barb has completed penetration of the bevel.