Airborne electromagnetic system with rigid loop structure comprised of lightweight modular non-rotational frames
The present invention provides a light weight, modular and rigid structure for supporting the transmitter loop of an airborne electromagnetic system. The airborne electromagnetic surveying system comprises a tow assembly connected to an aircraft, the tow assembly including a transmitter section comprising a transmitter coil for generating a primary electromagnetic field that induces a secondary electromagnetic field. The transmitter coil is supported by a generally rigid transmitter frame. The transmitter frame comprises a plurality of frame sections assembled in a way such that the generally rigid transmitter frame substantially retains a rigid shape during operation. The system may also include a receiver section located above the generally rigid transmitter frame in between the aircraft and the generally rigid transmitter frame for detecting the secondary electromagnetic field.
1. An airborne electromagnetic surveying system comprising:
a tow assembly connected to an aircraft, the tow assembly further comprising:
a transmitter section comprising:
a transmitter coil for generating a primary electromagnetic field that induces a secondary electromagnetic field, and
a generally rigid transmitter frame for supporting the transmitter coil, the transmitter frame comprising a plurality of fixedly connected frame sections assembled in a way such that the generally rigid transmitter frame substantially retains its shape during operation; and
a receiver section for detecting the secondary electromagnetic field,
wherein a first frame section has an elongated section and a connecting section connected to the elongated section,
a second frame section has a receiving section,
the connecting section is sized to fit tightly inside the receiving section to prevent rotation of the first frame section relative to the second frame section,
the first frame section has a tab on the connecting section,
the second frame section has a slot on the receiving section, and
the tab extends into the slot after the connecting section enters inside the receiving section for assembling the first and second frame sections.
2. The airborne electromagnetic surveying system of claim 1 , wherein the receiver section is located above the generally rigid transmitter frame in between the aircraft and the generally rigid transmitter frame.
3. The airborne electromagnetic surveying system of claim 1 , wherein the receiver section is located at the center of the generally rigid transmitter frame.
4. The airborne electromagnetic surveying system of claim 1 , wherein the plurality of frame sections are connected using fastening means to substantially eliminate or minimize relative movements therebetween.
5. The airborne electromagnetic surveying system of claim 1 , wherein when the first and the second frame sections are connected, the tab and the slot engage with each other to substantially eliminate or minimize relative movements or rotations between the first and the second frame sections.
6. The airborne electromagnetic surveying system of claim 1 , wherein the generally rigid transmitter frame has a diameter in excess of 30 meters.
7. The airborne electromagnetic surveying system of claim 1 , wherein the plurality of frame sections are serially connected to form the generally rigid transmitter frame.
8. The airborne electromagnetic surveying system of claim 1 , wherein the frame sections are connected in a manner that substantially eliminates the relative rotation therebetween, thereby preventing distortion of the shape of the transmitter frame during operation.
9. The airborne electromagnetic surveying system of claim 1 , wherein the generally rigid transmitter frame is constructed using lightweight materials.
10. A transmitter section for an airborne electromagnetic survey system, comprising:
a transmitter coil, and
a generally rigid transmitter frame for supporting the transmitter coil, the transmitter frame comprising a plurality of fixedly connected frame sections assembled in a way such that the generally rigid transmitter frame substantially retains its shape during operation,
wherein a first frame section has an elongated section and a connecting section connected to the elongated section,
a second frame section has a receiving section,
the connecting section is sized to fit tightly inside the receiving section to prevent rotation of the first frame section relative to the second frame section,
the first frame section has a first interlocking member on the connecting section,
the second frame section has a second interlocking member on the receiving section, and
the first interlocking member frictionally engages with the second interlocking member after the connecting section enters inside the receiving section for assembling the first and second frame sections.